* * * FOR ALL
TASK 72-50-00-430-801
1 . General.
A.This procedure gives instructions to assemble the high pressure turbine (HPT). Refer to Figure 1001.
B.This procedure begins with the combustor diffuser nozzle (CDN) assembly installed on the 11C3010   build-up fixture and the 11C3383   nozzle cover installed.
•
(33-019 , 72-00-02) (SIN 0010A) (SB 72-0068)
•
(33-020 , 72-00-02) (SIN 0010A)
•
(33-021 , 72-00-02) (SIN 0010A) (SB 72-0155) (CDN Assembly - PIP 2 Configuration)
•
(33-021B , 72-00-02) (SIN 0010A) (SB 72-0155) (CDN Assembly - PIP 2 Configuration).
C.All directions are aft looking forward (ALF), unless specified differently.
D.Install all the bolts with the heads up or forward, unless specified differently.
WARNING:
STODDARD SOLVENT IS TOXIC. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
E.Before you do this procedure, clean all rabbets and flanges with C04-035  isopropyl alcohol, C04-002  Stoddard solvent, or a 50-50 blend of C04-035  isopropyl alcohol and C04-228  denatured alcohol.
F.The No. 1 bolthole location is at the top vertical centerline (TVCL) line and subsequent bolthole locations are identified in numerical sequence clockwise (CW), ALF, unless specified differently.
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
 
2C80417G04
Fixture Spreader - Retaining Ring (retaining ring fixture spreader)
 
7C2015G01
Fixture, Lift/Turn - Propulsor Aft (lift/turn fixture)
 
7C2151G01
Fixture Lift-Center of Gravity, Variable
NOTE:
For use with 11C3434 during installation of HPT stage 2 nozzle assembly in horizontal only.
 
11C3010G02
Fixture, Build-Up Core Module (build-up fixture)
 
11C3015G02
Container, HPT Rotor Stage 2 Blades (blade container)
 
11C3017G02
Fixture, Install/Remove - Stage 2 Aft Blade Retainer (install/remove fixture)
 
11C3018G03
Fixture, Support - HPT Rotor, Vertical (vertical support fixture)
 
11C3019G03
Retainer, Blade - Slave, HPT Rotor, Stage 2 (slave blade retainer)
 
11C3025G04
Strongback, Lift and Turn - Super Core (strongback)
 
11C3037G01
Protector - HPT Rotor Assembly (protector)
 
11C3037G02
Protector - HPT Rotor Assembly (HPTR protector)
NOTE:
Tool 11C3037G02 is used as an alternative to 11C3037G01.
 
11C3051G01
Case, Dummy - Combustor Diffuser nozzle (CDN dummy case)
 
11C3055G03
Lock, Rotor - Aft, HPT Rotor (rotor lock)
 
11C3056G02
Fixture, Lift/Turn - HPT Rotor, Aft (lift/turn fixture)
 
11C3067G01
Fixture, Retainer - No. 4 Bearing Inner Race/Oil Scoop/Rotating Seal/Fwd Seal (retainer fixture)
 
11C3126G01
Fixture, Chill - HPT Blade Retainer, Stage 2 (chill Fixture)
 
11C3140G01
Protector - HPT Stage 2 Nozzle and Blades (protector)
 
11C3159G01
Guide, Vertical/Horizontal-TCF/Stage 2 HPT Nozzle Handling Fixture (guide)
 
11C3163G03
Adaptor, Lift TCF Horizontal/Vertical (lift adapter)
 
11C3213G01
Cover - No. 4 Bearing, Aft (cover)
 
11C3383G02
Cover, Protective-Stage 1 Nozzle-HPT (nozzle cover)
 
11C3434G01
Fixture, Lift/Turn - Horizontal/Vertical HPT Nozzle Assy Stage 2 (lift/turn fixture)
 
11C4559G01
Bracket Set, Stand Roll Over, Turbine Center Frame (bracket set)
 
11C4666G02
Container, Shipping HPT Module (shipping container)
 
9429M56G01
Stand, Build - Core Module (propulsor build stand)
 
9429M60G02
Stand, Adjustable Roll-Over - Sub Assembly (roll-over stand)
 
9429M60G03
Stand, Adjustable, Roll-Over - Sub Assembly (roll-over stand)
NOTE:
Tool 9429M60G03 is an alternative to 9429M60G02.
 
9429M68G01
Tool Set, Install/Remove - HPT Rotor Retaining Ring, Stage 2 (retaining ring tool set)
(2)Standard Tools and Equipment.
 
Description
Manufacturer
 
Induction Heater
Local Purchase
 
Three-Legged Sling
Local Purchase
(3)Locally Manufactured Tools. None.
B.Consumable Materials.
 
Code No.
Description
 
C01-027
Adhesive, Synthetic
 
C02-008
Petroleum Jelly (lubricant)
 
C02-019
Oil, Engine Lubricating (GE Spec. D50TF1) (engine oil)
 
C02-023
Oil, Engine Lubricating (MIL-PRF-23699) (engine oil)
 
C02-058
Compound, Thread Lubricating (lubricant)
 
C02-071
Anti-Seize and Lubricating Compound (lubricant)
 
C02-097
Tiolube Lubricant, Anti-Seize Compound (primary) (lubricant)
 
C04-002
Solvent, General (stoddard solvent)
 
C04-035
Solvent, General (isopropyl alcohol)
 
C04-228
Solvent, General (94-96% assay Ethanol) (denatured alcohol)
 
C05-003
Marking Pen (pen)
 
C10-021
Tape, Plastic (tape)
 
C10-154
Beeswax
 
C10-207
Swabs, Lint Free Rayon Tip (swab)
 
C10-182
Cloth, Cleaning For Aircraft Structural (cleaning cloth)
C.Referenced Procedures.
 
ATA No.
Description
 
70-14-00
Handling of Bearings
 
72-25-00
Assembly 001
 
72-30-00
Assembly 001
 
72-30-00
Assembly 002
 
72-31-00
Assembly 001
 
72-40-00
Assembly 001
 
72-51-00
Assembly 001
 
72-52-00
Assembly 001
 
72-53-00
Assembly 001
 
72-54-00
Assembly 001
D.Expendable Parts.
 
