* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
TASK 72-53-00-440-802
1 . General.
A.This procedure gives instructions to assemble the high pressure turbine (HPT) rotor assembly (34-020 , 72-00-02) (SIN 15000).
B.Make sure that all personnel read and fully understand this procedure before use.
C.Install protective covers on all assemblies and hardware that will not be used.
D.Install all of the bolts with the heads up or forward unless specified differently.
E.Apply the lubricants to the threads and the friction surfaces only.
WARNING:
STODDARD SOLVENT IS TOXIC. USE PERSONAL PROTECTION EQUIPMENT.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
WARNING:
TOLUENE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
F.Before you do this assembly, make sure that all rabbet and structural flange mating surfaces are clean and free of any foreign material and high metal. If necessary, clean the parts with C04-002  Stoddard solvent, C04-035  isopropyl alcohol, or C04-036  toluene.
G.Follow the instructions to make temporary marking. Refer to TASK 70-16-02-350-017 (TEMPORARY MARKING) .
H.This assembly contains shafts that are very important. Critical areas of the shafts that require caution and a visual inspection during the assembly procedure, are identified throughout this procedure. Refer to Figure 1001.
I.Make sure that all the mounting areas between life-limited parts and assembly/disassembly fixtures are clean and free from foreign material.
2 . Tools, Equipment, and Materials.
NOTE:
You can use equivalent alternatives for tools, equipment, and consumable materials.
A.Tools and Equipment.
(1)Special Tools.
 
Tool No.
Description
 
7C2000P01
Rotor Components/Assembly Inspection System (rotor components/assembly inspection system)
NOTE:
Tool 7C2000P01 is alternative to 9471M13P03.
 
7C2068G01
Gage, Orientation - HPT Interstage Seal (orientation gage)
 
7C2071G01
Fixture, Install/Remove - Shank Nut, Disk, HPT Rotor (install/remove fixture)
 
7C2141G01
Dam, Chill Installation - HPT Rotor Interstage Seal (dam chill fixture)
 
7C2199G02
Fixture, Installation - Balance Arbor, HPT Rotor (installation fixture)
 
11C3002G04
Fixture, Install/Remove - HPT Rotor FWD Seal (install/remove fixture)
 
11C3006G01
Fixture, Install/Remove HPT Inner Stage Seal (install/remove fixture)
 
11C3008G01
Fixture, Support - HPT Rotor
 
11C3012G02
Adapter, Balance and Grind - HPT Rotor (balance and grind adapter)
NOTE:
Tool 11C3012G02 is an alternative to 11C3012G03.
 
11C3012G03
Adapter, Balance and Grind - HPT Turbine Rotor
 
11C3015G01
Container, HPT Rotor Stage 1 Blades (blade container)
 
11C3015G02
Container, HPT Rotor Stage 2 Blades (blade container)
 
11C3018G03
Fixture - Support, HPT Rotor, Vertical (vertical support fixture)
 
11C3019G03
Retainer, Blade - Slave HPT Rotor Stage 2 (slave blade retainer)
 
11C3021G02
Fixture, Heat - HPT Rotor, Stage 1 Disk (heater fixture)
NOTE:
Tool 11C3021G02 is alternative to 11C4617P01.
 
11C3022G01
Fixture, Install/Remove Stage 2 Disk HPT Rotor (install/remove fixture)
 
11C3024G03
Fixture, Assembly/Disassembly - HPT Rotor (assembly/disassembly fixture)
 
11C3032G02
Retainer, Blade - Slave HPTR Stg 1 (slave blade retainer)
 
11C3033G01
Deleted
 
11C3034G01
Heater, Disk Stage 2 - HPT Rotor (120 VAC, 60 Hz) (heater)
 
11C3034G02
Heather, Disk Stage 2 - HPT Rotor (230 VAC, 50 Hz) (heater)
 
11C3037G01
Protector - HPT Rotor Assembly (HPTR protector)
 
11C3037G02
Protector - HPT Rotor Assembly (HPTR protector)
NOTE:
Tool 11C3037G02 is used as an alternative to 11C3037G01.
 
11C3041G02
Fixture, Clamping - HPT Rotor Blade, Stage 1 (clamp fixture)
 
11C3043G01
Fixture, Chill - HPT Rotor Stage 1 (chill fixture)
 
11C3056G01
Fixture, HPT Rotor Aft Lift (lift fixture)
NOTE:
Tool 11C3056G01 is an alternative to 11C3056G02.
 
11C3056G02
Fixture, HPT Rotor Aft Lift (lift fixture)
NOTE:
Tool 11C3056G02 is an alternative to 11C3056G01.
 
11C3060G02
Fixture, Lift/Turn - HPC Rotor Aft/HPT Rotor Forward (lift/turn fixture)
 
11C3068G01
Fixture, Install/Remove - Shank Nut, HPT Rotor Stage 2
 
11C3137G03
Fixture, Tip Notch HPT Stage 1 Rotor Blade (fixture)
 
11C3137G04
Fixture, Tip Notch HPT Stage 2 Rotor Blade (fixture)
 
11C3354G03
Fixture, Install - Stage 1 Blade Retainer (install/remove fixture)
 
11C3413G01
Fixture, Restrain - HPT Rotor Blades Stage 1 (stage 1 restrain fixture)
 
11C3413G02
Fixture, Restrain - HPT Rotor Blades Stage 2 (stage 2 restrain fixture)
 
11C3438G01
Fixture, Lift/Turn
 
11C4285P01
Adapter, Balance - HPT Rotor (balance adapter)
 
11C4537G01
Fixture, Horizontal - Transport Dolly HPT Rotor (horizontal transport dolly)
 
11C4554G01
Arbor, HPT Rotor Balance (balance arbor) (alternate to 11C3438G01. Use with 11C4558G01 lift fixture)
 
11C4556G01
Adapter, Drive - Balance, HPT Rotor (balance adapter)
NOTE:
Tool 11C4556G01 is alternative to 11C3012G02 and 11C4622G01.
 
11C4558G01
Fixture, Lift/Turn - Balance Arbor HPT Rotor (lift fixture) (alternate to 11C4285P01. Use with 11C4554G01 balance arbor)
 
11C4617P01
Heater, Induction - HPT Rotor (induction heater fixture)
NOTE:
Tool 11C4617P01 is alternative to 11C3021G02.
 
11C4622G01
Puller - Grind Arbor, Aft (puller)
NOTE:
Tool 11C4622G01 is alternative to 11C4556G01 that depends on the balance machine manufacturer.
 
11C4626P01
Blanket, Insulation - Stage 1 HPTR Disk (insulation blanket) (used with tool 11C3021)
 
11C4676G01
Container, Shipping - HPT Rotor Assembly (shipping container)
 
11C4697P01
Heater, Induction - HPT Rotor
NOTE:
Tool 11C4697P01 is an alternative to 11C4617P01.
 
11C4808G01
Blanket, Insulation - Stage 1 HPTR Disk (insulation blanket) (used with tool 11C3021)
 
9429M14G02
Fixture, Lift Arm - Standard (lift arm)
 
9429M57G03
Dolly, Transport - HPT Rotor, Vertical (dolly) (part of tool 11C3018)
 
9446M18P01
Controller, Heater-Resistive Element (controller)
 
9446M91G01
Deleted
 
9471M13P03
Inspection System - Rotor Components/ Assembly (inspection system)
 
9471M16P01
Supply, Power (used with tool 11C4697P01)
(2)Standard Tools and Equipment.
 
Description
Manufacturer
 
Advance Hydraulic Wrench AH-2543 (hydraulic wrench)
Advance Manufacturing Company Turnpike Industrial Park Westfield, MA 01085
 
Heat Tape (115V), P/N FRE161006 (heat tape (115V))
BH Thermal Corp. 1055 Gibbard Ave. Columbus, OH 43201 USA
 
Heat Tape (220V), P/N FRE162006 (heat tape (220V))
BH Thermal Corp. 1055 Gibbard Ave. Columbus, OH 43201 USA
 
Multiplier, No. 4600-268A (multiplier)
Local Purchase
 
PA-133R Air-Hydraulic Pump
Local Purchase
 
Rubber Bands
Local Purchase
 
Shim Stocks (0.011 inch (0.28 mm) and 0.010 inch (0.25 mm) thick)
Local Purchase
 
Sling, Three-Legged (three-legged sling)
Local Purchase
 
Sweeney Anchor Plate (23480-4)
B.K. Sweeney Company 6300 Stapleton South Drive Denver, CO 80216
 
Sweeney No. 8100 Torque Multiplier (torque multiplier)
B.K. Sweeney Company 6300 Stapleton South Drive Denver, CO 80216
 
Sweeney No. 8111 Torque Multiplier (torque multiplier)
B.K. Sweeney Company 6300 Stapleton South Drive Denver, CO 80216
 
Sweeney No. 8112 Torque Multiplier (torque multiplier)
B.K. Sweeney Company 6300 Stapleton South Drive Denver, CO 80216
(3)Locally Manufactured Tools. None.
B.Consumable Materials.
 
Code No.
Description
 
C01-027
Adhesive, Synthetic (synthetic adhesive)
 
C01-037
Adhesive, Synthetic (synthetic adhesive)
 
C01-050
Adhesive, Rubber (Fed. Spec. MMM-A-00185) (rubber cement)
 
C02-019
Oil, Engine Lubricating (engine oil)
 
C02-023
Oil, Engine Lubricating (engine oil)
 
C02-033
Petrolatum, Soft (lubricant)
 
C02-058
Compound, Thread Lubricating (lubricant)
 
C04-002
Solvent, General (Stoddard solvent)
 
C04-035
Solvent, General (isopropyl alcohol)
 
C04-036
Solvent, General (toluene)
 
C05-002
Ink, Marking (marking ink)
 
C05-003
Marking Pen
 
C10-012
Tape, Masking, High Temperature (tape)
 
C10-021
Tape, Plastic (tape)
 
C10-108
Brush, Disposable, Natural Bristle (brush)
 
C10-182
Cloth, Cleaning For Aircraft Structural (SAE-AMS 3819, BMS 15-5) (lint free cloth)
 
Dry Ice
Local Purchase
 
Liquid Nitrogen
Local Purchase
C.Referenced Procedures.
 
ATA No.
Description
 
70-16-02
Temporary Marking
 
70-42-00
Blending and Removal of High Metal Procedures
 
72-00-53
Inspection 001 - Configuration 01
 
72-50-00
Assembly 001
 
72-52-00
Assembly 001
D.Expendable Parts.
 
CSN
Description
 
01-010
Bolt - Machine THD CDP Seal (CDP bolt)
 
01-020
Bolt - Machine THD CDP Seal (CDP balance bolt)
 
01-040
Bolt - Machine
 
01-100
Nut, Self-Locking (shank nut)
 