CSN
Description
 
34-030 , 72-00-02
Self-Locking Nut
 
34-290 , 72-00-02
Ring Seal
 
34-330 , 72-00-02
Bridge Plates
 
34-340 , 72-00-02
Bridge Plates
 
34-350 , 72-00-02
Bridge Plates
 
01-120 , 72-53-00
Stage 2 Blade Damper
 
02-120 , 72-53-00
Stage 2 Blade Damper
* * * FOR ALL
Figure 1001   HPT Module
3 . Procedure.
Subtask 72-50-00-430-001
A.Make sure that the CDN assembly is correctly installed on the 11C3010   build-up fixture. Refer to Figure 1002.
NOTE:
The procedure to install the CDN assembly on the 11C3010   build-up fixture is in TASK 72-40-00-440-801 (72-40-00, ASSEMBLY 001, CONFIG 01) or TASK 72-40-00-440-802 (72-40-00, ASSEMBLY 001, CONFIG 02).
(1)If the CDN assembly is not available, use the 11C3051   CDN dummy case and attach the HPT section to the CDN assembly at the end of this procedure.
(a)Install the 11C3051   CDN dummy case on the 11C3010   build-up fixture as follows. Refer to Figure 1003.
1Install one support (item 2) of the 11C3051   CDN dummy case on the 11C3010   build-up fixture with six cap screws (item 6).
2Tighten the six cap screws (item 6) until fully seated.
3Install the second support (item 2) of the 11C3051   CDN dummy case on the 11C3010   build-up fixture with six cap screws (item 6).
4Tighten the six cap screws (item 6) until fully seated.
* * * FOR ALL
Figure 1002   CDN Installed on the Build-up Fixture, 11C3010
* * * FOR ALL
Figure 1003   11C3051 CDN Dummy Case Installed on 11C3010 Build-Up Fixture
Subtask 72-50-00-430-123
B.Do not do this procedure if the 11C3051   CDN dummy case is used. Remove the 11C3383   nozzle cover from the combustor diffuser assembly (01-089 , 72-40-00) (SIN 12000) or (01-090 , 72-40-00) (SIN 12000) or (01-091 , 72-40-00) (SIN 12000) or (01-092 , 72-40-00) (SIN 12000). Refer to Figure 1004.
* * * FOR ALL
Figure 1004   Removal of the 11C3383 Nozzle Cover
Subtask 72-50-00-220-012
C.Calculate and record the clearances between the HPT stage 1 nozzle assembly (01-080 , 72-40-00) (SIN 17200) or (01-081 , 72-40-00) (SIN 17200) or (01-082 , 72-40-00) (SIN 17200) and HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) or (34-021 , 72-00-02) (SIN 15000). Refer to Figure 1005, Figure 1006, and do as follows:
NOTE:
Dimensions are calculated with measured dimensions from lower level assembly buildups. Unless otherwise noted, dimensions used in calculation must be an arithmetic average when multiple readings are taken at the module assembly step. If only one reading is recorded from the module assembly, use this value directly.
NOTE:
If the level of engine disassembly did not remove the high pressure compressor (HPC) module, the calculation of clearance limits do not apply. HPT rotor, stage 1 nozzle assembly, and stage 2 nozzle assembly must agree with the limits specified in TASK 72-53-00-440-802 (72-53-00, ASSEMBLY 001 CONFIG 01) or TASK 72-53-00-440-803 (72-53-00, ASSEMBLY 001 CONFIG 02), TASK 72-40-00-440-801 (72-400-00, ASSEMBLY 001 CONFIG 01) or TASK 72-40-00-440-802 (72-40-00, ASSEMBLY 001 CONFIG 02), and TASK 72-52-00-440-801 (72-52-00, ASSEMBLY 001 CONFIG 01) or TASK 72-52-00-440-802 (72-52-00, ASSEMBLY 001 CONFIG 02) as required by level of disassembly in each specific module.
NOTE:
If during the shop visit the workscope of the engine does not disassemble the engine modules to the level that the values used to calculate H101 in Figure 1006 can be measured, the calculation of the propulsor clearance limits that follows do not apply. HPT rotor, stage 1 nozzle assembly, and stage 2 nozzle assembly must agree with the limits specified in TASK 72-53-00-440-802 (72-53-00, ASSEMBLY 001 CONFIG 01) or TASK 72-53-00-440-803 (72-53-00, ASSEMBLY 001 CONFIG 02), TASK 72-40-00-440-801 (72-400-00, ASSEMBLY 001 CONFIG 01) or TASK 72-40-00-440-802 (72-40-00, ASSEMBLY 001 CONFIG 02), and TASK 72-52-00-440-801 (72-52-00, ASSEMBLY 001 CONFIG 01) or TASK 72-52-00-440-802 (72-52-00, ASSEMBLY 001 CONFIG 02) as required by level of disassembly in each specific module.
(1)Deleted.
(2)Deleted.
(3)Deleted.
(4)Deleted.
NOTE:
Deleted.
(5)Deleted.
(6)To calculate the axial clearance, H101 record the values that follow:
(a)Record the value for dimension V on the record sheet. Refer to TASK 72-30-00-440-801 (72-30-00, ASSEMBLY 001 CONFIG 01) or TASK 72-30-00-440-805 (72-30-00, ASSEMBLY 001 CONFIG 02).
(b)Record the value for dimension C102R on the record sheet. Refer to TASK 72-30-00-440-802 (72-30-00, ASSEMBLY 002 CONFIG 01) or TASK 72-30-00-440-804 (72-30-00, ASSEMBLY 002 CONFIG 02).
(c)Record the value for dimension H101RMIN and H101RMAX on the record sheet. Refer to TASK 72-53-00-440-802 (72-53-00, ASSEMBLY 001 CONFIG 01) or TASK 72-53-00-440-803 (72-53-00, ASSEMBLY 001 CONFIG 02).
(d)Record the value for dimension H101SMIN and H101SMAX on the record sheet. Refer to TASK 72-40-00-440-801 (72-40-00, ASSEMBLY 001 CONFIG 01) or TASK 72-40-00-440-802 (72-40-00, ASSEMBLY 001 CONFIG 02).
(e)Record the value for dimension GA on the record sheet. Refer to TASK 72-30-00-440-802 (72-30-00, ASSEMBLY 002 CONFIG 01) or TASK 72-30-00-440-804 (72-30-00, ASSEMBLY 002 CONFIG 02).
(f)Record the value for dimension E103SAVG on the record sheet. Refer to TASK 72-25-00-440-801 (72-25-00, ASSEMBLY 001).
(g)Calculate H101MIN and H101MAX on the record sheet.
NOTE:
For configuration 01 compare calculated value to limits in Subtask 72-50-00-220-012 (paragraph C.(6)(h)) and Subtask 72-50-00-220-012 (paragraph C.(6)(i)) otherwise apply limits in Subtask 72-50-00-220-012 (paragraph C.(6)(j)) and Subtask 72-50-00-220-012 (paragraph C.(6)(k)).
* * * FOR ALL
(h)Make sure that the minimum value for H101MIN is not less than 0.233 inch (5.92 mm).
(i)Make sure that the maximum value for H101MAX is not more than 0.315 inch (8.00 mm).
* * * FOR ALL
(j)Make sure that the minimum value for H101MIN is not less than 0.239 inch (6.08 mm).
(k)Make sure that the maximum value for H101MAX is not more than 0.321 inch (8.15 mm).
(7)Deleted.
(8)Deleted.
(9)Deleted.
(10)If a calculated clearance is not in tolerance, find the cause and correct before you continue to build-up the HPT module.
* * * FOR ALL
Figure 1005   HPT Rotor/Stator Clearances.
* * * FOR ALL
Figure 1006   (Sheet 1 ) Record Sheet
* * * FOR ALL
Figure 1006   (Sheet 2 ) Record Sheet
* * * FOR ALL
Figure 1006   (Sheet 3 ) Record Sheet
Subtask 72-50-00-430-116
D.Install the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) or (34-021 , 72-00-02) (SIN 15000) on the aft end of the CDN assembly or the 11C3051   CDN dummy case as follows:
Subtask 72-50-00-430-117
(1)Remove the 11C3037   protector from the HPT rotor assembly as follows. Refer to Figure 1007.
(a)Adjust the top and side hook and loop straps (item 3) of the 11C3037   protector until you can get a hold on them.
(b)Use the hook and loop straps (item 3) to lift the 11C3037   protector from the HPT rotor assembly.
(2)Remove the 11C3019   slave blade retainer from the high pressure turbine rotor (HPTR) stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1). Refer to Figure 1008 and do as follows:
(a)Turn the hand knobs (item 10) opposite each other around the circumference to loosen the clamps (item 11).
(b)Move the check nut (item 4) to put the clamps (item 11) in the DISENGAGED position as shown on the retaining ring (item 2).
(c)Thread the slide hammer puller (item 5) into one of the eight threaded holes in the retaining ring (item 2).
(d)Remove the 11C3019   slave blade retainer with the slide hammer puller (item 5). Move the slide hammer puller (item 5) to different locations on the retaining ring (item 2), as necessary, to remove the slave blade retainer.
* * * FOR ALL
Figure 1007   HPTR Protector, 11C3037, and Vertical Support Fixture, 11C3018
* * * FOR ALL
Figure 1008   Removal of the Slave Blade Retainer, 11C3019
Subtask 72-50-00-430-016
(3)Remove the stage 2 HPT rotor blades (stage 2 blades) (01-110 , 72-53-00) (SIN 150B0) or (01-111 , 72-53-00) (SIN 150B0) or (01-112 , 72-53-00) (SIN 150B0) or (01-113 , 72-53-00) (SIN 150B0) or (02-110A , 72-53-00) (SIN 150B0) with the stage 2 HPT rotor blade dampers (stage 2 dampers) (01-120 , 72-53-00) (SIN 150B8) or (02-120 , 72-53-00) (SIN 150B8) from the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1). Refer to Figure 1009 and do as follows:
(a)Make sure that you can read the number marks on the stage 2 blades related to their positions in the HPTR stage 2 disk. If not, use the C05-003  pen to put marks on the stage 2 blades related to their positions in the HPTR stage 2 disk. Start the marks with the 1-1 slot in the HPTR stage 2 disk and move CW, ALF.
(b)To remove the first stage 2 blade, move (fan out) approximately 15 blades aft in the HPTR stage 2 disk dovetail slot a small distance until you can remove the first blade.
(c)Continue to remove the stage 2 blades and stage 2 dampers from the HPTR stage 2 disk. Make sure that you do not disengage the stage 2 dampers from the stage 2 blades.
(d)Put all the stage 2 blades in the 11C3015   blade container, airfoils facing down.
* * * FOR ALL
Figure 1009   Removal of the Stage 2 Blades and the Stage 2 Dampers
Subtask 72-50-00-430-114
(4)Attach the 11C3056   lift/turn fixture to the HPT rotor assembly as follows. Refer to Figure 1010.
CAUTION:
MAKE SURE THAT THE LIFT CAP IS NOT TOO TIGHT OR THE THREADS ARE NOT CROSS-THREADED OR DAMAGE TO THE PART CAN OCCUR.
(a)Thread the lift cap (item 2) of the 11C3056   lift/turn fixture on the aft end of the HPT rotor assembly until the threads are fully engaged. Do not use force to tighten the lift cap.
(b)Connect the lift bar (item 4) of the 11C3056   lift/turn fixture to the lift cap (item 2) in the vertical position with the pin (item 6).
* * * FOR ALL
Figure 1010   Installation of the Lift Fixture, 11C3056
Subtask 72-50-00-430-112
(5)Attach the lift bar (item 4) of the 11C3056   lift/turn fixture 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.
(6)Lift the HPT rotor assembly with the 11C3056   lift/turn fixture.
(7)Find the L mark on the HPT rotor assembly outside diameter. Transfer the L mark to the inside diameter of the HPT rotor assembly. Use the C05-003  pen to put the L mark at the same circumferential location on the inside diameter of the HPT rotor assembly. Refer to Figure 1011.
NOTE:
The L mark must be visible on the inside diameter near the forward flange of the stage 1 disk to align the HPTR with the HPCR.
* * * FOR ALL
Figure 1011   Transfer “L” Mark
Subtask 72-50-00-430-113
(8)Put the HPT rotor assembly in the CDN assembly or the 11C3051   CDN dummy case, and on the build-up fixture as follows:
(a)Align the L mark on the HPT rotor with TVCL of the 11C3010   build-up fixture.
(b)Slowly lower the HPT rotor assembly into the CDN assembly or the 11C3051   CDN dummy case. Make sure that the L mark on the HPT rotor assembly is aligned with the TVCL of the 11C3010   build-up fixture.
(c)Remove the 11C3056   lift/turn fixture from the HPT rotor assembly.
Subtask 72-50-00-430-090
E.Attach the 11C3159   guide to the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1) installed in the CDN assembly or the 11C3051   CDN dummy case. Refer to Figure 1012 and do as follows:
(1)Attach an overhead hoist to the eye of the lift spring (item 3).
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 guide fixture and put the tube (item 2) over the aft end of the stage 1 HPT rotor disk.
(3)Thread the flanged end of the tube (item 2) on the aft end of the stage 1 HPT rotor disk.
(4)Put the breaker bar through the 0.515 inch (13.08 mm) diameter holes of the tube (item 2).
CAUTION:
DO NOT USE TOO MUCH FORCE TO TIGHTEN THE GUIDE FIXTURE. THE STAGE 1 HPT ROTOR DISK CAN BE DAMAGED.
(5)Use the bar to turn the tube (item 2) on the stage 1 HPT rotor disk. Do not use excessive force to install the tube.
(6)Remove the breaker bar from the tube (item 2).
* * * FOR ALL
Figure 1012   Installation of the Guide, 11C3159
Subtask 72-50-00-430-091
F.Install the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) on the CDN assembly or the 11C3051   CDN dummy case as follows:
NOTE:
If the HPT rotor interstage seal (01-170, 72-53-00) (SIN 150B3) or (02-170, 72-53-00) (SIN 150B3) is a continued time part and has not had the coating replaced with TASK 72-53-43-300-801 (72-53-43, REPAIR 001) and any of the HPT stage 2 nozzle segments (01-370, 72-52-00) (SIN 174A0) or (01-372, 72-52-00) (SIN 174A0) or (01-380, 72-52-00) (SIN 174A1) or (01-382, 72-52-00) (SIN 174A1) have new honeycomb seals, then the honeycomb must be pre-grooved with TASK 72-52-00-440-801 (72-52-00, ASSEMBLY 001, CONFIG 01) or TASK 72-52-00-440-802 (72-52-00, ASSEMBLY 001, CONFIG 02).
(1)Attach the 11C3434   lift/turn fixture on the aft end of the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400). Refer to Figure 1013 and do as follows:
(a)Attach an overhead hoist to a three-legged sling.
(b)Attach the three-legged sling to the three shackles (item 5).
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.
(c)Lift the 11C3434   lift/turn fixture and align the foot of the adapter (item 2) marked as TOP with the TVCL of the HPT stage 2 nozzle assembly.
(d)Align the offset bolthole at TVCL in the aft flange of the HPT stage 2 nozzle assemlby with the offset bolthole in the adapter (item 2) marked as TOP.
(e)Lower the 11C3434   lift/turn fixture to the aft flange of the HPT stage 2 nozzle assembly.
(f)Attach the 11C3434   lift/turn fixture to the aft flange of the HPT stage 2 nozzle assembly with the cap screws (item 6), washers (item 9), and nuts (item 7). Put the cap screw heads on the aft side of the flange and the washers and nuts on the forward side of the flange. Tighten the nuts (item 7) with a wrench.
(g)If necessary, remove the slave HPT stage 2 nozzle hardware.
* * * FOR ALL
Figure 1013   Installation of the Lift/Install Fixture, 11C3434 on the HPT Stage 2 Nozzle Assembly
Subtask 72-50-00-430-118
(2)Alternative Procedure Available. Install the HPT stage 2 nozzle assembly on the CDN assembly. Refer to Figure 1014 and do as follows:
(a)Make sure that the HPT stage 2 nozzle assembly borescope hole is aligned with the hole in the case.
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 stage 2 nozzle assembly with an overhead hoist and put it over the CDN assembly.
(c)Carefully lower the HPT stage 2 nozzle assembly and engage the 11C3159   guide with the adapter (item 2) of the 11C3434   lift/turn fixture.
(d)Align the TVCL and offset boltholes of the HPT stage 2 nozzle assembly to the TVCL and offset boltholes of the CDN assembly.
(e)Lower the HPT stage 2 nozzle assembly on the CDN assembly. Engage the bolts (12024) in the CDN assembly aft flange through the boltholes in the HPT stage 2 nozzle assembly. Make sure that the offset boltholes are aligned.
Subtask 72-50-00-430-125
(2).A.Alternative Procedure. Install the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) on the 11C3051   CDN dummy case. Refer to Figure 1014 and do 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 stage 2 nozzle assembly with an overhead hoist and put it over the 11C3051   CDN dummy case.
(b)Carefully lower the HPT stage 2 nozzle assembly and engage the 11C3159   guide with the adapter (item 2) of the 11C3434   lift/turn fixture.
(c)Align the TVCL and offset boltholes of the HPT stage 2 nozzle assembly with the TVCL and offset boltholes of the 11C3051   CDN dummy case.
(d)Lower the HPT stage 2 nozzle assembly onto the 11C3051   CDN dummy case.
(e)Use 12 cap screws (item 3), flat washers (item 4), and plain nuts (item 5) to attach HPT stage 2 nozzle assembly forward flange with the 11C3051   CDN dummy case aft flange.
(f)Tighten the nuts until HPT assembly is fully seated. Make sure the offset boltholes are aligned.
Subtask 72-50-00-430-126
(3)Remove the 11C3434   lift/turn fixture from the HPT stage 2 nozzle assembly.
(4)Remove the 11C3159   guide from the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1).
(5)Make sure that the 11C3140   protector is installed on the HPT stage 2 nozzle assembly to protect the stage 2 nozzles from damage. Refer to Figure 1015.
* * * FOR ALL
Figure 1014   (Sheet 1 ) Installation of the HPT Stage 2 Nozzle Assembly
* * * FOR ALL
Figure 1014   (Sheet 2 ) Installation of the HPT Stage 2 Nozzle Assembly
* * * FOR ALL
Figure 1015   Stage 2 protector, 11C3140
Subtask 72-50-00-430-092
G.Do not do this procedure if the 11C3051   CDN dummy case is used. Install the bridge plates and brackets on the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) and CDN assembly flanges. Refer to Figure 1016, Figure 1017, and do as follows:
(1)Start at bolthole No. 1 TVCL and in a CW direction ALF, number every ten bolthole with a C05-003  pen .
(2)Install bridge plate (34-350 , 72-00-02) (SIN 17413) from bolts 118 to 41.
(3)Install bridge plate (34-340 , 72-00-02) (SIN 17412) from bolts 42 to 85.
(4)Install bridge plate (34-330 , 72-00-02) (SIN 17411) from bolts 86 to 117.
(5)Apply C02-058 lubricant to the threads and friction surfaces of the nuts (17440).
(6)Install the 16 nuts (17440) in the boltholes No. 4-5,13-14, 34-35, 50-51, 64-65, 80-81, 94-95, and 110-111. Torque the nuts in a criss-cross pattern to 276-324 lb in. (31.2-36.6 N.m).
Subtask 72-50-00-430-128
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
(7)Install the 64 nuts (34-030 , 72-00-02) (SIN 17440) in the boltholes No. 1, 3, 6-7, 10-12, 16, 18, 21-22, 25, 29, 31, 33, 36-37, 40, 43-44, 46, 48-49, 52, 55-59, 61, 63, 66-67, 70-74, 76, 78-79, 82, 87-89, 91, 93, 96-97, 100-104, 106, 108-109, 112, 115-116, and 119.
* * * END PRE SB   75-0003( )
Subtask 72-50-00-430-129
* * * SB   75-0003( HPTACC with Brackets Reduction )
(7).A.Install the 64 nuts (34-030 , 72-00-02) (SIN 17440) in the boltholes No. 1, 3, 6-7, 10-12, 17-18, 21-23, 29, 32-33, 36-37, 40, 43-44, 46, 48-49, 52, 55-59, 61, 63, 66-67, 70-74, 76, 78-79, 82, 87-89, 91, 93, 96-97, 100-104, 106, 108-109, 112, 115-116, and 119.
* * * END SB   75-0003( )
Subtask 72-50-00-430-130
(8)Torque the all the 80 nuts in a criss-cross pattern to 368-432 lb in. (41.6-48.8 N.m)
(9)Install the brackets on the aft side of CDN assembly and HPT stage 2 nozzle assembly flanges as follows:
Subtask 72-50-00-430-131
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
(a)Install the bracket (34-060 , 72-00-02) (SIN 62119) at the boltholes No. 2 and 120 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END PRE SB   75-0003( )
Subtask 72-50-00-430-132
* * * SB   75-0003( HPTACC with Brackets Reduction )
(a).A.Install the bracket (34-071 , 72-00-02) (SIN 62119) at the boltholes No. 2 and 120 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END SB   75-0003( )
Subtask 72-50-00-430-133
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
(b)Install the eight brackets (34-080 , 72-00-02) (SIN 6211B) at the boltholes No. 8-9, 23-24, 38-39, 53-54, 68-69, 83-84, 98-99, 113-114 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END PRE SB   75-0003( )
Subtask 72-50-00-430-134
* * * SB   75-0003( HPTACC with Brackets Reduction )
(b).A.Install the seven brackets (34-091 , 72-00-02) (SIN 6211B) at the boltholes No. 8-9, 38-39, 53-54, 68-69, 83-84, 98-99, and 113-114 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END SB   75-0003( )
Subtask 72-50-00-430-135
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
(c)Install the seven brackets (34-100 , 72-00-02) (SIN 6211A) at the boltholes No. 15 and 17, 30 and 32, 45 and 47, 60 and 62, 75 and 77, 90 and 92, 105 and 107 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END PRE SB   75-0003( )
Subtask 72-50-00-430-136
* * * SB   75-0003( HPTACC with Brackets Reduction )
(c).A.Install the five brackets (34-111 , 72-00-02) (SIN 6211A) at the boltholes No. 45 and 47, 60 and 62, 75 and 77, 90 and 92, 105 and 107 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
* * * END SB   75-0003( )
Subtask 72-50-00-430-137
* * * SB   75-0003( HPTACC with Brackets Reduction )
(d)Install the HPT manifold brackets (bracket) (34-360 , 72-00-02) (SIN 6211D) at the boltholes No. 15-16 and 30-31 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
NOTE:
PRE SB 75-0003 does not require installation of brackets (34-360 , 72-00-02) (SIN 6211D).
* * * END SB   75-0003( )
Subtask 72-50-00-430-138
* * * SB   75-0003( HPTACC with Brackets Reduction )
(e)Install the HPT manifold bracket (bracket) (34-370 , 72-00-02) (SIN 6211E) at the boltholes No. 24-25 with the nuts (34-030 , 72-00-02) (SIN 17440). Hand-tighten the nuts.
NOTE:
PRE SB 75-0003 does not require installation of brackets (34-360 , 72-00-02) (SIN 6211E).
* * * END SB   75-0003( )
Subtask 72-50-00-430-139
(f)Install the 7th stage air support bracket (bracket) (61111) at the boltholes No. 19-20 with the nuts (17440). Tighten the nuts (17440) hand tight.
(g)Install the 7th stage air damper bracket (bracket) (61116) at the boltholes No. 41-42 with the nuts (17440). Tighten the nuts hand tight.
(h)Attach the support bracket (bracket) (61117) to the 7th stage air damper bracket (61116) with the bolts (61121). Torque the bolts to 106-124 lb in. (12.0-14.0 N.m).
(i)Install the 7th stage air support bracket (bracket) (6111C) at the boltholes No. 85-86 with the nuts (17440). Tighten the nuts hand tight.
(j)Install the 7th stage air support bracket (bracket) (6121N) at the boltholes No. 117-118 with the nuts (17440). Tighten the nuts hand tight.
(k)Make sure that there is no gap between the flanges. Use a 0.001 inch (0.03 mm) gauge to check the gap between the flanges.
(l)Torque all the 40 nuts (17440) in a criss-cross pattern to 368-432 lb in. (41.6-48.8 N.m).
(10)Do the final torque to all the 120 nuts (17440) in a circle pattern to 368-432 lb in. (41.6-48.8 N.m).
(11)Remove the flange markings from the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400).
* * * FOR ALL
Figure 1016   Installation of Bridge Plates on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
Figure 1017   (Sheet 1 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
* * * SB   75-0003( HPTACC with Brackets Reduction )
Figure 1017   (Sheet 2 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
Figure 1017   (Sheet 3 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
* * * SB   75-0003( HPTACC with Brackets Reduction )
Figure 1017   (Sheet 4 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
Figure 1017   (Sheet 5 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
* * * FOR ALL
Figure 1017   (Sheet 6 ) Installation of the Brackets on the CDN Assembly and HPT Stage 2 Nozzle Assembly Flanges
Subtask 72-50-00-430-093
H.Install the stage 2 blades (01-110 , 72-53-00) (SIN 150B0) or (01-111 , 72-53-00) (SIN 150B0) or (01-112 , 72-53-00) (SIN 150B0) or (01-113 , 72-53-00) (SIN 150B0) or (02-110A , 72-53-00) (SIN 150B0) in the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400). Refer to Figure 1018 and do as follows:
NOTE:
The stage 2 blades are in the 11C3015   blade container.
(1)Make sure that a stage 2 blade damper (01-120 , 72-53-00) (SIN 150B8) or (02-120 , 72-53-00) (SIN 150B8) is installed in each stage 2 blade. If necessary, install one stage 2 blade damper in the stage 2 blade as follows:
(a)Apply C10-154  beeswax in the stage 2 blade where the stage 2 blade damper) will be installed.
(b)Put the stage 2 blade damper into the stage 2 blade.
(2)Install the stage 2 blades in the stage 2 HPT rotor disk (stage 2 disk) (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1) of the HPT stage 2 nozzle assembly as follows:
NOTE:
Stage 2 blades are numbered and are installed in the HPTR stage 2 disk in the order specified.
(a)Remove the 11C3140   stage 2 protector to install the stage 2 blades.
(b)Install the stage 2 blade marked with the No. 1 in the 1-1 slot of the HPTR stage 2 disk. Be careful to make sure that the stage 2 blade dampers remain correctly installed.
(c)Continue to install the stage 2 blades in a CW direction ALF in the sequence marked on the blades.
(d)To install the last stage 2 blade, move (fan out) approximately 15 blades aft in the dovetail slot a small distance until you can install the last blade.
(e)Push all the stage 2 blades back into position.
* * * FOR ALL
Figure 1018   Installation of the Stage 2 Blades and Stage 2 Blade Dampers
Subtask 72-50-00-210-005
(3)Do a visual inspection of the stage 2 blades for correct installation of the stage 2 blade damper (01-120 , 72-53-00) (SIN 150B8) or (02-120 , 72-53-00) (SIN 150B8) as follows:
(a)Move the stage 2 blades apart and use a light source to view the stage 2 blade damper.
(b)Make sure that the stage 2 blade damper is correctly installed in the slot of the stage 2 blade. If not, remove the stage 2 blade and correct as necessary. Replace the stage 2 blade damper if damaged.
Subtask 72-50-00-430-095
I.Install the HPT rotor stage 2 blade retainer (stage 2 blade retainer) (34-270 , 72-00-02) (SIN 150B5) or (34-271 , 72-00-02) (SIN 150B5) and the ring seal (34-290 , 72-00-02) (SIN 150N4) as follows:
Subtask 72-50-00-430-096
(1)Install the ring seal in the groove of the stage 2 blade retainer as follows. Refer to Figure 1019.
(a)Install the ring seal in the groove of the stage 2 blade retainer and hold in place with the C10-021  tape.
(b)Measure the gap AW between the ends of the ring seal.
(c)Remove the ring seal from the stage 2 blade retainer, and trim as necessary to obtain a gap AW of 0.180-0.220 inch (4.57-5.89 mm).
(d)Repeat Subtask 72-50-00-430-096 (paragraph 3.I.(1)(a)) thru (paragraph 3.I.(1)(c)) as necessary to obtain the correct gap AW.
(e)Apply C01-027  adhesive in the groove of the stage 2 blade retainer.
(f)Let the C01-027  adhesive become tacky to the touch. Do not install the ring seal until the adhesive becomes tacky.
(g)When the C01-027  adhesive becomes tacky, install the ring seal in the groove of the stage 2 blade retainer.
(h)Make sure that the ring seal is flush or below the forward surface of the blade retainer in the 360 degree circumference of the groove.
(i)Hold the ring seal in the groove with the C10-021   tape.
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
(j)Let the C01-027  adhesive dry for approximately 20 minutes.
NOTE:
To dry adhesive its temperature can be increased to a maximum of 250°F (121°C).
(k)Remove the tape after the C01-027  adhesive is dry. Be careful not to detach the ring seal from the adhesive.
* * * FOR ALL
Figure 1019   Installation of the Ring Seal in the Groove of the Stage 2 Blade Retainer
Subtask 72-50-00-140-001
WARNING:
STODDARD SOLVENT IS TOXIC. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(2)Clean the lower dovetail area of the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1) where the ring seal on aft stage 2 blade retainer will touch. Use a C10-207  swab moist with the C04-035  isopropyl alcohol, C04-002  Stoddard solvent, or a 50-50 blend of C04-035  isopropyl alcohol and C04-228  denatured alcohol.
Subtask 72-50-00-640-001
(3)Lubricate the aft stage 2 blade retainer and the rear HPT rotor retainer ring (aft retainer ring) (150B7) interface areas (Surfaces AX) with the C02-008  lubricant. Refer to Figure 1020.
* * * FOR ALL
Figure 1020   (Sheet 1 ) Installation of the Stage 2 Blade Retainer
* * * FOR ALL
Figure 1020   (Sheet 2 ) Installation of the Stage 2 Blade Retainer
Subtask 72-50-00-430-097
(4)Install the aft retainer ring (34-280 , 72-00-02) (SIN 150B7) on the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1). Refer to Figure 1020 and do as follows:
(a)Install the aft retainer ring inside the hook on the aft side of the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1).
NOTE:
Put the channel of the aft retainer ring forward.
(b)Compress the aft retainer ring completely inside the hook and install a clip (item 19) of the 11C3017   install/remove fixture around each end of the aft retainer ring end gap.
NOTE:
The clip holds the aft retainer ring aft and inboard in the hook of the HPTR stage 2 disk.
(c)Install the remaining clips (item 19) around the aft retainer ring approximately 30 degrees apart.
CAUTION:
THE AFT RETAINER RING MUST BE IN THE CORRECT POSITION OR THE AFT STAGE 2 BLADE RETAINER (150B5) WILL BE DAMAGED. YOU CANNOT INSTALL THE AFT STAGE 2 BLADE RETAINER IF THE AFT RETAINER RING EXTENDS OUT FROM THE RADIAL SURFACE OF THE HOOK.
(d)Make sure that the aft retainer ring is flush or below the radial surface of the HPTR stage 2 disk hook.
(5)Install the aft stage 2 blade retainer (34-270 , 72-00-02) (SIN 150B5) or (34-271 , 72-00-02) (SIN 150B5) on the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1) as follows:
(a)Put the stage 2 blade retainer on the HPTR stage 2 disk with the ring seal (150N4) against the HPTR stage 2 disk.
(b)Tap the stage 2 blade retainer lightly with a soft mallet to engage the HPTR stage 2 disk. Make sure that you do not damage the aft retainer ring (150B7).
(c)Install the 11C3126   chill fixture on the stage 2 blade retainer (150B5) as follows. Refer to Figure 1021.
1Carefully put each half of the 11C3126   chill fixture on the aft stage 2 blade retainer.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU OR THE PARTS TOUCHED BY DRY ICE. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
2Put dry ice in the 11C3126   chill fixture.
3Let the temperature of the aft stage 2 blade retainer decrease for 20 minutes.
CAUTION:
DO NOT USE TOO MUCH FORCE TO TIGHTEN THE PUSH-PULL PLATE. THE STAGE 1 HPT ROTOR DISK CAN BE DAMAGED.
(d)Install the push/pull plate (item 4) of the 11C3017   install/remove fixture on the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1). Turn the push/pull plate (item 4) CW to install. Do not use too much force to tighten the push-pull plate (item 4). Tighten the push-pull plate (item 4) until it is tight. Refer to Figure 1022.
WARNING:
DRY ICE CAUSES LOW TEMPERATURE BURNS, AND CAN CAUSE SUFFOCATION. DO NOT LET THIS MATERIAL TOUCH YOU OR THE PARTS TOUCHED BY DRY ICE. USE PERSONAL PROTECTION EQUIPMENT. USE EYE PROTECTION.
(e)After the temperature of the aft stage 2 blade retainer was decreased for 20 minutes, remove the 11C3126   chill fixture and the dry ice.
(f)Install the base (item 17) of the 11C3017   install/remove fixture on the aft stage 2 blade retainer as follows:
1Attach an overhead hoist to the hoist rings (item 8).
2Align the cutout in the base (item 17) with the split-line gap of the aft retainer ring (150B7).
NOTE:
The cutout will give access to the 2C80417   retaining ring fixture spreader.
3Lower the base (item 17) on the aft stage 2 blade retainer (150B5). The stage 2 ring (item 16) that is attached to the base (item 17) will be on the aft stage 2 blade retainer.
(g)Attach the nut (item 14) to the shaft on the push/pull plate (item 4).
(h)Connect a hydraulic pump to the hydraulic cylinder (item 7) of the 11C3017   install/remove fixture.
(i)Put the valve on the hydraulic pump in the PUSH position.
(j)Operate the hydraulic pump three to five full strokes to remove any free movement from the 11C3017   install/remove fixture.
(k)Make sure that the stage 2 ring (item 16) of the 11C3017   install/remove fixture is aligned with the aft stage 2 blade retainer (150B5).
CAUTION:
DO NOT APPLY MORE THAN 8,500 PSIG (58605 KPA) TO THE HYDRAULIC CYLINDER (ITEM 7) OF THE 11C3017   INSTALL/REMOVE FIXTURE. THE AFT STAGE 2 BLADE RETAINER CAN BE DAMAGED.
(l)Apply up to 7,000 psig (48263 kPa gage) pressure to install the aft stage 2 blade retainer (150B5). When pressure is applied, the 11C3017   install/remove fixture puts a downward pressure on the aft stage 2 blade retainer.
(m)Remove the clips (item 19) of the 11C3017   install/remove fixture.
(n)Install the 2C80417   retaining ring fixture spreader in the holes on the ends on the aft retainer ring (150B7). Refer to Figure 1023.
(o)Adjust the tool set to move the retainer ring outward (expanded position) around the hook of the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1). This will retain the stage 2 blade retainer.
(p)Put the valve on the hydraulic pump in the PULL position.
(q)Operate the hydraulic pump three to five full strokes to release the pressure from the stage 2 blade retainer.
(r)Remove the 2C80417   retaining ring fixture spreader.
(s)Remove the nut (item 14) of the 11C3017   install/remove fixture from the shaft on the push/pull plate (item 4). Refer to Figure 1022.
(t)Attach an overhead hoist to the hoist rings (item 8) and remove the 11C3017   install/remove fixture from the propulsor assembly (30-020 , 72-00-00) (SIN 0010C) or (30-021 , 72-00-00) (SIN 0010C) or (30-022 , 72-00-00) (SIN 0010C) or (30-023 , 72-00-00) (SIN 0010C).
CAUTION:
BE CAREFUL WHEN YOU REMOVE THE PUSH/PULL PLATE (ITEM 4) FROM THE STAGE 1 HPT ROTOR DISK OR DAMAGE TO THE ROTOR DISK CAN OCCUR.
(u)Carefully remove the push/pull plate (item 4) from aft end of the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1). Turn the push/pull plate (item 4) counterclockwise (CCW) to remove.
* * * FOR ALL
Figure 1021   Installation of the chill fixture, 11C3126
* * * FOR ALL
Figure 1022   Installation of the Stage 2 Blade Retainer with the Install/Remove Fixture, 11C3017
* * * FOR ALL
Figure 1023   Installation of the Aft Retainer Ring with the Retaining Ring Set Tool, 9429M68
Subtask 72-50-00-220-011
(6)Examine the correct installation of the aft retainer ring (150B7) and the aft stage 2 blade retainer (150B5) as follows. Refer to Figure 1020.
(a)Make sure that the split-line clearance of the aft retainer ring is 0.680 inch (17.27 mm) or larger and that clearance BC is 0.001 inch (0.03 mm) or larger and as follows:
1If the split-line gap and gap BC are smaller, the aft stage 2 blade retainer is not in the correct position in the HPTR stage 2 disk (01-130 , 72-53-00) (SIN 150B1) or (02-130 , 72-53-00) (SIN 150B1) and the aft retainer ring did not expand into the groove of the stage 2 blade retainer.
(b)Use a 0.001 inch (0.03 mm) shim to measure gap BD to make sure that the aft stage 2 blade retainer is completely installed. Check gap BD around the full circumference. A maximum gap of 0.005 inch (0.13 mm) for gap BD is permitted at only two stage 2 blades.
Subtask 72-50-00-430-098
(7)If the aft retainer ring (150B7) or the aft stage 2 blade retainer (150B5) is not correctly installed, do TASK 72-50-00-030-801 (72-50-00, Disassembly 001) to remove the aft stage 2 blade retainer. Do Subtask 72-50-00-140-001 (paragraph 3.I.(2)) thru Subtask 72-50-00-220-011 (paragraph 3.H.(6)) to reinstall the stage 2 blade retainer (150B5).
Subtask 72-50-00-220-017
J.Do a visual inspection of the borescope plugs and ports. Refer to TASK 72-00-00-800-804 (72-00-00, SPECIAL PROCEDURE 004) (paragraph 5.A. and 5.B.) and Figure 1025.
Subtask 72-50-00-430-099
K.Install the stage 1 HPT stator borescope plug (stage 1 borescope plug) (17290) in the HPT stator case (174B0) as follows. Refer to Figure 1024.
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)Apply C02-097  lubricant or C02-071  lubricant to the mating surfaces and the threads of the stage 1 borescope plug.
NOTE:
To reduce the likelihood of plug seizure during removal, it is recommended to use the C02-097  lubricant.
(2)Install the stage 1 borescope plug in the HPT stator case at the 3:00 o'clock position ALF.
(3)Torque the borescope plug to 142.6 to 167.4 lb in. (16.1 to 18.9 Nm), if both borescope plug and HPT stator case are new parts. Torque the borescope plug a second time.
NOTE:
Use of penetrating oil sprayed into the locking mechanism is permitted to free/unbind the locking mechanism. This must be performed before the replacement of the plug.
(4)The maximum running torque is 15.0 lb in. (1.7 Nm), if the borescope plug or the HPT stator case are not a new part. Torque the borescope plug to 142.6 to 167.4 lb in. (16.1 to 18.9 Nm) plus the running torque. Torque the borescope plug a second time.
(5)After the plug has been torqued, do a visual inspection of the plug and make sure that the locking feature is fully engaged with the lug on the borescope boss. Also make sure that the head of the borescope plug is fully seated against the borescope boss. If one of the two conditions are not met, the ratcheting feature of the plug can be seized or locked. Apply a penetrating oil directly in between the locking ring and the head of the plug. Re-apply torque to the plug until the plug begins to rotate freely. Tighten the plug from 142.6 to 167.4 lb in. (16.1 to 18.9 Nm). Do the visual inspection again before proceeding. If the conditions above cannot be met, replace the plug. Refer to Figure 1026.
* * * FOR ALL
Figure 1024   Installation of the Borescope Plug
* * * FOR ALL
Figure 1025   HPT Borescope Plugs
* * * FOR ALL
Figure 1026   Correct/Incorrect Installation of BSI Plugs
Subtask 72-50-00-430-100
L.Install the HPT rotor sump forward seal (forward seal) (35-450 , 72-00-02) (SIN 01401) on the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1) of the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) or (34-021 , 72-00-02) (SIN 15000). Refer to Figure 1027 and do as follows:
Subtask 72-50-00-430-140
* * * SB   72-0150( Introduction of New Damper Sleeve and Forward Seal )
(1)Install the damper sleeve (35-455 , 72-00-02) (SIN 01492) to the forward seal (35-450 , 72-00-02) (SIN 01401) as follows:
NOTE:
PRE SB 72-0150 does not use this step. SB 72-0150 introduces a new damper sleeve and forward seal.
(a)Install the damper sleeve in the inner groove of the forward seal.
(b)Do an inspection for axial positioning of the damper sleeve to make sure that it is correctly installed against the forward seal ID.
* * * END SB   72-0150( )
Subtask 72-50-00-430-141
(2)Put the forward seal on the stage 1 HPT rotor disk with the part number in the aft direction.
(3)Use the 11C3067   retainer fixture to push the forward seal on the stage 1 HPT rotor as follows:
(a)Put the spacer (item 6) on the stage 1 HPT rotor shaft. Make sure that it touches the forward seal.
(b)Put the retainer nut (item 2) with the end that has the mark USE FOR RETAINING NO. 4 BRG/OIL SCOOP/FWD SEAL on the spacer (item 6).
(c)Turn the retainer nut (item 2) CW to thread the retainer on the stage 1 HPT rotor disk.
(d)Use a 0.50 inch (12.7 mm) drive in the center of the cross bar (item 4) to tighten the retainer nut (item 2). Tighten the retainer nut (item 2) until the spacer (item 6) does not move and the forward seal is in the correct position.
(4)Remove the retainer nut (item 2) and the spacer (item 6).
* * * FOR ALL
Figure 1027   (Sheet 1 ) Installation of the Forward Seal
* * * FOR ALL
Figure 1027   (Sheet 2 ) Installation of the Forward Seal
Subtask 72-50-00-220-013
(5)Measure the drop (dim AD) from the stage 1 HPT rotor aft end to the forward seal aft flange as follows. Refer to Figure 1028.
(a)Measure the drop at four equally spaced locations.
(b)Record the minimum and the maximum for dim AD. Make sure that the dimension is 3.127-3.157 inches (79.43-80.19 mm).
* * * FOR ALL
Figure 1028   Verify Installation of the Forward Seal
Subtask 72-50-00-430-101
CAUTION:
KEEP ROLLER BEARING COMPONENTS (ROLLERS, CAGES, INNER RACES, AND OUTER RACES) AS A SET BY SERIAL NUMBER. BEARINGS ARE MATCHED ASSEMBLIES. DO NOT MIX SERVICEABLE BEARING COMPONENTS WITH COMPONENTS THAT HAVE DIFFERENT SERIAL NUMBERS. BEARING COMPONENTS THAT ARE MIXED WITH DIFFERENT SERIAL NUMBERS CAN RESULT IN ENGINE FAILURE.
CAUTION:
DO NOT TOUCH THE BEARINGS WITH YOUR HANDS. WEAR CLEAN, LINT FREE GLOVES WHEN YOU HANDLE THE BEARINGS OR DAMAGE TO THE PARTS CAN OCCUR.
CAUTION:
DO NOT TOUCH THE BEARING CAGE OR ROLLER PARTS WITH THE ASSEMBLY TOOLS. DAMAGE TO THE PARTS CAN OCCUR.
M.Install the No. 4 cylindrical roller bearing (No. 4 bearing) (15-090 , 72-54-00) (SIN 01400) or (15-091 , 72-54-00) (SIN 01400) inner race on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) or (34-021 , 72-00-02) (SIN 15000). Refer to TASK 70-14-00-620-003 (HANDLING OF BEARINGS) and Figure 1029 and do as follows:
(1)Get access to the No. 4 bearing outer race in the turbine frame assembly (35-009 , 72-00-02) (SIN 92500) or (35-010 , 72-00-02) (SIN 92500) or (35-011 , 72-00-02) (SIN 92500) or (35-012 , 72-00-02) (SIN 92500) or (35-015 , 72-00-02) (SIN 92500). If necessary remove the 11C3213   cover or other covering from the bearing area.
(2)Make sure that the No. 4 bearing inner and outer race serial numbers match.
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.
(3)Use a lint free C10-182  cleaning cloth to apply a light layer of C02-019  engine oil or C02-023  engine oil on No. 4 bearing inner race and the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1) in the area where the No. 4 bearing inner race will be installed (area P).
Subtask 72-50-00-430-102
WARNING:
USE THERMAL GLOVES WHEN YOU MOVE OR TOUCH HOT OR COLD PARTS. HOT OR COLD PARTS CAN CAUSE INJURY.