01-220
Damper, Stage 1
3 . Procedure.
Subtask 72-53-00-220-055
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
WARNING:
TOLUENE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
A.Clean the areas where the HPT rotor stage 1 disk (stage 1 disk) (150A1) will touch the 11C3024   assembly/disassembly fixture, with a 50/50 blend of C04-035  isopropyl alcohol and C04-036  toluene.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1001   (Sheet 1 ) HPT Rotor Assembly
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1001   (Sheet 2 ) HPT Rotor Assembly
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1001   (Sheet 3 ) HPT Rotor Assembly
Subtask 72-53-00-220-110
B.Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1002   Install the Stage 1 HPTR on the Support Fixture, 11C3008
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1003   Measurement of the Stage 1 HPT Rotor Runout
Subtask 72-53-00-220-117
(4)Deleted.
(5)Deleted.
(6)Deleted.
(7)Deleted.
(8)Deleted.
Subtask 72-53-00-220-056
C.Make sure that the 11C3024   assembly/disassembly fixture does not have any high metal. Blend as necessary. Refer to TASK 70-42-00-350-002 (BLENDING AND REMOVAL OF HIGH METAL PROCEDURES).
Subtask 72-53-00-440-284
D.Install the 11C3021   heater fixture on the 11C3024   assembly/disassembly fixture.
NOTE:
It is not necessary to install the 11C3021   heater fixture when the stage 1 disk (01-280) (SIN 150A1) is heated with the 11C4617   induction heater fixture.
Subtask 72-53-00-440-143
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
E.Prepare the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1004.
(1)Remove the shaft adapter (item 7) as follows.
(a)Loosen and remove the stress ring (item 6).
(b)Loosen and remove the setscrews (item 15).
(c)Loosen the ring (item 4) to disengage it from the shaft base (item 5).
(d)Loosen the shaft adapter (item 7).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(e)Attach an overhead hoist to the hoist (item 9) to remove the shaft adapter (item 7) and the ring (item 4) from the shaft base (item 5).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1004   (Sheet 1 ) Removal of the Ring and the Shaft Adapter from the Assembly/Disassembly Fixture, 11C3024
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1004   (Sheet 2 ) Removal of the Ring and the Shaft Adapter from the Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-144
(2)Install the disk bore protector (item 10) on the end of the shaft base (item 5) of the 11C3024   assembly/disassembly fixture. Refer to Figure 1005.
NOTE:
The 11C3021   heater fixture consists of a G01 and a G02. The G01 is for 120 VAC/60 Hz and the G02 is for 240 VAC/50 Hz.
(3)Install the heat element (item 5 or item 6) and the temperature bayonet mount (item 7) on the 11C3021   heater fixture on the tray (item 2).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1005   Installation of the Protector on the Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-145
F.Install the 11C3056   lift fixture as follows. Refer to Figure 1006.
CAUTION:
DO NOT TIGHTEN THE 11C3056 LIFT FIXTURE TOO MUCH. DAMAGE TO THE STAGE 1 DISK THREADS AND TOOLING CAN OCCUR.
(1)Attach the 11C3056   lift fixture to the threads on the aft end of the stage 1 disk (150A1). Turn clockwise (CW), looking forward (ALF), until the 11C3056   lift fixture is fully engaged on the HPT rotor shaft.
(2)Attach an overhead hoist to the 11C3056   lift fixture.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1006   Installation of the Lift Fixture, 11C3056, and the Retaining Segments of the Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-146
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
G.Attach the stage 1 disk (150A1) to the 11C3024   assembly/disassembly fixture as follows:
  (1)Deleted.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(2)Lift the stage 1 disk and install the retaining ring segments (item 24) on the aft face of the forward flange. Refer to Figure 1006.
(3)Install the tray (item 2) and post (item 3) of the 11C3021   heater fixture onto the 11C3024   assembly/disassembly fixture. Refer to Figure 1004.
(4)Apply C02-058  lubricant to the threads of the nuts (item 14) and the faces of the washers (item 20).
(5)Install a washer (item 20) and a nut (item 14) on each of the four short studs of the retaining rings (item 24).
(6)Torque the nuts (item 14) to 276-324 lb in. (31-37 N.m).
(7)Align the four short studs with the large holes in the base (item 21). Refer to Figure 1007.
(8)Lower the stage 1 disk and attach the forward flange to the 11C3024   assembly/disassembly fixture as follows:
(a)Apply C02-058  lubricant with a C10-108  brush to the threads of the retaining rings (item 24), the faces of the washers (item 20), and the nuts (item 14).
(b)Attach 12 washers (item 20) and 12 nuts (item 14) to the studs of the retaining rings (item 24).
(c)Torque the nuts (item 14) to 276-324 lb in. (31-37 N.m) in a crisscross pattern. Continue this procedure until all of the nuts are tight.
(9)Remove the 11C3056   lift fixture. Refer to Figure 1006.
(10)Use a C05-003  marking pen to mark in a clockwise (CW) direction aft looking forward (ALF) of the stage 1 disk the position of the 1-1 and 5-5 disk post. Refer to Figure 1008.
(11)Use a C05-003  marking pen to remark the X stamped from vendor on the aft shaft of the stage 1 disk.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1007   Installation of the Stage 1 Disk on the Assembly/Disassembly Fixture, 11C3024
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1008   Marking of the Stage 1 Disk
Subtask 72-53-00-440-285
H.Alternative Procedure Available. Heat the stage 1 disk (01-280) (SIN 150A1) with the 11C3021   heater fixture. Refer to Figure 1009 and do as follows:
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(1)Connect the 9446M18   controller.
  (2)Install the 11C4626   insulation blanket or 11C4808   insulation blanket. Refer to Figure 1009.
CAUTION:
MAKE SURE THE STAGE 1 DISK TEMPERATURE IS NOT MORE THAN 700°F (371°C) OR THE STAGE 1 DISK CAN BE DAMAGED.
(3)Heat the stage 1 disk (150A1) at the rabbet to 500°F (260°C) with a maximum temperature of 700°F (371°C). Check with a calibrated temperature probe to make sure that the temperature is not more than the maximum limit.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1009   Installation of the Heater Shroud, 11C3021
Subtask 72-53-00-440-515
H.A.Alternative Procedure. Heat the stage 1 disk (01-280) (SIN 150A1) with or without the aft stage 1 blade retainer (01-180) (SIN 150BB) with the 11C4617   induction heater fixture. Refer to Figure 1010 and do as follows:
(1)Install the 11C4617   induction heater fixture on the stage 1 disk (01-280) (SIN 150A1) as follows:
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
MAKE SURE THAT THE STAGE 1 DISK TEMPERATURE IS NOT MORE THAN 700°F (371°C) OR DAMAGE TO THE STAGE 1 DISK CAN OCCUR.
(a)Install the induction coil assembly and locating assembly on the stage 1 disk (01-280) (SIN 150A1).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift and lower the 11C4617   induction heater fixture on the stage 1 disk (01-280) (SIN 150A1) with a hoist. Make sure that the induction coil assembly is aligned with stage 1 disk (01-280) (SIN 150A1) while lowering it.
CAUTION:
MAKE SURE THAT THE THERMOCOUPLE MAKES CONTACT WITH THE SURFACE OF THE STAGE 1 DISK. CONTACT BETWEEN THERMOCOUPLE AND STAGE 1 DISK IS VERY IMPORTANT TO OPERATION.
(c)Attach the thermocouple with the thermocouple holder on the forward side of the stage 1 disk (01-280) (SIN 150A1) approximately 0.75-1.00 inch (19.1-25.4 mm) inboard from the outer rim.
(d)Turn the power switch to the “ON” position.
(e)Press the “Load Circuit” button on the touch screen after the Eldec MICO 50kW medium frequency with programmable controller starts.
(f)After the “Load Circuit” button changes color to green, press the “Heating” button on the touch screen to display the heating parameter window.
(g)Press the “Heating On/Off” button to start the heat cycle. Record the stage 1 disk (01-280) (SIN 150A1) temperature that will be displayed on the screen.
NOTE:
The heat cycle will continue approximately 6 minutes and will stop automatically.
(h)Remove the 11C4617   induction heater fixture from the stage 1 disk (01-280) (SIN 150A1) with a hoist.
(i)With a handheld thermocouple measure the aft surface of the stage 1 disk (01-280) (SIN 150A1) approximately 0.75-1.00 inch (19.1-25.4 mm) inboard from outer rim. Record the temperature.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1010   (Sheet 1 ) Installation of the Induction Heater Fixture, 11C4617
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1010   (Sheet 2 ) Installation of the Induction Heater Fixture, 11C4617
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1010   (Sheet 3 ) Installation of the Induction Heater Fixture, 11C4617
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1010   (Sheet 4 ) Installation of the Induction Heater Fixture, 11C4617
Subtask 72-53-00-440-302
I.Install the ring seal (150N2) into the groove on the stage 1 blade retainer (150BB) as follows. Refer to Figure 1011.
(1)Put the stage 1 blade retainer (150BB), forward end up, on a work table.
(2)Cut four ring seal segments to 20.0 inches (508 mm) in length.
(3)Use a file to remove unwanted material from the ends of the ring seal segments. Make sure that there are no burrs on the segments.
(4)Put a ring seal segment into the groove in the forward face of the stage 1 blade retainer. Apply C10-012   tape to hold it in position. Then, install the next segment. Keep an end gap of 0.100-0.140 inch (2.54-3.56 mm).
(5)Repeat this procedure until all four of the ring seal segments are installed. Cut the segments as necessary to keep an end gap of 0.100-0.140 inch (2.54-3.56 mm).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1011   Installation of the Ring Seal in the Stage 1 Blade Retainer
Subtask 72-53-00-220-123
(6)Measure the distances between the ends of the ring seal segments as follows:
(a)If the distance is more than 0.140 inch (3.56 mm), install a new ring seal segment.
(b)If the distance is less than 0.100 inch (2.54 mm), remove a part of the ring seal segment.
(7)Remove the C10-012  tape and the ring seal segments from the blade retainer.
WARNING:
SYNTHETIC ADHESIVE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(8)Apply small amounts of C01-027  synthetic adhesive or C01-037  synthetic adhesive into the groove in the aft face of the stage 1 blade retainer (01-180) (SIN 150BB).
(9)Allow the adhesive to cure for 15-20 minutes until it is tacky.
NOTE:
The adhesive may be heat cured, but do not exceed 250° F (121° C).
(10)Install the ring seal segments into the groove in the forward face of the stage 1 blade retainer (150BB).
(11)Make sure that the ring seal segments are fully in the groove of the blade retainer.
(12)Measure the distances between the ends of the ring seal segments to make sure that they are 0.100-0.140 inch (2.54-3.56 mm).
Subtask 72-53-00-440-287
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
J.Install the stage 1 blade retainer (150BB) on the stage 1 disk (150A1) with the 11C3354   install/remove fixture as follows. Refer to Figure 1015.
WARNING:
DELETED.
WARNING:
DELETED.
(1)Deleted.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(2)Attach an overhead hoist to the hoist (item 9) of the 11C3024   assembly/disassembly fixture. Refer to Figure 1004.
(3)Use an overhead hoist and lower the adapter shaft (item 7) and install it on the stage 1 disk.
(4)Attach an overhead hoist to the 11C3354   install/remove fixture and move it over the stage 1 disk and prepare to install it.
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(5)Put liquid nitrogen on the stage 1 blade retainer (01-180) (SIN 150BB) and let it sit for 1 minute. Chill the stage 1 blade retainer with dry ice for 25 minutes as an alternative to liquid nitrogen.
(6)Install the stage 1 blade retainer (150BB) it on the aft side of the stage 1 disk by hand.
(7)Quickly lower and install the 11C3354   install/remove fixture on the stage 1 blade retainer (150BB).
(a)Install the push ring (item 21) onto the adapter shaft (item 7) of the 11C3024   assembly/disassembly fixture.
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE MORE PRESSURE THAN THE MAXIMUM HYDRAULIC PRESSURE. STAY AWAY FROM THE AREA BEHIND OR IN FRONT OF THE PUSHER/PULLER. A MALFUNCTION CAN CAUSE INJURY OR CAN KILL YOU.
(b)Apply 1000 psi (6895 Kpa) of hydraulic pressure into the actuator.
(8)Deleted.
(9)Remove the 11C3354   install/remove fixture as follows. Refer to Figure 1022.
Subtask 72-53-00-220-111
(10)Do a visual inspection with mirror and flashlight and make sure that the segments of the ring seal (150N2) are in the correct groove.
Subtask 72-53-00-440-288
(11)Install the disk bore protector (item 10) of the 11C3024   assembly/disassembly fixture. Refer to Figure 1005.
Subtask 72-53-00-220-222
(12)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1012.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1012   Critical Areas of the Stage 1 Disk Aft Shaft to Inspect the After Stage 1 Blade Retainer Installation
Subtask 72-53-00-440-152
K.Lubricate the interstage seal (150B3) and the stage 1 disk (150A1) as follows:
(1)Apply C02-033  lubricant to the surfaces of the interstage seal that will touch the stage 1 disk (150A1). Refer to the areas labeled X in Figure 1014.
(2)Turn the interstage seal and put it, aft end up, on a work table.
(3)Apply C02-033  lubricant to the surfaces of the stage 1 disk that will touch the interstage seal. Refer to the areas labeled X in Figure 1014.
(4)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1013   Prepare the Stage 1 Disk to Install the Interstage Seal
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1014   Prepare the Stage 1 Disk to Install the Interstage Seal
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1015   (Sheet 1 ) Install/Remove Fixture, 11C3354
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1015   (Sheet 2 ) Install/Remove Fixture, 11C3354
Subtask 72-53-00-440-153
L.Alternative Procedure Available. Increase the temperature of the stage 1 disk (01-280) (SIN 150A1) as follows:
  (1)Use the 11C3021   heater fixture and 11C4626   insulation blanket or 11C4808   insulation blanket to apply heat to the stage 1 disk.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
MAKE SURE THE STAGE 1 DISK TEMPERATURE IS NOT MORE THAN 700°F (371°C) OR THE STAGE 1 DISK CAN BE DAMAGED.
(2)Apply heat until the temperature of the stage 1 disk rabbet and retainer is 500°F (260°C). Measure the temperature with a calibrated temperature probe. Make sure that the temperature does not exceed 700°F (371°C) as maximum.
Subtask 72-53-00-440-516
L.A.Alternative Procedure. Heat the stage 1 disk (01-280) (SIN 150A1) with the aft stage 1 blade retainer (01-180) (SIN 150BB) with the 11C4617   induction heater fixture. Refer to Figure 1010 and do as follows:
(1)Install the 11C4617   induction heater fixture on the stage 1 disk (01-280) (SIN 150A1) as follows:
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
MAKE SURE THAT THE STAGE 1 DISK TEMPERATURE IS NOT MORE THAN 700°F (371°C) OR DAMAGE TO THE STAGE 1 DISK CAN OCCUR.
(a)Install the induction coil assembly and locating assembly on the stage 1 disk (01-280) (SIN 150A1).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift and lower the 11C4617   induction heater fixture on the stage 1 disk (01-280) (SIN 150A1) with a hoist. Make sure that the induction coil assembly is aligned with stage 1 disk (01-280) (SIN 150A1) while lowering it.
CAUTION:
MAKE SURE THAT THE THERMOCOUPLE MAKES CONTACT WITH THE SURFACE OF THE STAGE 1 DISK. CONTACT BETWEEN THERMOCOUPLE AND STAGE 1 DISK IS VERY IMPORTANT TO OPERATION.
(c)Attach the thermocouple with the thermocouple holder on the forward side of the stage 1 disk (01-280) (SIN 150A1) approximately 0.75-1.00 inch (19.1-25.4 mm) inboard from the outer rim.
(d)Turn the power switch to the “ON” position.
(e)Press the “Load Circuit” button on the touch screen after the Eldec MICO 50kW medium frequency with programmable controller starts.
(f)After the “Load Circuit” button changes color to green, press the “Heating” button on the touch screen to display the heating parameter window.
(g)Press the “Heating On/Off” button to start the heat cycle. Record the stage 1 disk (01-280) (SIN 150A1) temperature that will be displayed on the screen.
NOTE:
The heat cycle will continue approximately 6 minutes and will stop automatically.
(h)Remove the 11C4617   induction heater fixture from the stage 1 disk (01-280) (SIN 150A1) with a hoist.
(i)With a handheld thermocouple measure the aft surface of the stage 1 disk (01-280) (SIN 150A1) approximately 0.75-1.00 inch (19.1-25.4 mm) inboard from outer rim. Record the temperature.
Subtask 72-53-00-440-154
M.Attach the locator (item 2) and the clamp (item 3) of the 11C3006   install/remove fixture to the interstage seal (150B3) as follows. Refer to Figure 1017.
(1)Align the locator (item 2) on the interstage seal with the tabs down.
(2)Make sure that the tabs on the forward side of the locator (item 2) engage the air crossover holes on the interstage seal.
(3)Remove the capscrews (item 36) to disconnect the clamp (item 3) halves.
(4)Put the clamp (item 3) in position on the interstage seal with the rim in the slot.
(5)Install the capscrews (item 36) to connect the clamp (item 3) halves. Tighten the capscrews (item 36).
(6)Install the lifting pins (item 27) in the clamp (item 3).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1016   Chilling the HPT Rotor Interstage Seal with the 7C2141 Chill Fixture.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1017   Installation of the Locator and the Clamp Ring of the Install/Remove Fixture, 11C3006, on the Interstage Seal
Subtask 72-53-00-440-155
N.Decrease the temperature of the interstage seal (150B3) as follows:
Subtask 72-53-00-440-308
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
(1)Alternative Procedure Available. Put the interstage seal, aft side up, in dry ice for 30 minutes with the 7C2141   dam chill fixture. Refer to Figure 1016.
Subtask 72-53-00-440-309
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURER’S (MATERIAL) SAFETY DATA SHEET FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF THIS PRODUCT.
(1).A.Alternative Procedure. Apply liquid nitrogen around the forward outer rim of the interstage seal to decrease the temperature with the 7C2141   dam chill fixture. Refer to Figure 1016.
NOTE:
When the interstage seal is cold, the installation must be completed in a maximum of 1 minute.
Subtask 72-53-00-440-156
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
O.Attach the interstage seal (150B3) to the stage 1 disk (150A1) as follows. Refer to Figure 1018.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(1)Attach a lift hoist to the lifting pins (item 27) of the 11C3006   install/remove fixture.
(2)Put the interstage seal on the stage 1 disk as follows:
(a)Make sure that the 31 slots in the inner bore of the interstage seal are aligned with the 32 tabs on the stage 1 disk.
(3)Lower interstage seal onto stage 1 HPT disk
(4)Rotate interstage seal by hand by pushing on torque blocks until seated with orientation gauge.
(5)If seal does not rotate by hand, attach 2 breaker bars to torque blocks and rotate interstage seal.
(6)If seal still does not rotate lift interstage seal off stage 1 disk using hoist do as follows:
(a)Repeat Subtask 72-53-00-440-155 (paragraph 3.N.).
(b)If this process has been tried twice without seal installation go to Subtask 72-53-00-440-156 (paragraph 3.O.).
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(7)Try to manually put the interstage seal in the correct position as follows:
(a)Attach two breaker bars to the torque blocks (item 18) of the 11C3006   install/remove fixture. Refer to Figure 1019.
(b)Install the pusher (item 22).
(c)Install the nut (item 7).
(d)Use the breaker bars to lock the interstage seal until the tabs align and the 7C2068   orientation gage fits in the inner diameter slot at the base of the interstage seal and the stage 1 disk.
(e)If the interstage seal will not turn. Refer to Subtask 72-53-00-440-156 (paragraph 3.O.(9)).
(f)If the interstage seal rabbets have engaged the stage 1 disk and the tabs are not aligned. Refer to Subtask 72-53-00-440-156 (paragraph 3.O.(9)).
(g)When the interstage seal is installed, do the steps that follow:
1Remove the capscrews (item 36) and the clamp (item 3) halves of the 11C3006   install/remove fixture.
2Remove the lifting pins (item 27) from the clamp (item 3) and install them in the locator (item 2).
3Remove the locator (item 2) from the interstage seal.
4Refer to Subtask 72-53-00-220-064 (paragraph (3.P.) to continue this procedure.
(8)Remove the lift hoist from the lifting pins (item 27).
(9)Turn the interstage seal (150B3) until the 7C2068   orientation gage fits. Refer to Figure 1018.
(10)Remove the disk bore protector (item 10) of the 11C3024   assembly/disassembly fixture from the end of the shaft base (item 5).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1018   Installation of the Install/Remove Fixture, 11C3024 and the Orientation Gage, 7C2068
Subtask 72-53-00-440-160
(11)Install the shaft adapter (item 7) on the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1004.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(a)Attach an overhead hoist to the hoist (item 9) to lift the shaft adapter (item 7) and install it on the shaft base (item 5).
(b)Tighten the shaft adapter (item 7).
(c)Engage and tighten the ring (item 4).
(d)Install and tighten the setscrews (item 15).
(e)Install and tighten the stress ring (item 6).
(f)Remove the quick release pin (item 11).
(g)Remove the hoist (item 9).
(12)Attach the collar (item 17) and the pusher (item 5) of the 11C3006   install/remove fixture to the stage 1 disk (150A1) and the interstage seal (150B3) as follows. Refer to Figure 1020.
(a)Install the collar (item 17) as follows:
1Put the collar (item 17) on the aft surface of the interstage seal against the hub face and ID bayonet.
2Engage the two tabs on the collar (item 17) with the two wide slots in the interstage seal.
3Make sure that the four slots on the collar (item 17) and the interstage seal are aligned.
(b)Install the pusher (item 22) on the collar (item 17). Make sure that the slot in the aft end of the pusher (item 22) is aligned with the 1-1 slot on the stage 1 disk shaft. Refer to Figure 1021.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1019   Installation of the Inner Stage Seal, 11C3006
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1020   Installation of the Collar, Pusher, and Locating Ring
Subtask 72-53-00-440-162
(13)Install the locating ring (item 6) as follows:
(a)Put the locating ring (item 6) above the shaft adapter (item 7) of the 11C3024   assembly/disassembly fixture with the tab down.
(b)Align the tab in the locating ring (item 6) of the 11C3024   install/remove fixture with the slot in the pusher (item 5).
(c)Lower the locating ring (item 6) into position so that the tab engages the 1-1 slot on the stage 1 disk shaft. Adjust the position of the pusher (item 5) as necessary to correctly engage the tab of the locating ring (item 6) in the 1-1 slot.
(14)Install the nut (item 7) as follows. Refer to Figure 1021.
(a)Engage the internal threads of the nut (item 7) of the 11C3006   install/remove fixture on the external threads of the stress ring (item 6) of the 11C3024   assembly/disassembly fixture.
CAUTION:
DO NOT TIGHTEN THE NUT (ITEM 7) TOO MUCH. DAMAGE TO THE STAGE 1 DISK SHAFT AND TOOLING CAN OCCUR.
(b)Tighten the nut (item 7) of the 11C3006   install/remove fixture only until the locating ring (item 6) cannot move. Do not tighten the nut (item 7) more than necessary.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1021   Installation of the Nut and Retainer Nut
Subtask 72-53-00-210-004
(c)Look through the slot in the pusher (item 5) to make sure that the locating ring (item 6) is in the correct position with the tab engaged in the 1-1 slot of the HPT rotor shaft.
Subtask 72-53-00-440-164
(15)Install the retainer nut (item 8) as follows:
(a)Put the retainer nut (item 8) in position with the large diameter down.
(b)Engage the internal threads of the retainer nut (item 8) on the external threads of the stress ring (item 6) of the 11C3024   assembly/disassembly fixture. Use the spanner wrench (item 14) of the 11C3006   install/remove fixture.
Subtask 72-53-00-220-060
(16)Look through the view holes of the pusher (item 22) of the 11C3006   install/remove fixture to examine the position of the pusher (item 22 in relation to the shoulder of the stage 1 disk (150A1) as follows:
(a)Make sure that there is no space between the stop on the pusher (item 22) and the shoulder on the aft shaft of the stage 1 disk as follows. Refer to Figure 1021.
1If there is no space, then tighten the retainer nut (item 8) against the pusher (item 22) with the spanner wrench (item 14).
2If there is a space, then tighten the retainer nut (item 8) to move the pusher (item 22) until the space is gone. Use the spanner wrench (item 14) to apply torque.
3If too much torque is necessary to close the space, then do as follows. Refer to Figure 1022.
aPut the spanner wrench (item 14) into position in the ring (item 15).
bPut the ring (item 15) on the aft surface of the pusher (item 22).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
cUse a three-legged sling and overhead hoist to lift the pusher plate/cylinder assembly.
NOTE:
The pusher plate/cylinder assembly includes the pusher plate (item 10), extension (item 11), end rod (item 12), nut (item 13), hydraulic cylinder (item 29), female coupling (item 30), and spherical washer (item 31).
dLower the pusher plate/cylinder assembly down to the ring (item 15) as you engage the end rod (item 12) of the 11C3006   install/remove fixture to the shaft adapter (item 7) of the 11C3024   assembly/disassembly fixture.
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE MORE THAN MORE THAN THE MAXIMUM HYDRAULIC PRESSURE. STAY AWAY FROM THE AREA BEHIND OR IN FRONT OF THE PUSHER/PULLER. A MALFUNCTION CAN CAUSE INJURY OR CAN KILL YOU.
CAUTION:
DO NOT APPLY MORE THAN 10000 PSI (68948 KPA) OF PRESSURE. TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE INTERSTAGE SEAL.
eAttach a hydraulic pressure source to the female coupling (item 30) of the hydraulic cylinder (item 29) and slowly apply pressure until the bore of the interstage seal is in position.
fMake sure that the pins on the spanner wrench (item 14) engage the holes in the retainer nut (item 8).
gTighten the retainer nut (item 8) to keep the assembly in position.
hRemove the pusher plate/cylinder assembly, the ring (item 15), and the spanner wrench (item 14).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1022   Installation of the Interstage Seal Against the Stage 1 Disk
Subtask 72-53-00-440-168
(17)Install the housing (item 4) as follows. Refer to Figure 1023.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(a)Attach a sling and an overhead hoist to the hoist rings (item 32) to lift the housing (item 4).
CAUTION:
MAKE SURE THAT THE TOP VERTICAL CENTERLINES OF THE HOUSING AND THE CLAMP ARE CORRECTLY ALIGNED BEFORE YOU LOWER THE HOUSING. DAMAGE TO THE ENGINE HARDWARE CAN OCCUR.
(b)Align the top vertical centerline on the housing (item 4) with the top vertical centerline on the clamp (item 3).
(c)Lower the housing (item 4) until it is approximately 1.00 inch (25,4 mm) above the surface of the interstage seal.
(d)Look through the view holes in the housing (item 4) and find the scribe line on the locating ring (item 6).
(e)Make sure that the scribe line on the locating ring (item 6) is aligned with the DISENGAGED mark on the housing (item 4).
(f)Lower the housing (item 4) so that the dowel pins (item 26) engage the related holes in the clamp (item 3) and locator (item 2). Adjust the position of the housing (item 4) as necessary to align the dowel pins (item 26), but keep the scribe lines aligned.
(g)Install the capscrews (item 19) to attach the housing (item 4) to the clamp (item 3) and locator (item 2).
(h)Torque the capscrews (item 19) to 5-10 lb ft (7-14 N.m).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1023   Installation of the Housing of the Install/Remove Fixture, 11C3006
Subtask 72-53-00-440-169
(18)Install the Sweeney-8100torque multiplier as follows. Refer to Figure 1024.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(a)Use an overhead hoist to lift the Sweeney-8100torque multiplier.
(b)Install the Sweeney-8100torque multiplier on the splined drive (item 9) of the 11C3006   install/remove fixture.
(c)Install the anti torque plate (item 21) of the 11C3006   install/remove tool to hold the Sweeney-8100torque multiplier in position.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1024   Installation of the Torque Multiplier on the Install/Remove Fixture, 11C3006
Subtask 72-53-00-220-061
(19)Visually examine the position of the housing (item 4) in relation to the pusher (item 5) as follows. Refer to Figure 1023.
(a)Look through the holes in the housing (item 4) to see if there is a space between the aft surface of the pusher (item 5) and the forward surface of the upper plate on the housing (item 4).
Subtask 72-53-00-440-170
(b)If there is no space, then the pusher plate/cylinder assembly is not necessary. Refer to Subtask 72-53-00-440-170 (paragraph 3.O.(20)) to continue this procedure.
(c)If there is a space, then use the pusher plate/cylinder assembly to continue this procedure. Refer to Subtask 72-53-00-440-170 (paragraph 3.O.(20)).
(20)Attach the pusher plate/cylinder assembly to the housing (item 4) and the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1025.
NOTE:
The pusher plate/cylinder assembly includes the pusher plate (item 10), extension (item 11), end rod (item 12), nut (item 13), hydraulic cylinder (item 29), female coupling (item 30), and spherical washer (item 31).
(a)Lower the pusher plate/cylinder assembly to the housing as you engage the end rod (item 12) of the 11C3006   install/remove fixture in the shaft adapter (item 7) of the 11C3024   assembly/disassembly fixture.
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE MORE THAN MORE THAN THE MAXIMUM HYDRAULIC PRESSURE. STAY AWAY FROM THE AREA BEHIND OR IN FRONT OF THE PUSHER/PULLER. A MALFUNCTION CAN CAUSE INJURY OR CAN KILL YOU.
CAUTION:
DO NOT APPLY MORE THAN 10000 PSI (68948 KPA) OF PRESSURE. YOU CAN CAUSE DAMAGE TO THE TOOL OR HARDWARE.
(b)Attach a hydraulic pressure source to the female coupling (item 30) of the hydraulic cylinder (item 29) on the 11C3006   install/remove fixture. Operate the hydraulic cylinder (item 29) to put the housing (item 4) in the correct position.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1025   Installation of the Pusher Plate/Cylinder Assembly of the Install/Remove Fixture, 11C3006
Subtask 72-53-00-220-062
(c)Measure the space between the housing (item 4) and the pusher (item 22) with a 0.001 inch (0.03 mm) shim. Do this through the slots on the top of the splined drive (item 9).
(21)Do a visual inspection of the alignment marks as follows:
(a)Make sure that the scribe line in the locator ring (item 6) is aligned with the DISENGAGED mark on the housing (item 4).
Subtask 72-53-00-440-173
(b)If the marks are aligned, go to Subtask 72-53-00-440-170 (paragraph (3.O.(21)) to continue this procedure.
(c)If the marks are not aligned, disassemble the 11C3006   install/remove fixture and install it again. Refer to Subtask 72-53-00-440-156 (paragraph 3.O.(9)).
(22)Engage the interstage seal as follows:
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
(a)Put liquid nitrogen or dry ice on the aft side of the forward lip of the interstage seal.
(b)Turn the Sweeney-8100torque multiplier clockwise (CW) until the pin of the locating ring (item 6) is aligned with the ENGAGED mark on the housing (item 4).
CAUTION:
DO NOT TORQUE MORE THAN 11000 LB FT (14914 N.M). YOU CAN CAUSE DAMAGE TO THE TOOL OR HARDWARE.
(c)Adjust as necessary until the 7C2068   orientation gage fits in an inner diameter slot at the base of the pusher (item 22) of the 11C3006   install/remove fixture. Refer to Figure 1018 and Figure 1025.
CAUTION:
DO NOT MOVE ANY TOOLS WHILE THE DISK AND INTERSTAGE SEAL BECOME STABLE. DAMAGE TO THE SEAL CAN OCCUR.
(d)Let the temperature of the assembly stabilize for 30 minutes.
Subtask 72-53-00-210-005
(23)Make sure that the ring seal (150N2) is correctly installed in the groove.
NOTE:
Segments cannot be pushed into the groove after the install/remove fixture, 11C3006 has been removed, unless the interstage seal is removed and installed again.
Subtask 72-53-00-440-176
(24)Remove the 11C3006   install/remove fixture from the interstage seal as follows:
(a)Release the pressure from the hydraulic cylinder (item 29). Refer to Figure 1025.
(b)Turn and disengage the end rod (item 12) of the 11C3006   install/remove fixture from the shaft adapter (item 7) of the 11C3024   assembly/disassembly fixture.
(c)Attach an overhead hoist to the hoist rings (item 32) of the 11C3006   install/remove fixture on the pusher plate (item 10) and remove the pusher plate/cylinder assembly from the housing (item 4).
(d)Remove the anti torque plate (item 21) of the 11C3006   install/remove tool from the torque multiplier. Refer to Figure 1024.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(e)Remove the Sweeney-8100torque multiplier from the splined drive (item 9) of the 11C3006   install/remove fixture.
(f)Remove the capscrews (item 19) that attach the housing (item 4) to the clamp (item 3). Refer to Figure 1023.
(g)Attach a three-legged sling and overhead hoist to the hoist rings (item 32) on the housing (item 4) and remove it from the clamp (item 3).
(h)Remove the retainer nut (item 8) with the spanner (item 14).
(i)Remove the nut (item 7) with the spanner wrench (item 14).
(j)Remove the locating ring (item 6).
(25)Remove the shaft adapter (item 7) from the 11C3024   assembly/disassembly fixture as follows. Refer to Sheet 2 and Figure 1021.
(a)Loosen and remove the stress ring (item 6).
(b)Loosen and remove the setscrews (item 15).
(c)Loosen and disengage the ring (item 4) from the shaft base (item 5).
(d)Loosen the shaft adapter (item 7).
(e)Attach the hoist (item 9) to the shaft adapter (item 7) with the quick release pin (item 11).
(f)Attach an overhead hoist to the hoist (item 9) to remove the shaft adapter (item 7) and the ring (item 4) from the shaft base (item 5).
(26)Install the disk bore protector (item 10) on the end of the shaft base (item 5) of the 11C3024   assembly/disassembly fixture. Refer to Figure 1005.
(27)Remove the remaining items of the 11C3006   install/remove fixture as follows:
(a)Remove the pusher (item 5) and the collar (item 17). Refer to Figure 1022.
(b)Remove the lifting pins (item 27) from the clamp (item 3). Refer to Figure 1005.
(c)Remove the capscrews (item 36) to disconnect the clamp (item 3) halves and remove the clamp (item 3) from the interstage seal.
(d)Install the lifting pins (item 27) in the locator (item 2).
(e)Use a three-legged sling and an overhead hoist to remove the locator (item 2).
Subtask 72-53-00-220-223
(28)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1026.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1026   Critical Areas of the Stage 1 Disk Aft Shaft to Inspect the After Interstage Seal Installation
Subtask 72-53-00-220-064
P.Deleted.
(1)Deleted.
Subtask 72-53-00-440-180
(2)Deleted.
Subtask 72-53-00-440-181
CAUTION:
MAKE SURE THAT THE INTERSTAGE SEAL KEYS ARE NOT INSTALLED IN THE KEY RETAINING WIRE CUTOUTS. DAMAGE TO THE HARDWARE CAN OCCUR.
Q.Install the HPT rotor interstage seal keys (interstage seal keys) (150AE) in the four spaces in the interstage seal (150B3) between the tabs of the stage 1 disk (150A1). Refer to Figure 1027.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1027   Installation of the Interstage Seal Keys and the Retaining Wire on the Interstage Seal
Subtask 72-53-00-440-182
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
R.Install the interstage seal key retaining wire (retaining wire) (150W8) into the groove around the interstage seal (150AE) as follows:
(1)Apply C02-033  lubricant on the retaining wire.
(2)Put the straight end in first.
(3)Push the retaining wire along the groove and under the interstage seal keys (150AE) so that the shape is not changed.
(4)After the installation of the retaining wire, make sure that the hook end of the retaining wire points to the inner diameter.
Subtask 72-53-00-220-224
(5)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1028.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1028   Critical Areas of the Stage 1 Disk Aft Shaft to Inspect the After Interstage Seal Key Retaining Wire installation
Subtask 72-53-00-440-183
S.Install the ring seal (150N3) in the interstage seal (150B3) as follows. Refer to Figure 1029.
(1)Cut four ring seal segments to 20.00 inches (508.0 mm) in length.
(2)Use a file to remove unwanted material from the ends of the ring seal segments and make the ends square. Make sure that there are no burrs on the segments.
(3)Put the ring seal segments into the groove in the aft face of the interstage seal. Apply C10-012   tape to hold it in position. Then, install the next segment. Keep an end gap of 0.100-0.140 inch (2.54-3.56 mm).
(4)Repeat this procedure until all of the ring seal segments are installed. Cut the segments as necessary to keep an end gap of 0.100-0.140 inch (2.54-3.56 mm).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1029   Installation of the Ring Seal in the Interstage Seal
Subtask 72-53-00-220-065
(5)Measure the distances between the ends of the ring seal segments as follows:
(a)If the distance is more than 0.140 inch (3.56 mm), install a new ring seal segment.
(b)Remove a part of the ring seal segment if the distance is less than 0.100 inch (2.54 mm).
Subtask 72-53-00-440-184
(6)Remove the C10-012  tape and the ring seal from the interstage seal.
WARNING:
SYNTHETIC ADHESIVE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(7)Apply small amounts of C01-027  synthetic adhesive or C01-037  synthetic adhesive in the groove in the forward face of the interstage seal and on each of the ring seal segments.
(8)Install the ring seal in the groove in the aft face of the interstage seal.
Subtask 72-53-00-220-066
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
WARNING:
SYNTHETIC ADHESIVE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(9)Let the C01-027  synthetic adhesive or C01-037  synthetic adhesive cure for 15-20 minutes or until it is tacky.
NOTE:
The adhesive may be heat cured as long as the temperature used is not more than 250° F (121° C).
(10)Make sure that the ring seal segments are fully in the groove of the interstage seal and does not go above the groove of the interstage seal (150B3).
(11)Measure the distances between the ends of the ring seal segments to make sure that they are 0.100-0.140 inch (2.54-3.56 mm).
Subtask 72-53-00-440-185
T.Install the damper ring (150B9) on the interstage seal (150B3) as follows. Refer to Figure 1030.
(1)Compress the damper ring and install it in position on the aft side of the interstage seal.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1030   Installation of the Damper Ring on the Interstage Seal
Subtask 72-53-00-220-068
(2)Measure dimension AB between the ends of the damper ring as follows:
(a)Make sure that the damper ring is fully in position.
(b)Measure dimension AB with a vernier caliper. Make sure that the distance is a minimum of 0.060 inch (1.52 mm).
Subtask 72-53-00-440-186
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
U.Alternative Procedure Available. Assemble the shank nuts (01-100) (SIN 15041) into the aft flange of the HPT rotor stage 2 disk (stage 2 disk) (150B1) with the 11C3068   install/remove fixture. Refer to Figure 1031 and do as follows:
(1)Install the shank nuts (15041) into the aft flange of the stage 2 disk.
(2)Put the installation socket (item 2) on a 3/8-inch ratchet.
(3)Put the installation socket (item 2) into the front flange of the stage 2 disk and turn it CW into the shank nut (15041).
(4)Continue to turn the ratchet CW until the shank nut (15041) is tight against the stage 2 disk.
(5)Repeat steps 1 through 4 for each shank nut (15041).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1031   Installation of the Shank Nuts on the Stage 2 Disk with the Install/Remove Fixture, 11C3068
Subtask 72-53-00-220-069
(6)Make sure that there are no cracks in the shank nuts.
Subtask 72-53-00-220-070
(7)Make sure that the washer faces of the shank nuts are fully flush with the flange of the stage 2 disk.
Subtask 72-53-00-220-225
(8)Do a general visual inspection of the exposed surfaces of HPT rotor stage 2 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1032.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1032   Critical Areas of the Stage 2 Disk Aft Shaft to Inspect the After Shank Nut Installation
Subtask 72-53-00-440-305
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
U.A.Alternative Procedure. Install the shank nuts (15041) in the aft flange of the stage 2 disk (150B1) with the 7C2071   install/remove fixture as follows. Refer to Figure 1034.
(1)Install the shank nuts (15041) in the HPT rotor stage 2 disk (150B1) flange with the 7C2071   install/remove fixture as follows. Refer to Figure 1034.
(a)Remove the protection from the 7C2071   install/remove fixture.
(b)Wipe clean the 7C2071   install/remove fixture parts and HPT rotor stage 2 disk (150B1) with C10-182  lint free cloth.
(c)Examine the 7C2071   install/remove fixture for damage and foreign material and high metal.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTIVE EQUIPMENT. USE IN A WELL-VENTILLATED AREA.
(d)Clean mating surfaces with C04-035   isopropyl alcohol.
(e)Install the flaring driver (item 6) on the plunger (item 7) of the 7C2071   install/remove fixture.