CAUTION:
THE INDUCTION HEATER CAN DAMAGE ELECTRONIC DEVICES. MAKE SURE THAT NO PERSONAL PACE MAKERS OR ELECTRONIC DEVICES ARE 10 FEET (3.0 METER) FROM THE INDUCTION HEATER.
(4)Increase the temperature of the No.4 bearing inner race with an induction heater to 350°F (177°C), maximum 400°F (204°C). Use a temperature probe to check the temperature of the inner race.
CAUTION:
MAKE SURE THAT THE NO. 4 BEARING INNER RACE PULLER GROOVE IS INSTALLED IN THE AFT DIRECTION OR YOU CAN DAMAGE THE INNER RACE WHEN YOU REMOVE IT.
(5)Put the No. 4 bearing inner race on the stage 1 HPT rotor (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1) with the puller groove in the aft direction.
(6)Use the 11C3067   retainer fixture to push the No. 4 bearing inner race on the stage 1 HPT rotor as follows:
(a)Put the spacer (item 3) on the stage 1 HPT rotor shaft. Make sure that the spacer touches the inner race.
(b)Put the retainer nut (item 2) with the end that has the mark USE FOR RETAINING NO. 4 BRG/OIL SCOOP/FWD SEAL on the spacer (item 3).
(c)Turn the retainer nut (item 2) CW to thread the retainer on the stage 1 HPT rotor disk.
(d)Use a 0.50 inch (12.7 mm) drive in the center of the cross bar (item 4) to tighten the retainer nut (item 2). Tighten the retainer nut (item 2) until the spacer (item 3) does not move and the No. 4 bearing inner race is in the correct position.
(7)Let the temperature of the No. 4 bearing inner race decrease to room temperature.
(8)Remove the retainer nut (item 2) and the spacer (item 3).
Subtask 72-50-00-220-014
(9)Examine the shims to make sure that the No. 4 bearing inner race is correctly installed on the stage 1 HPT rotor shaft as follows:
(a)Use a 0.001 inch (0.03 mm) shim stock.
(b)Make sure that the shim stock cannot go between the No. 4 bearing inner race and the forward seal (01401).
(c)Examine the shims at four equally spaced locations.
* * * FOR ALL
Figure 1029   Installation of the No. 4 Bearing Inner Race
Subtask 72-50-00-430-104
N.Install the turbine frame assembly (35-009 , 72-00-02) (SIN 92500) or (35-010 , 72-00-02) (SIN 92500) or (35-011 , 72-00-02) (SIN 92500) or (35-012 , 72-00-02) (SIN 92500) or (35-015 , 72-00-02) (SIN 92500) on the propulsor assembly (30-020 , 72-00-00) (SIN 0010C) or (30-021 , 72-00-00) (SIN 0010C) or (30-022 , 72-00-00) (SIN 0010C) or (30-023 , 72-00-00) (SIN 0010C) as follows:
Subtask 72-50-00-430-122
CAUTION:
DO NOT USE TOO MUCH FORCE TO TIGHTEN THE GUIDE FIXTURE. THE STAGE 1 HPT ROTOR DISK CAN BE DAMAGED.
(1)Install the 11C3159   guide on the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1). Refer to Figure 1030.
Subtask 72-50-00-220-016
(2)Do a visual inspection of the HPT Stator Case (174B0) aft cavities for foreign object damage (FOD).
Subtask 72-50-00-430-121
(3)Install the 11C3163   lift adapter to the turbine frame assembly as follows. Refer to Figure 1031.
(a)Attach a three-legged sling to the three shackles (item 10) of the 11C3163   lift adapter.
(b)Turn the nine locating pins (item 9) so the pin points out to the disengaged 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.
(c)Lift the 11C3163   lift adapter with an overhead hoist and put it over the turbine frame assembly with the horizontal lift tube at TVCL.
NOTE:
The horizontal lift tube is used for horizontal installation of the turbine frame assembly. There is an offset bolthole near TVCL on the turbine frame assembly that must align with the offset pin in the lift adapter.
(d)Lower the lift adapter on the turbine frame assembly. Align the pins (item 18) and the locating pins (item 9) to the flange boltholes. Make sure that the offset bolthole and offset locating pin (item 9) are aligned.
(e)Rotate the nine locating pins (item 9) so the pin points inward to the engaged position.
* * * FOR ALL
Figure 1030   Installation of the Guide, 11C3159
* * * FOR ALL
Figure 1031   Installation of the Lift Adapter, 11C3163
Subtask 72-50-00-430-106
(4)Remove the turbine frame assembly from the 11C4559   bracket set installed on the 9429M60   roll-over stand as follows. Refer to Figure 1032.
CAUTION:
MAKE SURE THAT THE FLOOR LOCKS REMAIN LOCKED AT ALL TIMES UNLESS YOU MOVE THE ROLL-OVER STAND. THE ROLL-OVER STAND CASTERS DO NOT GIVE SUFFICIENT STABILITY TO PERMIT SAFE WORKING CONDITIONS.
(a)Lower the floor locks (item 69) of the 9429M60   roll-over stand until they touch the floor. The floor locks must stay in contact with the floor to prevent movement of the roll-over stand. Make sure that the roll-over stand is level.
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 turbine frame assembly to remove the weight from the 11C4559   bracket set.
(c)Remove the plain nuts (item 9) and the caps crews (item 8) of the 11C4559   bracket set from the turbine frame assembly forward flange.
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 turbine frame assembly from the 11C4559   bracket set on the 9429M60   roll-over stand.
* * * FOR ALL
Figure 1032   (Sheet 1 ) Turbine Frame Assembly in Dolly/Bracket Set
* * * FOR ALL
Figure 1032   (Sheet 2 ) Turbine Frame Assembly in Dolly/Bracket Set
Subtask 72-50-00-430-107
(5)Slowly lower the turbine frame assembly on the HPT stator case (174B0) aft flange. Carefully engage the No. 4 bearing (15-090 , 72-54-00) (SIN 01400) or (15-091 , 72-54-00) (SIN 01400) outer race with the roller assembly.
(6)Align the turbine frame assembly TVCL to the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) TVCL. Make sure that the off-set boltholes are aligned.
NOTE:
The offset boltholes are the first boltholes CCW of TVCL, ALF.
(7)Remove the 11C3163   lift adapter from the turbine frame assembly as follows. Refer to Figure 1033.
(a)Remove the six 0.375-16 UNC-3B bolts and six pins (item 18) that attach the 11C3163   lift adapter to the turbine frame assembly.
(b)Attach a three-legged sling to the three shackles (item 10) of the 11C3163   lift adapter.
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.
(c)Lift the 11C3163   lift adapter with an overhead hoist and remove it from the turbine frame assembly.
(8)Remove the 11C3159   guide from the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1).
(9)On the forward flange of the turbine frame assembly, put a number every ten boltholes with a C05-003  pen in a CW direction ALF. Refer to Figure 1034.
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.
(10)Apply C02-058  lubricant to the mating surfaces and threads on the nuts (34-200 , 72-00-02) (SIN 92540) and the bolts (34-180 , 72-00-02) (SIN 92520). Make sure that there is lubricant in the V-groove of the threads.
(11)Attach the TCF assembly (35-009 , 72-00-02) (SIN 92500) or (35-010 , 72-00-02) (SIN 92500) or (35-011 , 72-00-02) (SIN 92500) or (35-012 , 72-00-02) (SIN 92500) or (35-015 , 72-00-02) (SIN 92500) to the HPT stator case (01-490 , 72-52-00) (SIN 174B0) with 16 bolts (34-180 , 72-00-02) (SIN 92520) and 16 nuts (34-200 , 72-00-02) (SIN 92540) in the boltholes No. 1, 16, 17, 32, 33, 48, 49, 64, 65, 80, 81, 96, 97, 112, 113, and 128 with the boltheads aft. Hand-tighten the nuts.
Subtask 72-50-00-430-142
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
(12)Install the support bracket (34-230 , 72-00-02) (SIN 62110) and bracket (34-210 , 72-00-02) (SIN 62111) on the turbine frame assembly forward flange and the HPT stator case (01-490 , 72-52-00) (SIN 174B0) aft flange as follows:
NOTE:
All brackets are installed on the forward side of the flange with the bend of the bracket pointed aft.
(a)Install the bracket (34-210 , 72-00-02) (SIN 62111) in the boltholes No. 2 and 127 on the forward side of the flanges. Attach with the bolts (34-190 , 72-00-02) (SIN 92521) and nuts (34-200 , 72-00-02) (SIN 92540) with the bolthead forward. Hand-tighten the nuts.
(b)Install the 15 support brackets (34-230 , 72-00-02) (SIN 62110) on the forward side of the flanges in the boltholes No. 7 and 10, 15 and 18, 23 and 26, 31 and 34, 39 and 42, 47 and 50, 55 and 58, 63 and 66, 71 and 74, 79 and 82, 87 and 90, 95 and 98, 103 and 106, 111 and 114, 119 and 122. Attach with the bolts (34-190 , 72-00-02) (SIN 92521) and nuts (34-200 , 72-00-02) (SIN 92540) with the bolthead forward. Hand-tighten the nuts.