(f)Install the install anvil (item 3) on the body (item 2) of the 7C2071   install/remove fixture with the ball lock pin (item 10).
(g)Connect the PA-133R   air hydraulic pump to the 7C2071   install/remove fixture relief valve (item 11) and a supply of clean, dry air.
(h)Put the 12 shank nuts (15041) in the flange holes in the HPT rotor stage 2 disk (150B1) aft flange.
CAUTION:
DO NOT APPLY MORE THAN 3600 PSI (24821.1 KPA) TO THE FIXTURE. PRESSURE OF MORE THAN 3600 PSI (24821.1 KPA) CAN DAMAGE THE HARDWARE.
(i)Put the install anvil (item 3) of the 7C2071   install/remove fixture over a shank nut (15041) and operate the 7C2071   install/remove fixture to extend the flaring driver (item 6) to install the shank nut (15041). Do not apply more than 3600 psi (24821.1 kPa) to the fixture.
(j)Move the 7C2071   install/remove fixture to the shank nuts (15041) that remain and install them one at a time.
(k)Make sure each shank nut (15041) is tightly attached and the washer face of the shank nut (15041) is flush with the flange.
(l)When all of the shank nuts (15041) are installed use 3X magnification glass to do a visual inspection of all shank nuts (15041) for cracks. No cracks are permitted.
(m)Store the 7C2071   install/remove fixture.
Subtask 72-53-00-220-226
(2)Do a general visual inspection of the exposed surfaces of HPT rotor stage 2 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1033.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1033   Critical Areas of the Stage 2 Disk Aft Shaft to Inspect the After Shank Nut Installation
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1034   Installation of the Shank Nuts on the Stage 2 Disk with the Install/Remove Fixture, 7C2071
Subtask 72-53-00-440-187
CAUTION:
DO THIS STEP ONLY IF THERE IS ENOUGH TIME TO FINISH IT. THE STAGE 2 DISK AND THE INTERSTAGE SEAL ARE INTERFERENCE FIT PARTS. THEY MUST BE FULLY ASSEMBLED BEFORE THEIR TEMPERATURES BECOME EQUAL OR DAMAGE TO THE PARTS CAN OCCUR.
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
V.Assemble the stage 2 disk (150B1) on the interstage seal (150B3) and the stage 1 disk (150A1) as follows:
(1)Before the installation of the stage 2 disk (01-130) (SIN 150B1), measure the thickness of the aft shaft flange at four equally spaced locations. Record the average value as dimension AD. Refer to Figure 1035.
Dimension AD = ____________.
(2)Before the installation of the stage 2 disk (01-130) (SIN 150B1), measure the stage 1 disk (01-280) (SIN 150A1) aft shaft axial drop from the aft castellations to the spline aft face at four equally spaced locations. Record the average value as dimension AE. Refer to Figure 1036.
Dimension AE = ____________.
(3)Install the guide tube (item 4) of the 11C3022   install/remove fixture with the threads engaged on the aft end of the stage 1 disk shaft. Refer to Figure 1037.
(4)Retract the hydraulic cylinder (item 7).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(5)Attach a hoist to the sling link (item 11) to lift the puller (item 2).
(6)Lower the puller (item 2) to the aft flange of the stage 2 disk (150B1).
(7)Attach the puller (item 2) to the aft flange of the stage 2 disk (150B1) with the captive screws (item 5). Torque the captive screws (item 5) to 92-108 lb in. (10.4-12.2 N.m).
(8)Use a C05-003  marking pen to mark in a CW direction ALF of the stage 2 disk (150B1) the position of the 1-1 and 5-5 disk post. Refer to Figure 1038.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
MAKE SURE THE STAGE 2 DISK TEMPERATURE IS NOT MORE THAN 700°F (371°C) OR THE STAGE 1 DISK CAN BE DAMAGED.
NOTE:
The 11C3034   heater consists of a G01 and a G02. The G01 is for 120 VAC, 60 Hz and the G02 is for 230 VAC, 50 Hz.
(9)Lift the stage 2 disk (150B1) and put it on the 11C3034   heater (item 2 or item 15).
(10)Increase the temperature of the stage 2 disk to 180 °F (82.2 °C) as follows. Refer to Figure 1038.
(a)Plug in the heater (item 6 or item 12) into the electrical outlet and set the output to “high”.
(b)Monitor the temperature of the stage 2 disk with a calibrated temperature probe.
(c)When the disk temperature reaches 180 °F (82.2 °C) turn the heater to low. Allow the heater to operate in the low position for several minutes before turning off to accelerate the cooling of the heater.
(11)Remove the bore disk protector (item 10) of the 11C3024   assembly/disassembly fixture. Refer to Figure 1005.
(12)Remove the stage 2 disk (150B1) from the 11C3024   heater and align the 1-1 slots of the stage 2 disk and stage 1 disk. Refer to Figure 1038.
(13)Align the plunger (item 3) of the 11C3022   install/remove fixture with the aft end of the guide tube (item 4). Refer to Figure 1037.
(14)Lower the stage 2 disk (01-130) (SIN 150B1) into position on the stage 1 disk/interstage seal assembly. Make sure that the 1-1 slots of the two disks are nearly/closely aligned.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1035   Stage 2 Aft Shaft Flange Thickness Measurement
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1036   Stage 1 Disk Aft Shaft Axial Drop from the Aft Castellations to the Spline Aft Face
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1037   Installation of the Install/Remove Fixture, 11C3022
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1038   Installation of the Stage 2 Disk on the Heater, 11C3034
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1039   Installation of the Stage 2 Disk on the Stage 1 Disk and Interstage Seal
Subtask 72-53-00-220-071
(15)Make sure that there is no space between the stage 2 disk and the interstage seal in a minimum of four positions. Use a 0.001 inch (0.03 mm) shim.
Subtask 72-53-00-440-188
(16)Remove the 11C3022   install/remove fixture. Refer to Figure 1039.
Subtask 72-53-00-220-227
(17)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk and stage 2 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1040.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1040   Critical Areas of the Stage 1 and Stage 2 Disk Aft Shafts to Inspect the After Stage 2 Disk Installation
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1041   Installation of the Coupling Nut on the Stage 1 Disk Shaft
Subtask 72-53-00-440-192
W.Assemble the HPT aft rotating seal (aft seal) (150B4) to the stage 2 disk (150B1) as follows:
(1)Apply C02-033  lubricant to the surfaces of the bayonet on the forward side of the aft seal (150B4) labeled Y. Refer to Figure 1042.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(2)Fill a chill fixture with dry ice and chill the aft seal for 20-30 minutes.
(3)Put the aft seal on the stage 2 disk.
(4)Make sure that the bayonet tabs are aligned with the rail of the stage 2 disk and that the boltholes are aligned.
(5)Apply C02-058  lubricant to the threads and friction surfaces of the machine bolts (bolts) (15022).
NOTE:
Use a minimum quantity of lubricant necessary for assembly. After assembly, remove remaining lubricant with a clean cloth.
NOTE:
Balance weights (01-070) (SIN 150W1), (01-060) (SIN 150W2), and (01-075) (SIN 150W3) can be used as needed, along with bolts (01-040) (SIN 15022) when the final balance procedure is done.
(6)Make sure the bayonet tab is fully seated on the rail of the stage 2 disk.
(7)Install the bolts (01-040) (SIN 15022) through the aft seal and into the stage 2 disk.
(8)Torque the bolts to 106-124 lb in. (12.0-14.0 N.m) in a crisscross pattern.
(9)Install the damper ring (150BC) on the aft seal (150B4). Refer to Figure 1044.
(10)Measure the damper ring end gap. The end gap must be between 0.060-0.210 inch (1.52-5.33 mm).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1042   Apply Soft Petrolatum to the Aft Seal
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1043   Installation of the Aft Seal on the Stage 2 Disk
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1044   Installation of the Damper Ring on the Aft Seal
Subtask 72-53-00-440-194
X.Torque the coupling nut (01-030) (SIN 150AD). Refer to TASK 72-53-00-800-801 (72-53-00, SPECIAL PROCEDURE 001).
Subtask 72-53-00-440-304
Y.Measure dimension AL between the stage 1 blade retainer (01-180) (SIN 150BB) and the aft edge of the stage 1 disk (01-280) (SIN 150A1) at eight equally-spaced locations. Refer to Figure 1045.
(1)Use a shim to make sure that the gap clearance AL is not more than 0.002 inch (0.05 mm).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1045   Measurement of the Dimension AL on the Stage 1 Disk and the Interstage Seal
Subtask 72-53-00-220-115
Z.Do a runout measurement of the number 4 bearing journal:
(1)If the 11C3008   HPT rotor support fixture is not installed on the rotary table of the 9471M13   inspection system, install it as follows. Refer to Figure 1046.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTIVE EQUIPMENT. USE IN A WELL-VENTILLATED AREA.
(a)Clean the top surface of the rotary table with C04-035   isopropyl alcohol.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift the 11C3008   HPT rotor support fixture and align the mounting holes with the holes in the rotary table of the 9471M13   inspection system.
(c)Line up the 11C3008   HPT rotor support fixture mounting hole with the tapped holes in the rotary table and secure it with capscrews (item 7). Do not fully tighten the capscrews at this time. Refer to Figure 1002.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1046   Measurement of the No. 4 Bearing Journal Runout
Subtask 72-53-00-220-119
(a)Make a selection of Tilt/Center from the main menu on the computer screen.
(b)Make a selection of the setup named GEnx HPTR AFTER COUPLING NUT from the SELECT A PARAMETER FILE.
NOTE:
This setup only uses one of the four gages.
(c)Put gage 1 against the O.D. of the 11C3008   HPT rotor support fixture base (item 2).
(d)Push on the DISPLAY GAGES button on the computer screen.
(e)Turn the rotary table and watch the readings.
(f)Move the 11C3008   HPT rotor support fixture as necessary to center it on the rotary table within 0.004 inch (0.10 mm).
(g)Tighten capscrews (item 7).
(h)Remove gage 1 from the 11C3008   HPT rotor support fixture.
(2)Do the runout of the number 4 bearing journal as follows:
(a)Attach the 11C3056   lift fixture to the threads on the aft end of the stage 1 disk (150A1). Turn CW, ALF, until the 11C3056   lift fixture is fully engaged on the HPT rotor shaft. Lower the HPT Rotor assembly (34-020 , 72-00-02) (SIN 15000) on to the 11C3008   HPT rotor support fixture.
(b)Remove the 11C3056   lift fixture.
CAUTION:
DO NOT TURN THE ROTARY TABLE UNTIL YOU MAKE SURE THAT THERE IS NO INTERFERENCE BETWEEN THE STAGE 1 AND STAGE 2 HPT ROTORS AND THE GAGES. YOU CAN DAMAGE THE GAGES.
NOTE:
This procedure uses only three of the four gages.
(c)Put the plunger of gage 1 against the forward rabbet of the front shaft outboard of the bolt holes.
(d)Put the lever of gage 3 against the forward face of the front shaft directly across from gage 1.
(e)Put the plunger of gage 2 against the number 4 bearing journal.
NOTE:
The gages are setup correctly if you can see that the tips of the barrels (gages 1 and 2) and lever (gage 3) are aligned so they sit in an imaginary plane that cuts through the centerline of the rotary table.
(f)Push on the DISPLAY GAGES button on the computer screen.
(g)Adjust all of the gages so the bar graphs are close to zero.
NOTE:
It is not necessary to adjust the gages fully to zero.
NOTE:
You must make sure that TILT is highlighted on the computer screen.
(h)Push on the DISPLAY LINEAR PLOT button on the computer screen.
CAUTION:
DO NOT TURN THE ROTARY TABLE UNTIL YOU MAKE SURE THAT THERE IS NO INTERFERENCE BETWEEN THE STAGE 1 HPT AND STAGE 2 HPT ROTORS AND THE GAGES. YOU CAN DAMAGE THE GAGES.
(i)Slowly turn the rotary table and make sure that all of the gages and cables are clear.
NOTE:
The tilt check must be performed before the center check.
(j)Make a selection TILT on the computer screen.
(k)Turn the rotary table and collect the data.
(l)Turn the large silver tilt knobs until the value is less than 0.0003 inch (0.008 mm).
NOTE:
Use the tilt knob that is closest to line up under the gages and can be under the gages on the left or the right.
(m)Turn the rotary table and line up the angle with the angle displayed next to the tilt reading.
(n)Make a selection CENTER on the computer screen.
(o)Turn the rotary table and collect data.
(p)Turn the small black center knobs until the value is less than 0.0003 inch (0.008 mm).
NOTE:
Use the center knob that is closet to line up under the gages and can be under the gages on the left or the right.
(q)Turn the rotary table and line up the angle with the angle displayed next to the center reading.
(r)Make a selection TILT on the computer screen and turn the rotary table. Make sure that the tilt reading is still in tolerance.
(s)Measure the number 4 bearing journal data as follows:
1Make a selection MEASURE button on the computer screen.
2Make a selection NEW RUN.
3Enter the serial number of the stage 1 disk (150A1).
NOTE:
The zero gage is formed when gage 1 and gage 2 are aligned and is the imaginary plane that cuts through the centerline of the rotary table.
4Turn the stage 2 disk (150B1) and line up the 1-1 slot with the zero gage.
5Press enter when they line up.
NOTE:
You must turn the rotary table with enough force to make two complete revolutions.
NOTE:
The direction of rotation is CCW looking down on the rotary table.
NOTE:
No data is taken during the first 360 degrees of rotation. After the rotary table goes past the zero position mark, it will start to collect data.
6Turn the rotary table to collect the data to make two complete revolutions.
7Stop the table when the data is collected.
8Press the PRINT button on the computer screen.
(t)Look at the last line of the print out for the stack projection (SP).
(u)Look at the bottom corner of the computer screen for the angle display.
(v)Turn the rotary table until the display angle matches the concentricity angle.
(w)Use a C05-003  marking pen and put a large capital L in a location that is easy to see at assembly.
(3)Do a check of the runout of the aft stage 1 blade retainer (01-180) (SIN 150BB) as follows. Refer to Figure 1047.
NOTE:
This procedure will use the gages that are set up on the forward flange rabbet and the forward flange face (gages 1 and 3), gage 2 can remain in position on the No. 4 bearing journal. The gage 4 will be used on the stage 1 blade retainer tip forward face.
(a)Keep the gage 1 and gage 3 in position on the forward flange rabbet and forward flange face.
(b)Do the tilt and center procedure if not previously done.
(c)Put the lever of gage 4 on the forward face of the stage 1 blade retainer tip.
(d)Press the DISPLAY GAGES button on the computer screen.
(e)Adjust the gage (gage 4) to make the bar graph near zero.
(f)Press the DISPLAY LINEAR PLOT button on the computer screen.
(g)Make sure the gages and cables will not interfere when the rotary table is turned.
(h)Turn the rotary table to collect the data.
(i)Do the measurement of the stage 1 blade retainer tip as follows:
1Press the MEASURE button on the computer screen.
2Press the NEW RUN button on the computer screen.
3Enter the serial number of the HPT stage 1 disk in the computer.
(j)Turn the stage 2 disk (150B1) and align the 1-1 slot on the stage 1 disk (150A1) with the gage.
(k)Press ENTER when the stage 2 disk (150B1) and the 1-1 slot on the stage 1 disk (150A1) and the gage are aligned.
(l)Turn the rotary table two full rotations to collect the data.
(m)Stop the rotary table after the data is collected.
(n)Press the PRINT button on the computer screen.
(o)Runout must not be more that 0.015 inch (0.38 mm).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(4)Use and overhead hoist and lower the 11C3056   lift fixture. Refer to Figure 1048.
(5)Attach the 11C3056   lift fixture to the HPT rotor assembly.
(6)Lift the stage 1 HPT Rotor and put it on the 11C3024   assembly/disassembly fixture.
(7)Put the collected data printout with the HPT rotor assembly.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1047   (Sheet 1 ) Measurement of the Stage 1 Blade Retainer Runout
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1047   (Sheet 2 ) Measurement of the Stage 1 Blade Retainer Runout
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1048   Installation of the HPT Rotor Assembly on the Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-202
AA.Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) on the 11C4537   horizontal transport dolly. Refer to the manufacturer's instructions and do as follows:
(1)Lift the HPT rotor assembly from the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1006.
(a)Attach the 11C3056   lift fixture to the threads on the aft end of the stage 1 disk. Turn CW, ALF, until the 11C3056   lift fixture is fully engaged on the HPT rotor shaft.
(b)Attach an overhead hoist to the 11C3056   lift fixture.
(c)Remove the nuts (item 14) and washers (item 20) that attach the HPT rotor assembly to the 11C3024   assembly/disassembly fixture.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(d)Lift the HPT rotor assembly from the 11C3024   assembly/disassembly fixture.
(e)Remove the retaining rings (item 8) of the 11C3024   assembly/disassembly fixture from the aft face of the forward flange of the stage 1 disk.
Subtask 72-53-00-440-306
(2)Alternative procedure available. Install the 11C4285   balance arbor and 11C3438   lift fixture on the HPT stage 1 disk as follows:
(a)Install the 11C4285   balance arbor on the stage 1 disk as follows. Refer to Figure 1049.
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURER’S (MATERIAL) SAFETY DATA SHEET (SDS) FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF CONSUMABLE PRODUCTS.
1Decrease the temperature of the forward flange of the stage 1 disk with dry ice or liquid nitrogen.
2Clean the mating surfaces of the 11C4285   balance arbor with C04-035  isopropyl alcohol.
3Put the 11C4285   balance arbor on the 7C2199   installation fixture. Install the arbor with the large flange up. Refer to Figure 1049.
4Optional Procedure. Increase the temperature of the arbor to 350°F (177°C).
5The steps that follow must be done as quickly as possible in order to make the assembly of the HPT rotor and balance arbor easier.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
6Lift the HPT rotor assembly from the 11C3018   vertical support fixture.
7Put the HPT rotor assembly in position above the 11C4285   balance arbor on the 7C2199   installation fixture.
8Align the 1-1 mark on the arbor with the 1-1 slot on the HPT stage 1 disk (150A1).
9Lower the forward flange of the HPT stage 1 disk into the inner diameter of the arbor.
10Adjust the HPT rotor assembly as necessary to align the boltholes of the forward flange with the boltholes in the balance arbor.
11Push the 11C4285   balance arbor against the HPT stage 1 disk to make sure that the arbor was installed. Use rubber mallet if necessary.
12Let the parts go back to ambient temperature. Use the fan (item 14) of the 7C2199   installation fixture to help the parts go back to room temperature.
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURER’S (MATERIAL) SAFETY DATA SHEET FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF THIS PRODUCT.
13Apply the C02-058  lubricant on the cap screw (item 2) threads.
14Install 23 cap screws (item 2) in every hole of the arbor. Install the cap screws from inside the stage 1 disk with the bolt heads up.
15Install a balance nut (item 3) on each cap screw.
16Torque the balance nuts to 32 lb ft (43.4 N.m) in a criss-cross pattern.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
17Lift the HPT rotor assembly from the 7C2199   installation fixture.
18Install the plastic cover (item 4) with the five hex head bolts (item 5).
(b)Install the 11C3438   lift fixture and 9429M14   lift arm on the 11C4285   balance arbor as follows. Refer to Figure 1050.
1Attach the adapter plate (item 2) and clevis (item 3) to the 11C4285   balance arbor with cap screws (item 4).
2Attach the 9429M14   lift arm fixture to the clevis (item 3) with the ball lock pin.
3Attach an overhead hoist to the 9429M14   lift arm.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1049   Installation of the 11C4285 Balance Adapter
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1050   Installation of the 11C3438 Lift/Turn Fixture and 9429M14 Lift Arm Fixture on the 11C4285 Balance Adapter
Subtask 72-53-00-440-307
(2).A.Alternative Procedure. Install the 11C4554   balance arbor on the stage 1 disk as follows. Refer to Figure 1052.
(a)Put the HPT rotor assembly on the 11C3018   vertical support fixture. Refer to TASK 72-00-02-430-817 (72-00-02, ASSEMBLY 002).
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
(b)Decrease the temperature of the forward flange of the stage 1 disk with dry ice or liquid nitrogen.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTIVE EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(c)Clean the mating surfaces of the 11C4554   balance arbor with C04-035  isopropyl alcohol.
(d)Put the arbor (item 2) of the 11C4554   balance arbor on the 7C2199   installation fixture. Install the arbor with the large flange up. Refer to Figure 1052.
(e)Increase the temperature of the arbor to 350°F (177°C).
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(f)Install the HPT rotor assembly onto the 11C4554   balance arbor as follows:
NOTE:
To make assembly of the HPT rotor and balance arbor easier, do the steps that follow as quickly as possible.
1Lift the HPT rotor assembly from the 11C3018   vertical support fixture.
2Put the HPT rotor assembly in position above the 11C4554   balance arbor on the 7C2199   installation fixture.
3Align the 1-1 mark on the arbor (item 2) with the 1-1 slot on the stage 1 disk (150A1).
4Lower the forward flange of the stage 1 disk into the inner diameter of the arbor (item 2).
5Adjust the HPT rotor assembly as necessary to align the boltholes of the forward flange with the boltholes in the balance arbor. Use a cap screw (item 8) of the 11C4554   balance arbor to make sure the boltholes align.
(g)Let the parts go back to ambient temperature. Use the fan (item 14) of the 7C2199   installation fixture to help the parts go back to room temperature.
(h)Install 23 cap screws (item 8) in every other hole of the arbor (item 2). Install the cap screws from inside the stage 1 disk with the bolt heads up.
CAUTION:
ONLY USE THE BALANCE NUTS OF THE 11C4554 BALANCE ARBOR. THESE NUTS ARE BALANCED TO EACH OTHER. USE OF ANY OTHER NUTS CAN CAUSE AN UNSAFE, OUT OF BALANCE CONDITION. DAMAGE TO THE TOOLS OR THE HARDWARE CAN OCCUR.
(i)Install a balance nut (item 4) on each cap screw (item 8).
(j)Tighten the balance nuts (item 4) to 32 lb ft (43.4 N.m) in a crisscross pattern.
(k)Lift the HPT rotor assembly from the 7C2199   installation fixture.
(l)Install the dust cover (item 3) of the 11C4554   balance arbor on the arbor (item 2) with capscrews (item 9). Refer to Figure 1053.
(m)Install the 11C4558   lift fixture on the 11C4554   balance arbor as follows:
1Remove the ball lock pin and remove the lift arm (item 4).
2Attach the adapter plate (item 2) and clevis (item 5) to the 11C4554   balance arbor with cap screws (item 6).
3Attach the lift arm (item 4) to the clevis (item 5) with the ball lock pin.
4Attach an overhead hoist to the lift arm (item 4).
CAUTION:
MAKE SURE THE ARMS OF THE LIFT FIXTURES ARE HINGED IN THE SAME DIRECTION BEFORE YOU TURN THE HPT ROTOR ASSEMBLY. DAMAGE TO THE TOOLS OR HPT ROTOR ASSEMBLY CAN OCCUR
(3)Lift the forward end of the HPT rotor assembly and lower the aft end until the HPT rotor assembly is horizontal. Refer to Figure 1053.
(4)Put the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) on the 11C4537   horizontal transport dolly. Refer to Figure 1051 and do as follows:
(a)Engage floor locks and open the swing clamp (item 4) of the 11C4537   horizontal transport dolly.
(b)Release the retractable plunger (item 18) and move the slider stop (item 8) out.
(c)Put the HPT rotor assembly on the 11C4537   horizontal transport dolly and make sure the forward end points to the push handles.
1 Put the HPT rotor assembly in a position to make sure that the coupling nut (01-030) (SIN 150AD) sits on the 5 inch wheel (item 16).
(d)Optional procedure. Prevent the HPT rotor assembly from axial movement as follows:
1 Install the axial stop (item 9) of the 11C4537   horizontal transport dolly on the aft shaft of the HPT rotor assembly.
2 Move the slider stop (item 8) in and lock it with the retractable plunger (item 18).
3 If necessary, adjust the axial stop (item 9).
(e)Close the swing clamp (item 4) and tighten it with the hand knob (item 15).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1051   (Sheet 1 ) Installation of the HPT Rotor Assembly on the Horizontal Transport Dolly, 11C4537
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1051   (Sheet 2 ) Installation of the HPT Rotor Assembly on the Horizontal Transport Dolly, 11C4537
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1052   Installation of the 11C4554 Balance Arbor
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1053   (Sheet 1 ) Installation of the 11C4558 Lift Fixture
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1053   (Sheet 2 ) Lift the HPT Rotor Assembly with the 11C3056 Lift Fixture and the 11C4558 Lift Fixture
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1054   Lift the HPT Rotor Assembly with the 11C3056 Lift Fixture and the 9429M14 Lift Arm
Subtask 72-53-00-440-286
AB.Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1055   Installation of the 11C3012 Balance and Grind Adapter
Subtask 72-53-00-440-209
* * * FOR 1B/P/G03.1B/P/G04
* * * PRE SB   72-0089( Stage 1 Blades without TBC Improvement )
AC.Alternative Procedure Available. Install the HPT blades (stage 1 blades) (01-210) (SIN 150A0) or (01-211) (SIN 150A0). Refer to Figure 1056 and as follows:
(1)Prepare the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) for installation as follows:
(a)Use a C05-003  marking pen and mark each stage 1 blade from 1-62.
(b)Pan weigh the stage 1 blades from 1-62.
(c)Make a plot of the stage 1 blades for the minimum amount of unbalance possible.
(d)Record the weight and mark it on each tip of the stage 1 blades.
(2)Install the stage 1 blades into the stage 1 disk (01-280) (SIN 150A1) as follows:
(a)Do a visual inspection to make sure that the four seal rings (01-200) (SIN 150N2) are fully seated in the groove on the forward face of the stage 1 blade retainer (01-180) (SIN 150BB) before each of the stage 1 blades is installed.
(b)Install the first stage 1 blade (01-210) (SIN 150A0) or (01-211) (SIN 150A0), in the order shown on the stage 1 blades plot, in the 1-1 dovetail slot of the stage 1 disk (01-280) (SIN 150A1).
(c)Make sure that the leading edge of the stage 1 blade points forward.
(d)Continue to install the stage 1 blades.
(e)To install the last blades, move approximately 15 blades forward in the dovetail slot, a small distance until you can install the last blade.
(f)Push the blades back into position.
(g)Make sure that the stage 1 blades are against the stage 1 blade retainer (01-180) (SIN 150BB).
* * * FOR 1B/P/G03.1B/P/G04
* * * END PRE SB   72-0089
Subtask 72-53-00-440-310
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
NOTE:
Subtask 72-53-00-440-310 (paragraph 3.AC.A.) and Subtask 72-53-00-440-529 (paragraph 3.AC.B.) are alternatives. Subtask 72-53-00-440-310 (paragraph 3.AC.A.) is preferred.
NOTE:
Post SB 72-0494 stage 1 blades must be installed in an engine which has incorporated a higher flowing HPT support nozzle. Refer to GEnx-1B SB 72-0294, or SB 72-0359, or SB 72-0379, or SB 72-0380. Post SB 72-0494 stage 1 HPT blade P/N 2706M85G10   can be mixed in a set with P/N 2706M85G07   . Post SB 72-0494 HPT stage 1 blade P/N 2706M85G10   cannot be used with a HPT forward seal P/N 2352M60P01   .
* * * SB   72-0089( Stage 1 Blades with TBC Improvement )
AC.A.Alternative Procedure Available. Install the stage 1 blades (01-211) (SIN 150A0). Refer to Figure 1056 and as follows:
(1)Prepare the stage 1 blades (01-211) (SIN 150A0) for installation as follows:
(a)Use a C05-003  marking pen and mark each stage 1 blade from 1-62.
(b)Pan weigh the stage 1 blades from 1-62.
(c)Make a plot of the stage 1 blades for the minimum amount of unbalance possible.
(d)Record the weight and mark it on each tip of the stage 1 blades.
(2)Install the stage 1 blades into the stage 1 disk (01-280) (SIN 150A1) as follows:
(a)Do a visual inspection to make sure that the four seal ring (01-200) (SIN 150N2) are fully seated in the groove on the forward face of the stage 1 blade retainer (01-180) (SIN 150BB) before each of the stage 1 blades is installed.
(b)Install the first stage 1 blade (01-211) (SIN 150A0), in the order shown on the stage 1 blades plot, in the 1-1 dovetail slot of the stage 1 disk (01-280) (SIN 150A1).
(c)Make sure that the leading edge of the stage 1 blade points forward.
(d)Continue to install the stage 1 blades.
(e)To install the last stage 1 blade, move approximately 15 blades forward in the dovetail slot, a small distance until the last stage 1 blade can be installed.
(f)Push the stage 1 blades back into position.
(g)Make sure that the stage 1 blades are against the interstage seal (01-170) (SIN 150B3).
* * * END SB   72-0089
Subtask 72-53-00-440-529
NOTE:
Post SB 72-0494 stage 1 blades must be installed in an engine which has incorporated a higher flowing HPT support nozzle. Refer to GEnx-1B SB 72-0294, or SB 72-0359, or SB 72-0379, or SB 72-0380. Post SB 72-0494 stage 1 HPT blade P/N 2706M85G10   can be mixed in a set with P/N 2706M85G07   . Post SB 72-0494 HPT stage 1 blade P/N 2706M85G10   cannot be used with a HPT forward seal P/N 2352M60P01   .
AC.B.Alternative Procedure. Install the stage 1 blades (01-210) (SIN 150A0) or (01-211)(SIN 150A0) and the stage 1 dampers (01-220) (SIN 150AB) into the stage 1 disk (01-280) (SIN 150A1). Refer to Subtask 72-53-00-440-239 (paragraph 3.AR.).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1056   (Sheet 1 ) Installation of the Stage 1 and 2 Blades
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1056   (Sheet 2 ) Installation of the Stage 1 and 2 Blades
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1056   (Sheet 3 ) Installation of the Stages 1 and 2 Blades
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1056   (Sheet 4 ) Installation of the Stages 1 and 2 Blades
Subtask 72-53-00-440-211
AD.Install the stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) as follows. Refer to Figure 1056.
(1)Prepare the stage 2 blades for installation as follows:
(a)Use a C05-003  marking pen and mark each stage 2 blade from 1-62.
(b)Pan weigh the stage 2 blades from 1-62.
(c)Make a plot of the stage 2 blades for the minimum amount of unbalance possible.
(d)Record the weight and mark it on each stage 2 blade tip.
(2)Install the stage 2 blades in the stage 2 disk (01-130) (SIN 150B1) as follows:
(a)Install the first stage 2 blade, in the order shown, in the 1-1 dovetail slot of the stage 2 disk (01-130) (SIN 150B1).
(b)Make sure that the leading edge of the stage 2 blade points to the forward end of the stage 1 disk (01-280) (SIN 150A1).
(c)Continue to install the stage 2 blades.
(d)To install the last stage 2 blade, move approximately 15 blades aft in the dovetail slot, a small distance until the last stage 2 blade can be installed.
(e)Push the stage 2 blades back into position.
(f)Make sure that the stage 2 blades are against the interstage seal (01-170) (SIN 150B3).
Subtask 72-53-00-440-212
AE.Optional Procedure, required if Subtask 72-53-00-440-213 (paragraph 3.AF.) is accomplished. Install the rubber band blade retainers to hold the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0). Refer to Figure 1057 and do as follows:
CAUTION:
MAKE SURE THAT THE RUBBER BAND BLADE RETAINERS ARE SIZE NO. 32 RUBBER BANDS. IF YOU DO NOT USE THE CORRECT SIZE, THE RUBBER BANDS CAN BREAK AND RELEASE THE BLADES DURING THE BALANCE PROCEDURE WHICH WILL CAUSE DAMAGE TO THE ENGINE HARDWARE AND TOOLING.
(1)Make sure that you have the correct size No. 32 rubber bands.
(2)Install two size No. 32 rubber bands around the front side of one stage 1 blade and pull it around the aft side of one adjacent stage 2 blade. Push the rubber bands down to the blade platforms.
(3)Continue this procedure until all 62 stage 1 blades and 62 stage 2 blades are retained with size No. 32 rubber bands.
(4)Make sure that all of the stages 1 and 2 blades are correctly retained.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1057   Installation of the Rubber Band Blade Retainers
Subtask 72-53-00-440-213
AF.Optional Procedure. Do a green balance of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) as follows:
(1)Move the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) from 11C4537   horizontal transport dolly to the balance machine.
(a)Attach the overhead hoist to the 11C3056   lift fixture and the 11C4558   lift fixture or the 9429M14   lift arm.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift the HPT rotor assembly from the 11C4537   horizontal transport dolly.
(c)Put the HPT rotor assembly on the balance machine. Refer to the balance machine manufacturer's instructions for the installation of the HPT rotor assembly on the balance machine.
(d)Remove the 11C4558   lift fixture or the 9429M14   lift arm and the 11C3056   lift fixture from the HPT rotor assembly.
(2)Refer to the balance machine manufacturer's instructions to do a green balance of the HPT rotor assembly as follows:
WARNING:
CLOSE THE COVER OF THE BALANCE MACHINE BEFORE YOU LET THE ROTOR TURN. DO NOT OPEN THE COVER UNTIL THE ROTOR STOPS. AFTER THE POWER IS TURNED OFF, THE ROTOR WILL CONTINUE TO TURN WITH SUFFICIENT MOMENTUM TO CAUSE AN INJURY OR KILL YOU.
(a)Operate the balance machine at 750 rpm (minimum of 700 rpm).
(b)Cycle the balance machine, to 750 rpm, 2-3 times, to let the blades settle in position before proceeding.
WARNING:
LUBRICATING OILS MAY CAUSE SKIN, EYE AND RESPIRATORY IRRITATION WITH PROLONGED OR REPEATED CONTACT. USE PROPER PERSONAL PROTECTIVE EQUIPMENT TO PREVENT SKIN AND EYE CONTACT. IF EYE OR SKIN CONTACT OCCURS FLUSH EYES WITH WATER AND/OR WASH SKIN THOROUGHLY WITH SOAP AND WATER.
(c)Apply a light coat of C02-019  engine oil or C02-023  engine oil to the balance rollers.
(d)Make a two-plane setup to read in the planes of the plane CG, stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0), and plane CJ, stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0).
(e)Balance to a maximum of 100 gram inches in the planes of the stage 1 blades and stage 2 blades.
(f)Change the stage 1 blades and stage 2 blades from one position to another as necessary for the correct balance.
(g)Record the final magnitude of imbalance in gram inches and the angle in degrees of each balance plane. Refer to Figure 1058.
(h)Deleted.
(i)Deleted.
(j)Number the stage 1 blades and the stage 2 blades as follows. Refer to Figure 1060.
1Use a C05-003  marking pen to mark the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) from 1-62 in a counterclockwise (CCW) direction, forward looking aft (FLA). Refer to TASK 70-16-02-350-017 (TEMPORARY MARKING).
2Use a C05-003  marking pen to mark the stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) from 1-62 in a CW direction, ALF. Refer to TASK 70-16-02-350-017 (TEMPORARY MARKING).
(3)Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) in the 11C4537   horizontal transport dolly. Refer to the manufacturer's instructions and do as follows:
(a)Attach the 11C3056   lift fixture to the HPT rotor assembly and attach an overhead hoist to the lift bar (item 4).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Use a second overhead hoist and attach it to the lift bar (item 5) of the 11C3060   lift/turn fixture.
(c)Lift the HPT rotor assembly from the balance machine and put the HPT rotor assembly in the 11C4537   horizontal transport dolly.
(d)Remove the 11C3060   lift/turn fixture and the 11C3056   lift fixture from the HPT rotor assembly.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1058   HPT Rotor Assembly Green Balance - Record Sheet
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1059   DELETED
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1060   Stage 1 and Stage 2 Blades Numeration
Subtask 72-53-00-440-214
AG.Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1061   DELETED
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1062   DELETED
Subtask 72-53-00-440-215
AH.Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1063   DELETED
Subtask 72-53-00-220-076
AI.Deleted.
(1)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1064   HPT Rotor Assembly Dimensions
Subtask 72-53-00-220-078
(2)Deleted.
(3)Deleted.
(4)Deleted.
Subtask 72-53-00-440-216
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
AJ.Prepare the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) for grinding as follows:
(1)Install the 11C3019   slave blade retainer on the stage 2 disk (01-130) (SIN 150B1) as follows:
(a)If not installed already, install the rubber band blade retainers to hold the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0). Refer to Subtask 72-53-00-440-212 (paragraph 3.AE.).
(b)Install the aft lift fixture of the balance tooling and align the 11C3019   slave blade retainer as follows:
1Make sure that the nut supplied with the balance tooling is still on the HPT rotor shaft.
2Install the aft lift fixture supplied with the balance tooling on the nut. Attach the handling arm supplied with the balance tooling to the aft lift fixture.
3Put the 11C3019   slave blade retainer in position with the handling arm through the center of the tool. Attach the handling arm to an overhead hoist.
NOTE:
This step lets the installation of the 11C3019   slave blade retainer, without the use of the 11C3024   assembly/disassembly fixture.
4Make sure that the 11C3019   slave blade retainer is held captive by the lift equipment and the correct side of the retaining ring (item 2) will be against the stage 2 disk when you turn the HPT rotor assembly. Refer to Figure 1068.
(c)Lift the HPT rotor assembly a sufficient amount to install the 11C3019   slave blade retainer as follows:
CAUTION:
MAKE SURE THAT THE RUBBER BAND BLADE RETAINERS ARE INSTALLED TO HOLD EACH STAGE 2 BLADE WITH STAGE 1 BLADE IN THE STAGE 2 DISK. THE BLADE RETAINER, WILL KEEP THE BLADES IN THE DISK WHEN YOU TURN THE HPT ROTOR ASSEMBLY. DAMAGE TO THE STAGE 2 BLADES CAN OCCUR IF THEY FALL FROM THE DISK.
CAUTION:
MAKE SURE THAT THE SLAVE BLADE RETAINER, 11C3019, IS AWAY FROM MOVING ENGINE AND TOOLING PARTS WHEN YOU TURN THE HPT ROTOR ASSEMBLY. DAMAGE TO TOOLING AND ENGINE HARDWARE CAN OCCUR IF THE SLAVE BLADE RETAINER, 11C3019, CATCHES ON MOVING PARTS WHEN YOU TURN THE ASSEMBLY.
1Hold the 11C3019   slave blade retainer away from tooling and engine hardware when you lift the HPT rotor assembly.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
2Lift the HPT rotor assembly until the aft end is in a position where you can install the 11C3019   slave blade retainer (aft end approximately 45 degrees up from the horizontal position).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(d)Assemble the 11C3019   slave blade retainer on the stage 2 disk. Refer to Figure 1068 and do as follows:
1Make sure that the clamps (item 11) are in the DISENGAGED position as marked on the retaining ring (item 2).
2Align the 11C3019   slave blade retainer on the stage 2 disk and turn the hand knobs (item 10) to put the clamps (item 11) in the ENGAGED position.
3Make sure that the clamps (item 11) engage the disk posts.
CAUTION:
DO NOT TIGHTEN THE CLAMPS MORE THAN 50 LB IN. (5.6 NM). DAMAGE TO THE TOOL CAN OCCUR.
4Turn the hand knobs (item 10) opposite from each other around the circumference to tighten the clamps (item 11). Tighten these at approximately the same rate.
5Lightly hit the 11C3019   slave blade retainer with a non-metallic mallet as you tighten the hand knobs (item 10).
6Continue this procedure until the 11C3019   slave blade retainer is fully against the stage 2 disk.
Subtask 72-53-00-220-218
(e)Make sure that the 11C3019   slave blade retainer is correctly installed as follows:
1Measure the distance between the 11C3019   slave blade retainer and the stage 2 disk with a 0.001 inch (0.03 mm) shim.
2Make sure that there is no gap.
3If there is a gap, remove the 11C3019   slave blade retainer and install it again.
Subtask 72-53-00-440-525
(2)Install the HPT rotor assembly in the 11C3024   assembly/disassembly fixture as follows:
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(a)Lift the HPT rotor assembly from the horizontal dolly with forward and aft lift fixtures supplied with the balance machine.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(b)Turn the HPT rotor assembly to the vertical position, aft end down.
(c)Remove the handling arm and aft lift fixture of the balance tooling.
(d)Make sure that the disk bore protector (item 10) of the 11C3024   assembly/disassembly fixture is installed. Refer to Figure 1005.
(e)Lower the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) to the 11C3024   assembly/disassembly fixture. Refer to Figure 1066.
(3)Remove the balance arbor from the stage 1 disk (01-280) (SIN 150A1). Refer to the manufacturer's instructions and as follows:
(a)Remove the hardware that attaches the balance arbor to the stage 1 disk.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift the balance arbor from the stage 1 disk with the forward lift fixture and handling arm.
(4)Alternative Procedure Available. Install the 11C3032   slave blade retainer on the stage 1 disk (01-280) (SIN 150A1). Refer to Figure 1067 and do as follows:
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
(a)Put the 11C3032   slave blade retainer in dry ice for 10-15 minutes.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(b)Use the check nuts (item 4) to turn the eight clamps (item 3) to the DISENGAGED position as marked on the retaining ring (item 9).
(c)Install the 11C3032   slave blade retainer into the disk and move the clamps (item 3) to the ENGAGED position.