* * * END PRE SB   75-0003( )
Subtask 72-50-00-430-143
* * * SB   75-0003( HPTACC with Brackets Reduction )
(12).A.Install the support bracket (34-241 , 72-00-02) (SIN 62110) and bracket (34-221 , 72-00-02) (SIN 62111) on the turbine frame assembly forward flange and the HPT stator case (01-490 , 72-52-00) (SIN 174B0) aft flange. Refer to Figure 1034A and do as follows:
NOTE:
All brackets are installed on the forward side of the flange with the bend of the bracket pointed aft.
(a)Install the bracket (34-221 , 72-00-02) (SIN 62111) in the boltholes No. 2 and 127 on the forward side of the flanges.
(b)Attach the bracket (34-221 , 72-00-02) (SIN 62111) with bolts (34-190 , 72-00-02) (SIN 92521) and nuts (34-200 , 72-00-02) (92540) with the boltheads forward. Hand-tighten the nuts.
(c)Install the seven support brackets (34-241 , 72-00-02) (SIN 62110) on the forward side of the flanges in the boltholes No. 15 and 18, 31 and 34, 47 and 50, 63 and 66, 79 and 82, 95 and 98, 111 and 114.
(d)Attach the support brackets (34-241 , 72-00-02) (SIN 62110) with bolts (34-190 , 72-00-02) (SIN 92521) and nuts (34-200 , 72-00-02) (SIN 92540) with the boltheads forward. Hand-tighten the nuts.
* * * END SB   75-0003( )
Subtask 72-50-00-430-144
(13)Install the bolts (34-180 , 72-00-02) (SIN 92520) and nuts (34-200 , 72-00-02) (SIN 92540) in the remaining boltholes with the boltheads forward. Hand-tighten the nuts.
NOTE:
Borescope plug removal is required for boltholes No. 40 and 41.
(14)Torque the 16 equally spaced nuts (34-200 , 72-00-02) (SIN 92540) in a criss-cross pattern to 276-324 lb in. (31.2-36.6 N.m).
(15)Torque the 128 nuts (34-200 , 72-00-02) (SIN 92540) in a criss-cross pattern to 368-432 lb in. (41.6-48.8 N.m).
(16)Torque the 128 nuts (34-200 , 72-00-02) (SIN 92540) in a circle pattern to 368-432 lb in. (41.6-48.8 N.m).
* * * FOR ALL
Figure 1033   Installation of the Turbine Frame Assembly on HPT Stage 2 Nozzle
* * * FOR ALL
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
Figure 1034   (Sheet 1 ) HPT/Turbine Frame Assembly Flange Hardware Installation
* * * FOR ALL
* * * PRE SB   75-0003( HPTACC without Brackets Reduction )
Figure 1034   (Sheet 2 ) HPT/Turbine Frame Assembly Flange Hardware Installation
* * * FOR ALL
* * * SB   75-0003( HPTACC with Brackets Reduction )
Figure 1034A   (Sheet 1 ) HPT/Turbine Frame Assembly Flange Hardware Installation
* * * FOR ALL
* * * SB   75-0003( HPTACC with Brackets Reduction )
Figure 1034A   (Sheet 2 ) HPT/Turbine Frame Assembly Flange Hardware Installation
Subtask 72-50-00-430-108
O.Install the 11C3055   rotor lock on the aft end of the turbine frame assembly (35-009 , 72-00-02) (SIN 92500) or (35-010 , 72-00-02) (SIN 92500) or (35-011 , 72-00-02) (SIN 92500) or (35-012 , 72-00-02) (SIN 92500) or (35-015 , 72-00-02) (SIN 92500). Refer to Figure 1035 and do as follows:
(1)Install the threaded tube (item 18) as follows:
(a)Put a leverage bar through the 1.00 inch (25.4 mm) diameter holes at the aft end of the threaded tube (item 18).
(b)Thread the forward end of the threaded tube (item 18) into the aft end of the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1).
(c)Remove the leverage bar from threaded tube (item 18).
(2)Attach a lift strap to the hoist rings (item 11) on the restraint frame (item 19).
(3)Use an overhead hoist to lift the 11C3055   rotor lock and align the holes on the restraint ring of the restraint frame (item 19) with the studs on the turbine frame assembly. Lower the HPT rotor lock to the turbine frame assembly.
(4)Install the captive nuts (item 8) equally spaced on the studs of the turbine frame assembly.
(5)Torque the captive nuts (item 8) to 10 lb ft (13.56 N.m).
(6)Remove the lift strap and overhead hoist from the hoist rings (item 11).
(7)Install the axial lock nut (item 9) on the aft end of the threaded tube (item 18), but do not tighten.
(8)Put the anti-torque tube (item 3) in the threaded tube (item 18) and engage the slots in the stage 1 HPT rotor disk (01-280 , 72-53-00) (SIN 150A1) or (02-280 , 72-53-00) (SIN 150A1).
(9)Put the adapter pins (item 10) in the anti-torque tube (item 3) and thread into the restraint frame (item 19). There must be a 0.125 inch (3.18 mm) gap between the anti-torque tube (item 3) and the restraint frame (item 19) when the adapter pins (item 10) are installed.
(10)Tighten the axial locknut (item 9) with a spanner wrench.
(11)Install the two segments of the clamp ring (item 5) to the restraint frame (item 19) with 10 capscrews (item 15).
(12)Torque the capscrews (item 15) to 120 lb in (13.56 N.m).
* * * FOR ALL
Figure 1035   HPT Rotor Lock
Subtask 72-50-00-430-109
P.Install the 11C3025   strongback to the aft end of the turbine frame assembly (35-009 , 72-00-02) (SIN 92500) or (35-010 , 72-00-02) (SIN 92500) or (35-011 , 72-00-02) (SIN 92500) or (35-012 , 72-00-02) (SIN 92500) or (35-015 , 72-00-02) (SIN 92500). Refer to Figure 1036 and do as follows:
(1)Attach the 7C2015   lift/turn fixture to the 11C3025   strongback with the pins (item 3) of the 7C2015   lift/turn 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.
(2)Lift the 11C3025   strongback and align the TVCL of the strongback with the aft end of the turbine frame assembly.
(3)Carefully lower the 11C3025   strongback on the turbine frame assembly aft flange and engage the alignment pins in the flange boltholes at the 12:00 o'clock and 6:00 o'clock position.
(4)Attach the 11C3025   strongback to the turbine frame assembly aft flange with the capscrews (item 29) and washers (item 26) at 26 locations. Tighten the capscrews (item 29).
Subtask 72-50-00-430-127
Q.If the 11C3051   CDN dummy case was used, remove the HPT section from the CDN dummy case and install it on the CDN assembly 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 module buildup with the 7C2015   lift/turn fixture.
(a)Make sure that the 11C3055   rotor lock is installed.
(2)Install the CDN assembly on the 11C3010   build-up fixture. Refer to TASK 72-40-00-440-801 (72-40-00, ASSEMBLY 001).
(3)Install the HPT module buildup on the CDN assembly as follows:
(a)Find the "L" mark on the HPT rotor assembly (34-020 , 72-00-02) (SIN 15000) or (34-021 , 72-00-02) (SIN 15000) outside diameter.
(b)Align the "L" mark on the HPT rotor assembly with the TVCL of the 11C3010   build-up fixture.
(c)Slowly lower the HPT rotor assembly into the CDN assembly. Align the TVCL and off-set boltholes of the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) with the TVCL and off-set boltholes of the CDN assembly.
(d)Engage the bolts (01-060 , 72-41-00) (SIN 12024) in the CDN assembly aft flange through the boltholes in the HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400). Make sure that the off-set boltholes are aligned.
(4)Install the brackets on the CDN assembly and HPT stage 2 nozzle assembly (34-010 , 72-00-02) (SIN 17400) or (34-011 , 72-00-02) (SIN 17400) or (34-012 , 72-00-02) (SIN 17400) flange. Refer to Subtask 72-50-00-430-092 (paragraph 3.G.).
* * * FOR ALL
Figure 1036   Installation of the Strongback, 11C3025
Subtask 72-50-00-510-001
R.If the HPT module is to be transported to another facility, put the module in the 11C4666 shipping container. Refer to Figure 1037 and do as follows:
(1)Remove the container assembly cover (item 12) of the 11C4666   shipping container.
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 module and put it on the base plate (item 2) and firmly attach it with four brackets (item 13).
(3)To hold the rotor, install the plug clamp (item 8), plug base (item 9) and 0.25-20 cap screws (item 16), then install the clamp rod (item 7) into the top of the pilot post (item 4) and tighten it to hold the rotor.
(4)Put desiccant bags in the container.
(5)Install the container assembly cover (item 12) and keep it in place with the clamp assemblies P/N (9426M22P10).
* * * FOR ALL
Figure 1037   (Sheet 1 ) HPT Module Shipping Container, 11C4666
* * * FOR ALL
Figure 1037   (Sheet 2 ) HPT Module Shipping Container, 11C4666
* * * FOR ALL
Figure 1037   (Sheet 3 ) HPT Module Shipping Container, 11C4666