(d)Look through the inspection hole in the 11C3032   slave blade retainer to make sure that the clamps engage the disk posts.
CAUTION:
DO NOT TIGHTEN THE CLAMPS MORE THAN 50 LB IN. (5.6 NM). FAILURE OF THE TOOL CAN OCCUR.
(e)Turn the hand knobs (item 6), opposite from each other around the circumference, to tighten the clamps (item 3) a sufficient amount to hold the retaining ring (item 9) in position on the stage 1 disk. Tighten the hand knobs (item 6) at approximately the same rate.
CAUTION:
MAKE SURE THAT THE SLAVE BLADE RETAINER, 11C3032, IS AT AMBIENT TEMPERATURE BEFORE YOU CONTINUE TO TIGHTEN THE KNURLED KNOBS. IF THE TOOL IS TOO COLD, THE CLAMP FEET BREAK EASILY WHEN YOU FULLY TIGHTEN THE KNURLED KNOBS.
(f)Let the 11C3032   slave blade retainer go back to ambient temperature before you tighten the hand knobs (item 6) again.
(g)Lightly hit the 11C3032   slave blade retainer with a non-metallic mallet and continue to tighten the clamps (item 3).
(h)Continue this procedure until the 11C3032   slave blade retainer is fully against the stage 1 disk.
Subtask 72-53-00-440-530
(4).A.Alternative Procedure. Install the forward seal (01-250) (SIN 150A3) on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000). Refer to Subtask 72-53-00-440-240 (paragraphs 3.AS.) thru Subtask 72-53-00-440-270 (paragraph 3.AZ.).
Subtask 72-53-00-440-531
(5)Mask the HPT rotor components. Refer to Figure 1065:
(a)Use C10-021  tape or an applicable equivalent as necessary.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1065   (Sheet 1 ) HPT Rotor Masking for Grinding
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1065   (Sheet 2 ) HPT Rotor Masking for Grinding
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1065   (Sheet 3 ) HPT Rotor Masking for Grinding
Subtask 72-53-00-440-532
(6)Put the HPT rotor assembly in the 11C4537   horizontal transport dolly. Refer to Subtask 72-53-00-440-202 (paragraph 3.AA.).
Subtask 72-53-00-220-228
(7)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1069.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1066   Installation of the HPT Rotor Assembly on the Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-217
(8)Deleted.
(9)Deleted.
(10)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1067   Installation/Removal of the Slave Blade Retainer, 11C3032
Subtask 72-53-00-440-220
(11)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1068   Installation/Removal of the Slave Blade Retainer, 11C3019
Subtask 72-53-00-220-080
(a)Deleted.
Subtask 72-53-00-440-226
(12)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1069   Critical Areas of the Stage 1 Disk Aft Shaft ID Surface to Inspect Prior to Storage of HPT Rotor
Subtask 72-53-00-440-227
AK.Grind the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) as follows:
WARNING:
DO NOT BREATHE THE PARTICLES FROM GRINDING OR LET THE PARTICLES TOUCH YOU. THE PARTICLES CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT. USE LOCAL MECHANICAL EXHAUST VENTILATION OR AN APPROVED RESPIRATOR.
CAUTION:
MAKE SURE THAT THE BLADES ARE NOT INSTALLED IN DIFFERENT POSITIONS AFTER YOU GRIND THEM. IF THE BLADES ARE INSTALLED IN DIFFERENT POSITIONS, AN IMBALANCE OF THE ROTOR CAN OCCUR.
(1)Refer to the grind machine manufacturer's instructions for blade installation and grind procedures.
(2)Grind the stage 1 blades to a radius (H4R) of 15.4585-15.4615 inches (392.646-392.722 mm).
(3)Grind the stage 2 blades to a target radius (H8R) of 16.0605-16.0635 inches (407.937-408.013 mm).
NOTE:
A smaller stage 2 blade radius (H8R) is permitted if the stage 2 blade shrouds are match-ground to get the H8R clearances. Refer to TASK 72-50-00-430-801 (72-50-00, ASSEMBLY 001) and TASK 72-52-00-440-801 (72-52-99, ASSEMBLY 001).
NOTE:
Do not change the positions of the blades after you grind them.
Subtask 72-53-00-220-082
AL.Measure the H4R and H8R radii on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000). Refer to Figure 1064 and as follows:
(1)Deleted.
(2)Measure radius H4R, from the center of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) to the outer edge of the stage 1 blades (34-020 , 72-00-02) (SIN 15000) to the outer forward angel wing of the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0), as follows. Refer to Figure 1064.
(a)Measure at the outer edge of each stage 1 blade.
1Make sure that each H4R measurement is 15.4585-15.4615 inches (392.646-392.722 mm).
(b)Record the maximum radius of H4R.
Maximum radius of H4R = ________.
(c)Record the minimum radius of H4R.
Minimum radius of H4R = ________.
NOTE:
If the grinder allows it, the HPT blades can be notched at this time. Refer to Subtask 72-53-00-440-238 (paragraph 3.AQ.). When completed, continue with this procedure.
(3)Deleted.
(4)Measure radius H8R, from the center of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) to the outer edge of the stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0), as follows. Refer to Figure 1064.
(a)Measure at the outer edge of each stage 2 blade.
1Make sure that each H8R measurement is 16.0605-16.0635 inches (407.937-408.013 mm).
NOTE:
A smaller stage 2 blade radius (H8R) is permitted if the stage 2 blade shrouds are match-ground to get the H8 clearances. Refer to TASK 72-50-00-430-801 (72-50-00, ASSEMBLY 001) and TASK 72-52-00-440-801 (72-52-00, ASSEMBLY 001).
(b)Record the maximum radius of H8R.
Maximum radius of H8R = ________.
(c)Record the minimum radius of H8R.
Minimum radius of H8R = ________.
Subtask 72-53-00-440-228
AM.Put the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) aft end up on the 11C3024   assembly/disassembly fixture as follows:
(1)This procedure begins with the HPT rotor assembly in a dolly, in the horizontal position, with the balance arbor, slave race, and nut of the balance tooling installed.
(2)Attach the forward lift fixture and handling arm supplied with the balance tooling to the balance arbor. Connect the handling arm to an overhead hoist.
(3)Attach the aft lift fixture supplied with the balance tooling to the nut.
(4)Attach the handling arm to the aft lift fixture. Connect the handling arm to an overhead hoist.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(5)Lift the HPT rotor assembly from the dolly.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(6)Turn the HPT rotor assembly until it is in the vertical position, aft end up.
(7)Lower the HPT rotor assembly and remove the balance arbor. Refer to the manufacturer's instructions.
(8)Attach the stage 1 disk to the 11C3024   assembly/disassembly fixture. Refer to Subtask 72-53-00-440-146 (paragraph 3.G.).
(9)Remove the handling arm and aft lift fixture.
Subtask 72-53-00-440-229
AN.Remove the stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) from the stage 2 disk (01-130) (SIN 150B1) as follows:
(1)Remove the 11C3019   slave blade retainer from the stage 2 disk as follows. Refer to Figure 1068.
(a)Turn the hand knobs (item 10) opposite each other around the circumference to loosen the clamps (item 11).
(b)Move the hand knobs (item 10) to put the clamps (item 11) in the DISENGAGED position as shown on the retaining ring (item 2).
(c)Remove the 11C3019   slave blade retainer with the slide hammer (item 5).
(2)Put number marks on the stage 2 blades related to their positions in the stage 2 disk. Start the marks with the 1-1 slot and move CW.
(3)Remove the stage 2 blades from the stage 2 disk.
(4)Remove any grind dust from the stage 2 blades with a dry cloth. Make sure that the position marks are not removed.
(5)Put all the stage 2 blades in the 11C3015   blade container, airfoils facing down.
Subtask 72-53-00-440-230
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
AO.Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) on the 11C3024   assembly/disassembly fixture and 11C3041   clamp fixture, forward end up as follows:
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Remove the HPT rotor assembly from the 11C3024   assembly/disassembly fixture. Refer to Subtask 72-53-00-440-202 (paragraph 3.AA.(1)).
(2)Remove the nuts (item 14) and washers (item 20) from the four short studs to remove the retaining ring segments (item 24) from the aft face of the forward flange of the stage 1 disk (01-280) (SIN 150A1). Refer to Figure 1006.
(3)Install the balance arbor and forward lift fixture. Refer to Subtask 72-53-00-440-202 (paragraph (3.AA.(2)).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(4)Turn the HPT rotor assembly to the vertical position, aft end down.
(5)Remove the handling fixture and the aft lift fixture.
(6)Make sure that the bore disk protector (item 10) of the 11C3024   assembly/disassembly fixture is installed. Refer to Figure 1005.
(7)Install the table plate insert (item 5) of the 11C3041   clamp fixture on the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1070.
NOTE:
The remaining items of the 11C3041   clamp fixture are installed later in this procedure when you assemble the forward seal (150A3) on the stage 1 disk (150A1).
(a)Attach a three-legged sling to the hoist rings (item 8) on the base plate (item 2) of the 11C3041   clamp fixture.
(b)Lift the 11C3041   clamp fixture with an overhead hoist and install it on the 11C3024   assembly/disassembly fixture.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1070   Installation of the HPT Rotor Assembly on the Clamp Fixture, 11C3041, and Assembly/Disassembly Fixture, 11C3024
Subtask 72-53-00-440-236
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(8)Lower the HPT rotor assembly to the 11C3024   assembly/disassembly fixture so that the aft face of the stage 2 disk (150B1) is against the plate table insert (item 5) of the 11C3041   clamp fixture.
Subtask 72-53-00-440-237
AP.Remove the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) from the stage 1 disk (01-280) (SIN 150A1) as follows:
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Remove the balance arbor from the stage 1 disk. Refer to Subtask 72-53-00-440-217 (paragraph (3.AI.(2)).
(2)Remove the 11C3032   slave blade retainer from the stage 1 disk as follows. Refer to Figure 1067.
(a)Loosen and move the clamps (item 3) to the DISENGAGED position.
(b)Use the slide hammer puller (item 5) to remove the 11C3032   slave blade retainer.
(3)Put number marks on the stage 1 blades related to their positions in the stage 1 disk. Start the marks with the 1-1 slot and move CCW, FLA.
(4)Remove the stage 1 blades from the stage 1 disk.
CAUTION:
MAKE SURE THAT THE BLADES ARE FULLY CLEAN AFTER THE GRIND PROCEDURE. BLOCKED COOLING HOLES IN THE BLADES CAN CAUSE THE BLADES TO OVERHEAT.
(5)Remove any grind dust from the stage 1 blades with a dry cloth. Make sure that the position marks are not removed.
(6)Put all the stage 1 blades in the 11C3015   blade container, airfoils facing down.
Subtask 72-53-00-440-238
AQ.Machine tip notches in the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) as follows:
NOTE:
The tip notches could have been previously incorporated when the blade tips were machined to sized on the blade tip grind machine.
(1)Machine tip notches in the No. 1 and No. 32 stage 2 blades as follows:
(a)For position and dimensions of the tip notches for the stage 2 blades, refer to Figure 1071.
(b)Machine the two leading edge notches on the concave side of the stage 2 blades with the 11C3137G04   fixture. Refer to Figure 1071.
1Insert the grind bit (item 22) into the collet located at the front of the angle grinder (item 14). Extend the grind bit to 1.19 inches (30.2 mm) and tighten the chuck.
2Install the 11C3137G04   fixture on the HPT stage 2 rotor blade, turn the thumb screw (item 20) CCW, and fully retract it. This will let the 11C3137G04   fixture to be installed on the HPT stage 2 rotor blade.
3Turn the clamp knob (item 10) CCW to fully retract the clamping devices (item 9, 10, 12, 13, and 27).
4Put the 11C3137G04   fixture on the top of the HPT stage 2 rotor blade to let it rest on the blade bracket (item 16) straight pin.
5Put the 11C3137G04   fixture until the vertical trailing edge of the HPT stage 2 rotor blade is against the blade bracket (item 16) straight pin. The blade bracket (item 16) straight pin is opposite to the thumb screw (item 20) on the blade bracket (item 16).
6Turn the thumb screw (item 20) CW until the delrin foot (item 21) safely secures the 11C3137G04   fixture to the leading edge of the HPT stage 2 rotor blade.
7Make sure that the 11C3137G04   fixture continues on the blade bracket (item 16) straight pin.
8Turn the clamp knob (item 10) CW until the clamp foot (item 12) tightly secures the 11C3137G04   fixture into place on the HPT stage 2 rotor blade.
9Put the grind bit (item 22) closest to the blade bracket (item 16) straight pin and to the trailing edge of the HPT stage 2 rotor blade.
WARNING:
METAL PARTICLES FROM MACHINING CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT.
10Use shop supplied air to attach a female quick disconnect hose connector to the male quick disconnect hose connector on the top of the angle grinder (item 14).
11Turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22) until it barely touches the HPT stage 2 rotor blade.
12For the 0.01 inch (0.25 mm) notch, turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22), 0.01 inch (0.25 mm) past the initial point of contact with the HPT rotor blade stage 2 to create the wear notch.
13Turn the ball slide positioning stage (item 7) CW to lift the grind bit (item 22) to its original starting position and disconnect the hose from the angle grinder (item 14).
14Remove the grind bit (item 22) with two wrenches to loosen the angle grinder (item 14). Put one wrench on the collet flats of the angle grinder (item 14) and the other wrench on the flats of the grinder rotor/chuck body assembly.
15Insert the grind bit (item 29) into the collet located at the front of the angle grinder (item 14). Extend the grind bit (item 29) to 1.19 inches (30.2 mm) and tighten the angle grinder (item 14).
16Put the grind bit (item 29) closest to the leading edge of the HPT stage 2 rotor blade.
WARNING:
METAL PARTICLES FROM MACHINING CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT.
17Use shop supplied air to attach a female quick disconnect hose connector to the male quick disconnect hose connector on the top of the angle grinder (item 14).
18Turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 29) until it barely touches the HPT stage 2 rotor blade.
19For the 0.02 inch (0.51 mm) notch, turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22) 0.02 inch (0.51 mm) past the initial point of contact with the HPT stage 2 rotor blade to create the wear notch.
20Turn the ball slide positioning stage (item 7) CW to lift the grind bit (item 29) to its original starting position and disconnect the hose air supply.
21To remove the 11C3137G04   fixture turn the clamp knob (item 10) CCW until the clamp foot (item 12) is no longer in contact with the rotor assembly and remove the 11C3137G04   fixture from the HPT stage 2 rotor blade.
(2)Machine tip notches in the No. 1 and No. 32 stage 1 blades as follows:
(a)For position and dimensions of the tip notches for the stage 1 blades, refer to Figure 1072.
(b)Machine the two trailing edge notches on the convex side of the stage 1 blades with the 11C3137G03   fixture. Refer to Figure 1072.
1Insert the grind bit (item 22) into the collet located at the front of the angle grinder (item 14). Extend the grind bit to 1.19 inches (30.2 mm) and tighten the chuck.
2Install the 11C3137G03   fixture on the HPT stage 1 rotor blade, turn the thumb screw (item 20) CCW, and fully retract it. This will let the 11C3137G03   fixture to be installed on the HPT stage 1 rotor blade.
3Turn the clamp knob (item 10) CCW to fully retract the clamping devices (item 9, 10, 11, 12, and 27).
4Put the 11C3137G03   fixture on the top of the HPT stage 1 rotor blade to let it rest on the blade bracket (item 2) straight pin.
5Put the 11C3137G03   fixture until the vertical trailing edge of the HPT stage 1 rotor blade is against the blade bracket (item 2) straight pin. The blade bracket (item 2) straight pin is opposite to the thumb screw (item 20) on the blade bracket (item 2).
6Turn the thumb screw (item 20) CW until the delrin foot (item 21) safely attaches the 11C3137G03   fixture to the leading edge of the HPT stage 1 rotor blade.
7Make sure that the 11C3137G03   fixture continues on the blade bracket (item 2) straight pin.
8Turn the clamp knob (item 10) CW until the clamp foot (item 12) tightly secures the 11C3137G03   fixture into place on the HPT stage 1 rotor blade.
9Put the grind bit (item 22) closest to the blade bracket (item 2) straight pin and to the trailing edge of the HPT stage 1 rotor blade.
WARNING:
METAL PARTICLES FROM MACHINING CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT.
10Use shop supplied air to attach a female quick disconnect hose connector to the male quick disconnect hose connector on the top of the angle grinder (item 14).
11Turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22) until it barely touches the HPT stage 1 rotor blade.
12For the 0.01 inch (0.25 mm) notch, turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22), 0.01 inch (0.25 mm) past the initial point of contact with the HPT rotor blade stage 1 to create the wear notch.
13Turn the ball slide positioning stage (item 7) CW to raise the grind bit (item 22) to its original starting position and disconnect the hose from the angle grinder (item 14).
14Remove the grind bit (item 22) by using two wrenches to loosen the angle grinder (item 14). Put one wrench on the collet flats of the angle grinder (item 14) and the other wrench on the flats of the grinder rotor/chuck body assembly.
15Insert the grind bit (item 29) into the collet located at the front of the angle grinder (item 14). Extend the grind bit (item 29) to 1.19 inches (30.2 mm) and tighten the angle grinder (item 14).
16Put the grind bit (item 29) closest to the leading edge of the HPT stage 1 rotor blade.
WARNING:
METAL PARTICLES FROM MACHINING CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT.
17Use shop supplied air to attach a female quick disconnect hose connector to the male quick disconnect hose connector on the top of the angle grinder (item 14).
18Turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 29) until it barely touches the HPT stage 1 rotor blade.
19For the 0.02 inch (0.51 mm) notch, turn the micrometer thimble on the ball slide positioning stage (item 7) CCW to lower the grind bit (item 22) 0.02 inch (0.51 mm) past the initial point of contact with the HPT stage 1 rotor blade to create the wear notch.
20Turn the ball slide positioning stage (item 7) CW to raise the grind bit (item 29) to its original starting position and disconnect the hose air supply.
21To remove the 11C3137G03   fixture turn the clamp knob (item 10) CCW until the clamp foot (item 12) is no longer in contact with the rotor assembly and remove the 11C3137G03   fixture from the HPT stage 1 rotor blade.
WARNING:
METAL PARTICLES FROM MACHINING CAN CAUSE DAMAGE, INJURY, OR IRRITATION TO YOU. USE PERSONAL PROTECTION EQUIPMENT.
(3)Machine a 45 degree chamfer in the trailing edge of the No. 1 stage 1 blade. Refer to Figure 1072 for the location and dimensions of the 45 degree chamfer.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1071   (Sheet 1 ) Positions and Dimensions of the Stage 2 Blade Tip Notches
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1071   (Sheet 2 ) Positions and Dimensions of the Stage 2 Blade Tip Notches
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1072   (Sheet 1 ) Positions and Dimensions of the Stage 1 Blade Tip Notches
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1072   (Sheet 2 ) Positions and Dimensions of the Stage 1 Blade Tip Notches
Subtask 72-53-00-220-084
(4)Measure the stage 2 blade (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) notches as follows:
(a)Measure the depth of the notches of the No. 1 position blade. Refer to Figure 1071.
(b)Make a record of them as 1LE1 and 1LE2 on the Record Sheet. Refer to Figure 1073.
(c)Measure the depth of the notches of the No. 32 position blade. Refer to Figure 1071.
(d)Make a record of them as 32LE1 and 32LE2 on the Record Sheet. Refer to Figure 1073.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1073   Stage 1 and Stage 2 Blade Notches - Record Sheet
Subtask 72-53-00-220-085
(5)Measure the stage 1 blade (01-210) (SIN 150A0) or (01-211) (SIN 150A0) notches as follows:
(a)Measure the depth of the notches of the No. 1 position blade. Refer to Figure 1072.
(b)Make a record of them as 1TE1 and 1TE2 on the Record Sheet. Refer to Figure 1073.
(c)Measure the depth of the notches of the No. 32 position blade. Refer to Figure 1072.
(d)Make a record of them as 32TE1 and 32TE2 on the Record Sheet. Refer to Figure 1073.
Subtask 72-53-00-440-239
AR.Install the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and the stage 1 dampers (01-220) (SIN 150AB) into the stage 1 disk (01-280) (SIN 150A1) as follows:
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Record the serial numbers of the stage 1 blades on the Record Sheet. Refer to Figure 1074.
NOTE:
It is not necessary to record the serial numbers of the stage 1 blades in their related positions in the stage 1 disk.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
NOTE:
The rubber cement may be heat cured, but do not exceed 250° F (121° C).
(2)Apply C01-050  rubber cement to the stage 1 damper area of the stage 1 blade. Refer to Figure 1075.
(3)Install a new stage 1 damper into the concave side of each stage 1 blade platform. Do not use the old dampers again.
NOTE:
Taper side of the stage 1 dampers must face the inside of the stage 1 blades.
CAUTION:
MAKE SURE THAT THE STAGE 1 DAMPERS ARE ATTACHED TO THE STAGE 1 BLADES BEFORE THE BLADES ARE INSTALLED. AN IMBALANCE CAN OCCUR IF A STAGE 1 DAMPER IS NOT INSTALLED.
(4)Install the first stage 1 blade in the 1-1 dovetail slot of the stage 1 disk.
(5)Make sure that the leading edge of the stage 1 blade points forward.
(6)Continue this procedure to install the remaining stage 1 blades.
(7)To install the last stage 1 blade, fan the blades out on one side of the slot (move each blade axially (forward) a small distance until you can install the last blade).
(8)Push the stage 1 blades back into position.
(9)Make sure that the stage 1 blades are against the stage 1 blade retainer (01-180) (SIN 150BB).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1074   Stage 1 Blade Serial Number - Record Sheet
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1075   Installation of the Stage 1 Dampers and the Stage 1 Blades
Subtask 72-53-00-440-240
AS.Assemble the clamps (item 2) of the 11C3041   clamp fixture as follows. Refer to Figure 1076.
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Install the three hoist rings (item 8) on the top plate (item 12).
(2)Attach a three-legged sling to the hoist rings (item 8).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
BE CAREFUL WHEN YOU INSTALL THE DISK PLATE TO PREVENT DAMAGE TO THE ANGEL WINGS ON THE STAGE 1 BLADES.
(3)Lift the top table plate insert (item 5) with an overhead hoist and install it on the forward side of the stage 1 disk (150A1).
(4)Turn each clamp (item 2) as follows:
(a)Remove the ball lock pin (item 7).
(b)Remove the clamp (item 2) from the table plate insert (item 5).
(c)Turn the clamp (item 2) to put the end with the swivel screw clamp (item 9) up.
(d)Install the clamp (item 2) into the table plate insert (item 5) with the swivel screw clamp (item 9) above the top plate (item 12).
(e)Install the ball lock pin (item 7) to attach the clamp (item 2) to the table (item 3).
(f)Continue this procedure to turn the remaining clamps (item 2).
(5)Tighten the swivel screw clamp (item 9) to push the top plate (item 12).
(6)Tighten equally until the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) are 0.002 inch (0.05 mm) below the surface of the top plate (item 12).
Subtask 72-53-00-220-086
(7)Use a feeler gage to make sure that the surface of the blades is 0.002 inch (0.05 mm) below the surface of the top plate (item 12).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1076   Installation of the Clamps
Subtask 72-53-00-440-241
AT.Install the ring seal (02-260) (SIN 150N1) in the outer groove of the forward seal (01-250) (SIN 150A3) as follows. Refer to Figure 1077.
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Attach large plastic lift straps through the air holes of the forward seal at positions 180 degrees apart.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(2)Lift and turn the forward seal until the aft face is up and lower it on a work table.
(3)Cut the ring seal (02-260) (SIN 150N1) into four equal segments of 20.00 inches (508.0 mm) in length.
(4)Use a file to remove unwanted material from the ends of the ring seal (150N1) segments and make the ends square. Make sure that there are no burrs on the segments.
(5)Put a ring seal (150N1) segment into the outer groove in the aft side of the forward seal. Apply C10-012  tape to temporarily hold it in position. Then, install the next segment. Keep an end gap of 0.100-0.140 inch (2.54-3.56 mm).
(6)Repeat this procedure until all of the ring seal (02-260) (SIN 150N1) segments are installed. Cut the segments as necessary to keep an end gap of 0.100-0.140 inch (2.54-3.56 mm). Refer to Figure 1077.
(7)Mark the end gaps with C05-002  marking ink.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1077   Installation of the Ring Seals in the Forward Seal
Subtask 72-53-00-220-087
(8)Measure the distance between the ends of the ring seal (02-260) (SIN 150N1) segments as follows. Refer to Figure 1077.
(a)The distance permitted is 0.100-0.140 inch (2.54-3.56 mm).
(b)If the distance is more than 0.140 inch (3.56 mm), install a new ring seal segment.
(c)Remove a part of the ring seal segment if the distance is less than 0.100 inch (2.54 mm).
Subtask 72-53-00-440-242
(9)Remove the C10-012  tape and the ring seal (150N1) segments from the groove in the aft side of the forward seal.
WARNING:
SYNTHETIC ADHESIVE IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(10)Apply C01-027  synthetic adhesive or C01-037  synthetic adhesive in the groove of the forward seal and on the ring seal segments.
(11)Install the ring seal (150N1) segments into the outer groove in the aft side of the forward seal.
Subtask 72-53-00-220-088
(12)Make sure that the ring seal (150N1) segments are fully in the outer groove of the forward seal. Make sure that the ring seal (150N3) segments are fully in the inner groove of the forward seal.
(13)Measure the distance between the ends of the ring seal (02-260) (SIN 150N1) segments to make sure that they are 0.100-0.140 inch (2.54-3.56 mm). Refer to Figure 1077.
Subtask 72-53-00-440-243
AU.Lubricate the mating surfaces on the stage 1 disk (01-280) (SIN 150A1). Apply C02-033  lubricant to the surfaces marked Z for the stage 1 disk. Refer to Figure 1078.
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1078   Apply Soft Petrolatum to the Stage 1 Disk
Subtask 72-53-00-440-244
AV.Apply FRE161006 heat tape (115V) or FRE162006 heat tape (220V) to the stage 1 disk forward shaft as follows:
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Wind a length of FRE161006heat tape (115V) or FRE162006heat tape (220V) around the base of the forward shaft, where the shaft meets the stage 1 disk.
(2)Leave the FRE161006heat tape (115V) or FRE162006heat tape (220V) on the shaft for 20-30 minutes.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(3)Remove the FRE161006heat tape (115V) or FRE162006heat tape (220V).
Subtask 72-53-00-440-245
AW.Attach the forward seal (150A3) on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) with the 11C3002   install/remove fixture as follows:
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(1)Attach the disk adapter plate (item 70) to the stage 1 disk (01-280) (SIN 150A1) as follows. Refer to Figure 1079.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE IN A WELL-VENTILLATED AREA.
(a)Use C04-035  isopropyl alcohol and clean the forward side of the stage 1 disk (150A1).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Attach a three-legged sling to the hoist rings (item 36) on the disk adapter plate (item 70). Lift the disk adapter plate (item 70) with an overhead hoist.
(c)Align the 0 mark on the disk adapter plate (item 70) with the 1-1 slot of the stage 1 disk.
(d)Lower the disk adapter plate (item 70) to the stage 1 disk.
(e)Make sure that the dowel pin of the disk adapter plate is in stage 1 disk flange hole, aligned with the 1-1 slot.
(f)Install the nut channels (item 71) to the aft side of the forward flange with the captive screws (item 28) at four equally-spaced locations. Manually tighten the captive screws (item 28).
(g)Torque the captive screws (item 28) in a crisscross pattern in 20 lb ft (27 N.m) increments to 50-60 lb ft (68-81 N.m).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1079   Installation of the Disk Adapter Plate on the Stage 1 Disk
Subtask 72-53-00-440-247
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
DO THIS STEP ONLY IF YOU HAVE ENOUGH TIME TO FINISH THE INSTALLATION OF THE FORWARD SEAL. THE STAGE 1 DISK AND THE FORWARD SEAL ARE INTERFERENCE FIT PARTS. YOU MUST FULLY ASSEMBLE THEM BEFORE THEIR TEMPERATURES BECOME EQUAL, OR DAMAGE TO THE PARTS CAN OCCUR.
CAUTION:
DO NOT INCREASE THE TEMPERATURE OF THE STAGE 1 DISK MORE THAN 140°F (60°C). DAMAGE TO THE DISK CAN OCCUR.
(2)Apply FRE161006heat tape (115V) or FRE162006heat tape (220V) to the inner surface of the bore of the stage 1 disk (150A1). Increase the temperature of the bore to more than 140°F (60°C). Remove the FRE161006heat tape (115V) or FRE162006heat tape (220V).
(3)Install the 11C3002   install/remove fixture and zero it as follows:
(a)Apply C02-033  lubricant to the surfaces labeled Z on the forward seal (01-250) (SIN 150A3). Refer to Figure 1080.
(b)Put the forward seal (01-250) (SIN 150A3) on the staging table plate body (item 2) as follows. Refer to Figure 1080, and Figure 1081.
1Put the staging table plate body (item 2) on a large build table.
2Clean all of the mating surfaces of the staging table plate body (item 2) and remove the C02-033  lubricant from the indicator tips.
3Put a mark "0" in the forward side of FOS with a C05-003  marking pen.
4Find the slot at the FOS bore that is aligned with the zero (0) mark.
5Align the forward seal over the staging table plate body (item 2), aft end down.
6Make sure that the zero (0) slot at the FOS bore is engaged with the radial pin. Lower the forward seal.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1080   Forward Seal
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1081   Installation of the Forward Seal on the Staging Table Plate Body
Subtask 72-53-00-440-249
(c)Install the puller segmented ring (item 68) on the forward seal as follows. Refer to Figure 1082.
1Remove the capscrews (item 60) from the puller segmented ring (item 68) halves.
CAUTION:
BE CAREFUL WHEN YOU INSTALL THE PULLER SEGMENTED RING. YOU CAN CAUSE DAMAGE TO THE TEETH CORNERS OF THE FORWARD SEAL.
2Put the halves of the puller segmented ring (item 68) on the forward surface of the forward seal with the hook end of the puller segmented ring below the three seal teeth.
3Align the zero (0) mark of the puller segmented ring (item 68) with the zero (0) mark on the forward seal.
4Install the capscrews (item 60) into the puller segmented ring (item 68) and tighten manually.
5Put the puller segmented locator holder (item 23) in position at the slot at the zero (0) mark on the puller segmented ring (item 68).
6Move the puller segmented ring (item 68) as necessary until the puller segmented locator holder (item 23) goes freely into an air hole in the forward seal.
7Tighten the capscrews (item 60).
8Make sure that the puller segmented locator holder (item 23) moves freely into the air hole in the forward seal.
9Remove the puller segmented locator holder (item 23).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1082   Installation of the Puller Segmented Ring on the Forward Seal
Subtask 72-53-00-440-250
(d)Install the OD puller segmented ring (item 75) on the forward seal as follows. Refer to Figure 1083 and Figure 1082.
1If necessary, remove the capscrews (item 60) to disconnect the four segments of the OD puller segmented ring (item 75).
2Put each of the four segments in position to make a ring as follows:
aFind the matchmarks on the flanges of the segments that show the numbers 1, 2, 3, and 4.
bPut the segments in position so that the numbers on each pair of adjacent flanges are matched.
cMake sure that the segments are in the correct position related to the 1-1, 2-2, 3-3, or 4-4 matchmarks on the flanges.
3Align the flanges of the OD puller segmented ring (item 75) at the 3:00, 6:00, 9:00, and 12:00 o'clock positions.
4Align a 1-1 marked flanges of the OD puller segmented ring (item 75) with the zero (0) mark on the puller segmented ring (item 68) and the zero (0) mark on the forward seal.
5Install the capscrews (item 60).
6Manually tighten the capscrews (item 60) at the 3:00 and 9:00 o'clock positions only to make two half rings. Do not tighten the capscrews (item 60) at the 6:00 and 12:00 o'clock positions so that you can align the OD puller segmented ring (item 75) after you install the axial OD locator ring (item 73) later in this procedure.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1083   Installation of the OD Puller Segmented Ring on the Forward Seal
Subtask 72-53-00-440-251
(e)Install the restraint fixture assembly on the forward seal as follows. Refer to Figure 1084.
NOTE:
The restraint fixture assembly includes the restraint adapter tube (item 69), the axial OD locator ring (item 73), and the restraint plate (item 12).
1Make sure that the restraint adapter tube (item 69), the axial OD locator ring (item 73), and the restraint plate (item 12) are assembled.
2If necessary, tighten the capscrews (item 65) until the restraint plate legs (item 15) are against the restraint plate (item 12).
3Make sure that the eight lock screws (item 17) do not extend through the bottom of the bolt cage blocks (item 16).
4Loosen the four jacking screws (item 35) so they do not extend through the bottom of the restraint adapter tube (item 69). If necessary, remove the restraint adapter tube.
5Attach a three-legged sling to the hoist rings (item 36) on the restraint fixture assembly.
6Remove the axial adjustment nut (item 21) from the set-up table rod (item 9).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
7Use an overhead hoist to lift the restraint fixture assembly and align it above the forward seal.
8Align the zero (0) mark on the restraint fixture assembly with the zero (0) mark on the forward seal.
9Make sure that the pin of the staging table tube (item 5) is aligned with the DISENGAGED hole of the restraint adapter tube (item 69).
10Slowly lower the restraint fixture assembly to the forward seal.
11Make sure that the tabs of the restraint plate (item 12) engage the air holes of the forward seal.
12Make sure that there is space between the head of the capscrews (item 56) and the top of the restraint plate (item 12).
13Manually tighten the capscrews (item 57) to attach the restraint plate (item 12) to the puller segmented ring (item 68).
14Manually tighten the 16 capscrews (item 60) to attach the OD puller ring segment rings (item 75) to the axial OD locator ring (item 73). If necessary, turn the OD puller ring segment rings (item 75) to align with the axial OD locator ring (item 73).
15Tighten the eight capscrews (item 60) on the marked flanges of the OD puller ring segment rings (item 75). Torque the capscrews to 10 lb ft (13 N.m).
16Torque the 16 capscrews (item 60) on the top of the axial OD locator ring (item 73) in 15 lb ft (20 N.m) increments in a crisscross pattern until the OD puller ring segment rings (item 75) is fully against the axial OD locator ring (item 73).
17Install the axial adjustment nut (item 21) on the puller rod (item 9). Torque the axial adjustment nut to 75-100 lb ft (101-135 N.m).
18Tighten the eight capscrews (item 57) that hold the puller segment rings (item 68). Torque the capscrews to 10 lb ft (13 N.m).
19Make sure a 0.002 inch (0.05 mm) shim will go between the forward outer seal and the staging table outer ring (item 66).
20Remove the axial adjustment nut (item 21) from the puller rod (item 9).
21Put a 0.005 inch (0.13 mm) shim between the bottom of the eight capscrews (item 56) heads and the restraint plate (item 12). If clearance is not correct, remove the eight lock screws (item 17). Adjust the eight locking screws (item 56) until the clearance is 0.005 inch (0.13 mm). Install the eight lock screws (item 17).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1084   (Sheet 1 ) Installation of the Install/Remove Fixture, 11C3002, on the Forward Seal
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1084   (Sheet 2 ) Installation of the Install/Remove Fixture, 11C3002, on the Forward Seal
Subtask 72-53-00-440-252
(4)Install the forward seal on the stage 1 disk (01-280) (SIN 150A1) as follows. Refer to Figure 1085.
CAUTION:
MAKE SURE THAT ALL OF THE TOOLS NECESSARY FOR INSTALLATION OF THE FORWARD SEAL ARE PREPARED FOR USE BEFORE YOU REMOVE THE FORWARD SEAL FROM THE DRY ICE OR IF YOU USE LIQUID NITROGEN. IF THE TEMPERATURE OF THE FORWARD SEAL INCREASES, THE SEAL WILL EXPAND AND IT WILL NOT FIT CORRECTLY ON THE STAGE 1 DISK.
(a)Make sure that you have all of the necessary tools prepared for the installation of the forward seal before you continue with this procedure.
(b)Make sure that the temperature at the ID disk rabbet of the forward end of the stage 1 disk is not more than 140°F (60°C).
(c)Attach a three-legged sling to the hoist rings (item 36) on the restraint plate (item 12).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(d)Lift the forward seal from the staging table plate body (item 2) of the 11C3002   install/remove fixture.
Subtask 72-53-00-440-300
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
(e)Alternative Procedure Available. Decrease the temperature of the forward seal with dry ice and install it on the stage 1 disk as follows:
CAUTION:
DO NOT FREEZE THE FORWARD SEAL FOR MORE THAN 60 MINUTES. LONGER FREEZING TIME CAN CAUSE INTERFERENCE BETWEEN THE ID OF TOOLING AND THE OD OF THE STAGE 1 DISK SHAFT.
1Lower the forward seal into dry ice for a maximum of 30 minutes. Do not let frost collect on the forward seal or tooling.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
2Lift the forward seal from the dry ice.
Subtask 72-53-00-220-122
3Examine the forward seal and stage 1 disk as follows:
aMake sure that the rabbet diameters on the forward seal are clean.
bMake sure that the ring seal (150N1) segments are fully seated in the grooves on the aft side of the forward seal.
cMake sure that the rabbet diameters on the stage 1 disk are clean.
Subtask 72-53-00-440-301
4Align the forward seal above the stage 1 disk so that the 0 mark on the restraint fixture assembly is aligned with the 0 mark on the disk adapter plate (item 26).
5If necessary, adjust the position of the clamps (item 2) of the 11C3041   clamp fixture so that they do not catch on the OD puller segmented ring (item 75) of the 11C3002   install/remove fixture when you install the forward seal.
6Lower the forward seal to the stage 1 disk and engage the disk adapter puller rod (item 30) in the restraint adapter tube (item 69).
7Make sure that the pin of the disk adapter plate (item 26) is in the DISENGAGED hole of the restraint adapter tube (item 69).
8If you cannot engage the stage 1 disk with the forward seal, it is possible that the forward seal is too cold. Let the temperature of the forward seal increase until you can install it on the stage 1 disk.
Subtask 72-53-00-440-259
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
(e).C.Alternative Procedure. Decrease the temperature of the forward seal with liquid nitrogen and install it on the stage 1 disk as follows:
Subtask 72-53-00-220-092
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
1Examine the forward seal and stage 1 disk as follows:
aMake sure that the rabbet diameters on the forward seal are clean.
bMake sure that the ring seal (150N1) segments are fully seated in the grooves on the aft side of the forward seal.
cMake sure that the rabbet diameters on the stage 1 disk are clean.
Subtask 72-53-00-440-260
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
2Align the forward seal above the stage 1 disk so that the 0 mark on the restraint fixture assembly is aligned with the 0 mark on the disk adapter plate (item 26).
3If necessary, adjust the position of the clamps (item 2) of the 11C3041   clamp fixture so that they do not catch on the OD puller segmented ring (item 75) of the 11C3002   install/remove fixture when you install the forward seal.
4Lower the forward seal to the stage 1 disk and engage the disk adapter puller rod (item 30) in the restraint adapter tube (item 69).
5Make sure that the pin of the disk adapter plate (item 26) is aligned with the DISENGAGED hole of the restraint adapter tube (item 69).
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
6Put liquid nitrogen into the access holes in the restraint plate (item 12). Apply a sufficient quantity of liquid nitrogen for 75 percent of the 360 degree surface of the seal web. Refer to Figure 1084.
7Let the liquid nitrogen evaporate.
8Tap 360 degrees around the circumference of the restraint plate (item 12) to install the forward seal. Listen for the sound that occurs when the seal is fully installed on the stage 1 disk.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
WARNING:
NITROGEN, CAN DISPLACE OXYGEN IN ENCLOSED AREAS. USE IN WELL-VENTILATED AREA.
WARNING:
LIQUID NITROGEN, IS EXTREMELY COLD AND CAN CAUSE SEVERE LOW-TEMPERATURE BURNS. SKIN AND EYE PROTECTION IS REQUIRED TO PREVENT INJURY FROM SPLASH BURNS.
9If the forward seal is not correctly installed after the first application of liquid nitrogen, apply liquid nitrogen again to install the forward seal.
(f)Install the axial adjustment nut (item 21) on the disk adapter puller rod (item 30). Torque the axial adjustment nut (item 21) to 75-100 lb ft (101-135 N.m).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1085   (Sheet 1 ) Installation of the Forward Seal and the Install/Remove Fixture, 11C3002, on the Stage 1 Disk
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1085   (Sheet 2 ) Installation of the Forward Seal and the Install/Remove Fixture, 11C3002, on the Stage 1 Disk
Subtask 72-53-00-440-266
(f)Install the Sweeney-8112   torque multiplier as follows:
1Install the Sweeney-8112   torque multiplier anti-torque plate (item 29) on the spline adapter (item 19).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
2Install the Sweeney-8112   torque multiplier or the multiplier (4600-268A) on the anti-torque plate (item 29).
3Line up the anti torque pins on the anti-torque plate (item 29).
4Remove the big cap screws for fit the anti-rotation plate and install again the 2 big cap screws.
Subtask 72-53-00-220-093
(g)Look through the view window on the 11C3002   install/remove fixture to make sure that the forward seal bayonets are below the stage 1 disk bayonets.
Subtask 72-53-00-440-267
CAUTION:
DO NOT APPLY MORE THAN 10000 LB FT (13558 N.M) OF TORQUE. DAMAGE TO ENGINE HARDWARE CAN OCCUR.
(h)Operate the torque multiplier to turn the forward seal to a maximum of 6000 lb ft (8135 N.m) until the bayonets if the forward seal (150A3) are lined up with the bayonets on the stage 1 disk (150A1) and the alignment pin is in the ENGAGE position.
CAUTION:
DO NOT USE FORCE TO INSERT THE VERIFICATION PLUG. DAMAGE TO ENGINE HARDWARE CAN OCCUR.
(i)Use the verification plug (item 25) as a go-no-go gage to examine the alignment of the forward seal.
(5)Remove the 11C3002   install/remove fixture from the forward seal as follows:
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(a)Remove the Sweeney-8112torque multiplier.
(b)Remove the anti-torque plate (item 29).
(c)Remove the capscrews (item 57) and flat washers (item 44). Refer to Figure 1084.
(d)Remove the eight capscrews (item 57) to disconnect the ID puller segment ring (item 68) from the restraint plate (item 12).
(e)Remove the 16 capscrews (item 60) to disconnect the OD puller segmented ring (item 75) from the axial OD locator ring (item 73).
(f)Remove the axial adjustment nut (item 21) from the disk adapter puller rod (item 30). Refer to Figure 1085.
(g)Attach a three-legged sling and overhead hoist to the hoist rings (item 36) on the restraint fixture assembly.
(h) Remove the restraint fixture assembly from the forward seal.
CAUTION:
BE CAREFUL WHEN YOU REMOVE THE OD PULLER SEGMENTED RING. YOU CAN CAUSE DAMAGE TO THE TEETH CORNERS OF THE FORWARD SEAL.
(i)Remove the eight capscrews (item 60) to disconnect the segments of the OD puller segmented ring (item 75). Carefully remove the segments from the forward seal. Refer to Figure 1084.
CAUTION:
BE CAREFUL WHEN YOU REMOVE THE PULLER SEGMENTED RING. YOU CAN CAUSE DAMAGE TO THE TEETH CORNERS OF THE FORWARD SEAL.
(j)Remove the four capscrews (item 60) to disconnect the segments of the puller segmented ring (item 68). Carefully remove the segments from the forward seal.
(k)Remove the nut channels (item 71) as you adjust the capscrews (item 28) of the disk adapter plate (item 70) to the storage position. Refer to Figure 1079.
(l)Remove the disk adapter plate (item 70) from the stage 1 disk (150A1).
(6)Turn the clamps (item 2) and remove the top plate (item 12) of the 11C3041   clamp fixture  from the stage 1 disk (01-280) (SIN 150A1) as follows. Refer to Figure 1076.
(a)Loosen the swivel screw clamps (item 9) that hold the top plate (item 12).
(b)Remove the ball lock pins (item 7) that attach the clamps (item 2) to the top plate (item 12).
(c)Remove the clamps (item 2) from the base plate (item 12).
(d)Turn each of the clamps (item 2) to put the end with the swivel screw clamps (item 9) down.
(e)Install the ball lock pins (item 7).
(f)Attach a three-legged sling to the hoist rings (item 8).
(g)Lift the top plate (item 12) with an overhead hoist and remove it from the forward side of the stage 1 disk.
Subtask 72-53-00-220-094
AX.Measure dimension BB to make sure that the space between the forward seal (01-250) (SIN 150A3) and the forward shank face of each of the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) is less than 0.002 inch (0.051 mm). Refer to Figure 1086.
(1)Measure dimension BB at each of the 62 blades.
(2)Remove the forward seal (01-250) (SIN 150A3) and the stage 1 blades if the space is more than 0.002 inch (0.051 mm).
(3)Do a check that the four seal ring segments (150N2) are fully seated in the groove on the forward face of the stage 1 blade retainer (150BB).
(4)Install the forward seal (01-250) (SIN 150A3) and the stage 1 blades again.
Subtask 72-53-00-220-124
AY.Do a visual inspection of the cooling holes on the stage 1 disk (150A1) and the forward seal (150A3) to make sure that there is not unwanted material or handling damage.
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1086   Axial Seating Check of the Forward Seal
Subtask 72-53-00-440-270
AZ.Install the forward seal keys (seal keys) (01-240) (SIN 150A5) and the HPT rotor internal retaining ring (retaining ring) (01-230) (SIN 150A4) as follows. Refer to Figure 1087.
NOTE:
If Subtask 72-53-00-440-530 (paragraph 3.AJ.(4).A.) is done, this step is not required.
(1)Install the four seal keys (150A5) in the correct position 90 degrees apart as follows:
(a)Put one seal key (150A5) in any slot.
(b)Move CCW 15 slots and put in the next seal key (150A5).
(c)Move CCW 14 slots and put in the next seal key (150A5).
(d)Move 15 slots CCW and put in the last seal key (150A5).
(2)Measure the distance (CE) from the most forward surface of the seal keys to the lip on the forward seal (01-250) (SIN 150A3). Check the distance is not less than 0.000 inch (0.00 mm). Refer to Figure 1087.
CAUTION:
MAKE SURE THAT THE INTERNAL RETAINING RING IS CORRECTLY INSTALLED, NOT INSIDE OUT. DAMAGE TO THE ENGINE CAN OCCUR.
(3)Install the retaining ring (150A4).
(4)Make sure that the retaining ring (150A4) is installed correctly installed in the groove with all of the bayonets on top of the seal keys and that the edges are smooth and not separated.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1087   Installation of the Seal Keys and the Retaining Ring
Subtask 72-53-00-220-096
(5)Make sure that the tabs are still engaged in the slots after the retaining ring (150A4) is installed.
Subtask 72-53-00-440-272
BA.Install the front shaft damper sleeve (damper sleeve) (01-270) (SIN 150A6) into the stage 1 disk (01-280) (SIN 150A1) as follows. Refer to Figure 1088.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
DO NOT EXCEED 250°F (121°C) OR YOU MAY DAMAGE THE SLEEVE OR HARDWARE.
NOTE:
You can use C01-050  rubber cement to keep the damper sleeve in place and you can heat cure, but do not exceed 250°F (121°C).
(1)Compress the damper sleeve radially inward by hand.
(2)Install the damper sleeve into the inner diameter of the stage 1 disk.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1088   Installation of the Damper Sleeve in the Stage 1 Disk
Subtask 72-53-00-220-097
(3)Make sure that the damper sleeve is correctly installed over the rib on the ID of the shaft (the rib fits in the channel on the damper sleeve). Also make sure that there is a gap between the ends of the damper sleeve and that the damper sleeve is not creased or bent or distorted.
Subtask 72-53-00-440-273
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
BB.Turn the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) aft end up in the 11C3024   assembly/disassembly fixture as follows:
(1)Install the 11C3060   lift/turn fixture on the forward end of the HPT rotor assembly.
(2)Install the 11C3056   lift fixture on the aft end of the HPT rotor assembly.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(3)Lift the HPT rotor assembly from the 11C3024   assembly/disassembly fixture.
(4)Make sure that the nut supplied with the balance tooling is still on the HPT rotor shaft.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(5)Turn the HPT rotor assembly to the vertical position, aft end up.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(6)Use C04-035  isopropyl alcohol and clean the mate surface of the balance arbor and the forward end of the HPT rotor shaft.
(7)Put the alignment pin in the hole at the 1-1 position on the balance arbor.
(8)Wrap eitherFRE161006Heat Tape (115 v) orFRE162006Heat Tape (220 v) around the balance arbor. Increase the temperature of the balance arbor to approximately 200° F (93° C). Refer to the manufacturer's instructions for the maximum temperature permitted.
(9)Lower the stage 1 disk (150A1) forward flange on to the balance arbor and align the scribe mark on the balance arbor and the 1-1 slot on the stage 1 disk.
(10)Install the slave bolts (15020) through the forward flange and into the balance arbor and secure with the slave nuts.
(11)Torque the nuts to 200-300 lb in. (22.6-33.9 N.m) in a crisscross pattern.
(12)After the temperature of the balance arbor returns to room temperature torque the nuts again to 200-300 lb in. (22.6-33.9 N.m) in a crisscross pattern.
Subtask 72-53-00-440-274
BC.Install the stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0) and the stage 2 dampers (01-120) (SIN 150B8) into the stage 2 disk (01-130) (SIN 150B1) as follows:
(1)Record the serial numbers of the stage 2 blades in their related positions in the stage 2 disk on the Record Sheet. Refer to Figure 1089.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
NOTE:
The rubber cement may be heat cured, but do not exceed 250° F (121° C).
(2)Apply C01-050  rubber cement to the stage 2 damper area of the stage 2 blade. Refer to Figure 1090.
(3)Install a new stage 2 damper into the concave side of each stage 2 blade platform. Do not use the old dampers again.
NOTE:
Taper side of the stage 2 dampers must face the inside of the stage 2 blades.
CAUTION:
MAKE SURE THAT THE STAGE 2 DAMPERS ARE ATTACHED TO THE STAGE 2 BLADES BEFORE THE BLADES ARE INSTALLED. AN IMBALANCE CAN OCCUR IF A STAGE 2 DAMPER IS NOT INSTALLED.
(4)Install the first stage 2 blade in the 1-1 dovetail slot of the stage 2 disk.
(5)Make sure that the leading edge of the stage 2 blade points forward.
(6)Continue this procedure to install the remaining stage 2 blades.
NOTE:
Approximately 55 blades can be installed before you need to fan them out.
(7)To install the last stage 2 blade, fan the blades out on one side of the slot (move each blade axially (aft) a small distance until you can install the last blade).
(8)Push the stage 2 blades back into position.
(9)Make sure that the stage 2 blades are against the interstage seal (150B3).
Subtask 72-53-00-440-523
(10)Alternative Procedure Available. Attach the 11C3019   slave blade retainer to the stage 2 disk (01-130) (SIN 150B1). Refer to Subtask 72-53-00-440-220 (paragraph 3.AI.(5)(e)).
Subtask 72-53-00-440-524
(10).A.Alternative Procedure. Install the rubber band blade retainers to hold the stage 1 blades (01-210) (SIN 150A0) or (01-211) (SIN 150A0) and stage 2 blades (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0). Refer to Subtask 72-53-00-440-212 (paragraph 3.AE.).
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1089   Stage 2 Blade Serial Number and Position Number Record Sheet
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1090   (Sheet 1 ) Installation of the Stage 2 Dampers and the Stage 2 Blades
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1090   (Sheet 2 ) Installation of the Stage 2 Dampers and the Stage 2 Blades
Subtask 72-53-00-440-276
BD.Lift the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) from the 11C3024   assembly/disassembly fixture and the 11C3041   clamp fixture as follows:
(1)Install the aft lift fixture and the handling arm supplied with the balance machine.
(2)Lift the HPT rotor assembly from the 11C3024   assembly/disassembly fixture. Refer to Subtask 72-53-00-440-202 (paragraph 3.AA.(1)).
(3)Remove the nuts (item 14) and washers (item 20) from the four short studs to remove the retaining ring segments (item 24) from the aft face of the forward flange of the stage 1 disk (01-280) (SIN 150A1). Refer to Figure 1006.
(4)Remove the 11C3041   clamp fixture from the 11C3024   assembly/disassembly fixture as follows. Refer to Figure 1070.
(a)Attach a three-legged sling to the hoist rings (item 8) on the table (item 3) of the 11C3041   clamp fixture.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(b)Lift the 11C3041   clamp fixture with an overhead hoist and remove it from the 11C3024   assembly/disassembly fixture.
Subtask 72-53-00-440-277
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
BE.Lower the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) on an approved dolly, forward side down.
Subtask 72-53-00-220-098
BF.Measure the axial dimensions on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) as follows. Refer to Figure 1091.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1091   HPT Rotor Axial Dimension Measurements
Subtask 72-53-00-220-099
(1)Measure the axial dimension H101R, from the forward face of the stage 1 disk (01-280) (SIN 150A1) to the forward face of the platform forward skirt of the stage 1 blade (01-210) (SIN 150A0) or (01-211) (SIN 150A0), as follows:
(a)Measure at eight equally spaced locations as follows:
1Make sure that each measurement is 13.270-13.294 inches (337.06-337.66 mm).
(b)Record the maximum dimension of H101R.
Maximum dimension of H101R = ________.
(c)Record the minimum dimension of H101R.
Minimum dimension of H101R = ________.
(2)Deleted.
(3)Measure the axial dimension H107R, from the forward face of the stage 1 disk (01-280) (SIN 150A1) to the forward face of the platform forward skirt of the stage 2 blade (01-110) (SIN 150B0), (01-111) (SIN 150B0), (01-112) (SIN 150B0), or (01-113) (SIN 150B0), as follows:
(a)Measure at eight equally spaced locations as follows:
1Make sure that each measurement is 17.948-17.988 inches (455.88-456.89 mm).
(b)Record the maximum dimension of H107R.
Maximum dimension of H107R = ________.
(c)Record the minimum dimension of H107R.
Minimum dimension of H107R = ________.
(4)Deleted.
Subtask 72-53-00-440-278
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
DO NOT INSTALL USED BOLTS. BOLTS THAT WERE TORQUED BEFORE CAN BREAK.
BG.Install the new CDP bolts (01-010) (SIN 15020) or CDP balance bolts (01-020) (SIN 15021) into the forward flange of the stage 1 disk (150A1) as follows:
(1)Lift the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) from the inspection table.
WARNING:
DELETED.
(2)Use safety equipment to work below the forward flange of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) while you install the CDP bolts/balance bolts.
(3)Install the 46 new CDP bolts or CDP balance bolts through the holes in the forward flange with the heads pointed aft. Refer to Figure 1092.
Subtask 72-53-00-220-109
(4)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1092   Installation of the CDP Bolts
Subtask 72-53-00-440-280
BH.Do a final balance of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) as follows:
(1)Install the master balance arbor for the final balance. Refer to the manufacturer's instructions and Subtask 72-53-00-440-202 (paragraph 3.AA.(2)).
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(2)Lift the forward end of the HPT rotor assembly until it is horizontal.
(3)Put the HPT rotor assembly on the balance machine. Refer to the balance machine manufacturer’s instructions for installation of the HPT rotor assembly on the balance machine.
(4)Remove the forward and aft lift fixtures.
(5)If necessary, install the 11C3012   balance and grind adapter or 11C4556   balance adapter to the aft side arbor.
(6)Refer to the balance machine manufacturer's instructions to do a final balance of the HPT rotor assembly as follows:
WARNING:
CLOSE THE COVER OF THE BALANCE MACHINE BEFORE YOU LET THE ROTOR TURN. DO NOT OPEN THE COVER UNTIL THE ROTOR STOPS. AFTER THE POWER IS TURNED OFF, THE ROTOR WILL CONTINUE TO TURN WITH SUFFICIENT MOMENTUM TO CAUSE AN INJURY OR KILL YOU.
(a)Operate the balance machine at a minimum of 700 rpm.
(b)Make a two-plane setup to read in the planes of CE and CH as shown in Figure 1093.
(c)Correct the dynamic unbalance in the planes of CE and CH to less than 40 gram inches.
CAUTION:
DO NOT INSTALL USED BOLTS. BOLTS THAT WERE TORQUED BEFORE CAN BREAK.
(d)Replace the CDP bolts (01-010) (SIN 15020) with the new CDP balance bolts (01-020) (SIN 15021) as necessary to correct the imbalance in the plane CE. Refer to Figure 1092.
(e)Make a record of the changes.
(f)Use balance weights (01-060) (SIN 150W2), (01-070) (SIN 150W1), and (01-075) (SIN 150W3) as necessary, along with bolts (01-040) (SIN 15022) to correct the imbalance in the plane CH. Refer to Figure 1093.
(g)Make a record of the changes. Refer to Figure 1042.
(h)Make a record of the final magnitude of imbalance in gram inches and the angle in degrees of each balance plane. Put an L for light or an H for heavy after the angle. Refer to Figure 1058.
  (i)Deleted.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1093   Planes CE and CH for Final Balance
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1094   Runout of Surface CF
Subtask 72-53-00-440-281
BI.Remove the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) from the balance machine. Refer to the balance machine manufacturer's instructions and as follows:
(1)Install the forward and aft lift fixtures.
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(2)Lift the HPT rotor assembly from the balance machine in the horizontal position.
Subtask 72-53-00-440-282
BJ.Remove the balance arbor from the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000). Refer to the balance arbor manufacturer's instructions and as follows:
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
CAUTION:
MAKE SURE THAT THE TOOLS ARE HINGED IN THE CORRECT DIRECTION BEFORE THE HARDWARE IS TURNED. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE TOOLS OR THE HARDWARE.
(1)Turn the HPT rotor assembly until it is in the vertical position, aft end up.
(2)Lower the HPT rotor assembly and remove the balance arbor. Refer to the manufacturer's instructions.
(3)Measure the seating location of air duct on the aft shaft of HPT rotor assembly. Measure at four equally-spaced locations. Record the average of dimension L. Refer to Figure 1095.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1095   HPT Rotor Assembly Aft Shaft Dimension
Subtask 72-53-00-440-283
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
BK.Alternative Procedure Available. Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) on the 11C3018   vertical support fixture and the 11C3037   HPTR protector on the HPT rotor as follows:
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OR FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(1)Lift the HPT rotor assembly from the balance arbor with the aft lift fixture supplied with the balance tooling.
(2)Lower the HPT rotor assembly into the 11C3018   vertical support fixture. Refer to Figure 1097.
(3)Remove the handling arm, aft lift fixture, nut, and slave race supplied with the balance tooling. Refer to the manufacturer's instructions.
Subtask 72-53-00-220-229
(4)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk and stage 2 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1096.
Subtask 72-53-00-440-527
(5)Install the 11C3037   HPTR protector on the HPT rotor assembly.
Subtask 72-53-00-440-517
CAUTION:
THIS ASSEMBLY IS A CRITICAL PROCEDURE. PROPER USE OF PROTECTIVE TOOLING AND POST ASSEMBLY INSPECTIONS MUST BE COMPLETED. REFER TO THE REQUIREMENTS OF THE ENGINE MANUAL TO MAKE SURE THAT NO DAMAGE HAS BEEN CAUSED BY THE ASSEMBLY PROCEDURE OR TOOLING.
BK.A.Alternative Procedure. Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) into the 11C4676   shipping container as follows:
WARNING:
ALWAYS USE APPROVED EQUIPMENT AND PROCEDURES TO LIFT PARTS. STAY OUT FROM BELOW LOADS. IF THE PARTS ACCIDENTALLY MOVE OF FALL, THEY CAN CAUSE AN INJURY OR KILL YOU.
(1)Lift the HPT rotor assembly from the balance arbor with the aft lift fixture supplied with the balance tooling.
(2)Lower the HPT rotor assembly into the 11C4676   shipping container.
(3)Remove the handling arm, aft lift fixture, nut, and slave race supplied with the balance tooling. Refer to the manufacturer's instructions.
Subtask 72-53-00-220-221
(4)Do a general visual inspection of the exposed surfaces of HPT rotor stage 1 disk and stage 2 disk for nicks, dents, and scratches after the removal of tooling. Refer to TASK 72-00-53-200-801 (72-00-53, INSPECTION 001 - CONFIG 01) and Figure 1096.
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1096   Critical Areas of the Stage 1 Disk Aft Shaft ID and Stage 2 Disk OD Surface to Inspect Prior to Storage of HPT Rotor
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
Figure 1097   Installation of the HPT Rotor Assembly on the HPTR Truck, 11C3018