* * * FOR ALL
TASK 72-00-04-420-801
1 . General.
A.This procedure gives instructions to install the low pressure turbine (LPT) module assembly and mid fan shaft assembly to the propulsor module assembly (propulsor assembly). Refer to Figure 401.
Mid fan shaft assembly:
(45-010 , 72-00-02) (SIN 81000)
(45-010A , 72-00-02) (SIN 81000) - (SB 72-0114)
(45-011 , 72-00-02) (SIN 81000) - (SB 72-0040)
(45-011A , 72-00-02) (SIN 81000) - (SB 72-0114).
LPT module assembly:
(45-020 , 72-00-02) (SIN 00105)
(45-021 , 72-00-02) (SIN 00105) - SB 72-0160 (Non-rake capable configuration)
(45-022 , 72-00-02) (SIN 00105) - SB 72-0160 (Rake capable configuration).
The LPT module assembly contains:
LPT rotor/stator assembly
(01-010) (SIN 93000)
(01-010A) (SIN 93000) - (SB 72-0040).
TRF assembly:
(01-020) (SIN 94000)
(01-021) (SIN 94000) - SB 72-0160 (Non-rake capable configuration)
(01-022) (SIN 94000) - SB 72-0160 (Rake capable configuration).
Forward lock nut:
(20-330 , 72-00-02) (SIN 83006)
(20-330A , 72-00-02) (SIN 83006) - (SB 72-0114)
(20-331 , 72-00-02) (SIN 83006) - (SB 72-0232).
Spacer shim:
(20-335 , 72-00-02) (SIN 81072) - (SB 72-0425).
Propulsor assembly:
(30-020 , 72-00-00) (SIN 0010C)
(30-021 , 72-00-00) (SIN 0010C) - (SB 72-0161) (Propulsor Module - PIP2 Configuration)
(30-022 , 72-00-00) (SIN 0010C) - (SB 72-0161) (Propulsor Module - PIP2 Configuration)
(30-023 , 72-00-00) (SIN 0010C) - (SB 79-0018).
B.Make sure that personnel read this procedure and know the step-by-step instructions and special tool use before the LPT module assembly is installed.
C.This procedure begins with the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) and the compressor module assembly (33-009 , 72-00-02) (SIN 00108) or (33-010 , 72-00-02) (SIN 00108) or (33-011 , 72-00-02) (SIN 00108) or (33-012 , 72-00-02) (SIN 00108) installed in the 11C3044   engine module adapter assembly attached to the customer overhead rail system, or in the 11C3281   pedestals set. Refer to Figure 402.
D.This procedure begins with the LPT module assembly installed on the 11C3426   LPT module dolly with the 11C3280   adapter set. Refer to Figure 403.
E.This procedure begins with the 9C1147   VCG lift fixture or 11C4266   CG lift fixture and 11C3165   strongback fixture installed on the LPT module assembly.
F.Install protective covers on spare assemblies only.
G.Install all the bolts with the heads up and/or forward unless specified differently.
H.Apply the lubricants to the threads and the friction surfaces only.
I.Follow the instructions to safety parts with safety wire, safety cable, cotter pins, or tab washers. Refer to TASK 70-11-00-400-001 (FASTENER RETENTION PROCEDURES) .
WARNING:
STODDARD SOLVENT IS TOXIC. USE PERSONAL PROTECTION EQUIPMENT.
WARNING:
ACETONE IS EXPLOSIVE, AN IRRITANT, AN ALLERGEN, AND HAS POISONOUS DETERIORATION. USE VAPOR/FUME CONTROL OR USE A RESPIRATOR.
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
J.Before assembly, make sure that all rabbet and structural flange mating surfaces do not have foreign material and raised metal. If necessary, clean the parts with the C04-002  Stoddard solvent, C04-003  acetone, or C04-035  isopropyl alcohol.
K.All clock positions are aft looking forward (ALF), unless specified differently.
L.Make sure that there is no unwanted material in the assemblies of the LPT module assembly.
M.Make sure that mating parts are serviceable and have no deterioration.
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
 
9C1017G01
Remove/Install Fixture Variable CG (VCG fixture)
 
9C1147G04
Fixture, Lift Variable Center of Gravity - Fan Module, 6000 lb (2724 kg) maximum (VCG lift fixture)
 
11C3044G01
Adapter Assembly, Overhead Support - Engine Modules (engine module adapter assembly)
 
11C3057G02
Fixture, Lift/Turn - Fan Hub Frame (fan frame lift/turn fixture)
 
11C3084G03
Protector - Fan Disk Bore, Stage 1 (fan disk protector)
 
11C3165G01
Fixture, Strongback Lift, Turn and Restrain - LPT Module (strongback fixture)
 
11C3277G02
Fixture, Restrain - LP Turbine Rotor/Turbine Rear Frame (LPT restrain fixture)
 
11C3278G01
Deleted
 
11C3280G01
Adapter Set For Dolly, Low Pressure Turbine - Module/Mid Shaft (adapter set)
 
11C3281G01
Bracket Set, Support - Main Engine, TRF (TRF pedestals)
 
11C3281G02
Bracket Set, Support - Main Engine, FHF (FHF pedestals)
 
11C3281G03
Bracket Set, Support - Main Engine, TCF (TCF pedestals)
 
11C3282G01
Fixture, Guide - Low Pressure Turbine Shaft TCF (guide fixture)
 
11C3283G01
Fixture, Extension - LPT Mid Shaft (extension fixture)
 
11C3287G01
Cover, Closure Flow Test - C-Sump Carbon Seal (flow cover)
 
11C3288P01
Protector - Carbon Seal Runner (carbon runner seal protector)
 
11C3296P01
Protector, Thread/Spline - LPT Shaft, Forward (fan shaft protector)
 
11C3304G02
Fixture, Install - Forward Retainer and Lockplate (forward retainer fixture)
NOTE:
Tool 11C3304G02 is an alternative to 11C3304G03.
 
11C3304G03
Fixture, Install - Forward Retainer and Lockplate (forward retainer fixture)
 
11C3327G01
Fixture, Guide - LPT Midshaft Extension (LPT mid-shaft guide fixture)
 
11C3328G02
Tool Set, Install/Remove - No. 5 Bearing Aft Seal & Air Oil External (install/remove tool)
 
11C3329G02
Deleted.
 
11C3334G01
Fixture, Torque - No. 5 Bearing Spanner Nut (No. 5 bearing locknut torque fixture)
 
11C3421G02
Fixture Install/Remove - Fan Shaft Cover (fan shaft cover fixture)
NOTE:
This tool is used with the aft support ring removed.
 
11C3421G03
Fixture Install/Remove - Fan Shaft Cover (fan shaft cover fixture)
NOTE:
This tool is used with the aft support ring either installed or removed.
 
11C3423G02
Deleted.
 
11C3423G03
Fixture, Torque - LPT/Fan Coupling Nut (coupling nut torque fixture)
 
11C3424G01
Gage, Mid Fan Shaft to Shaft Nut (mid fan shaft gage)
 
11C3426G02
Dolly, LPT Module/Mid-Shaft (LPT module dolly)
 
11C3474P02
Guide-Installation No. 5 Bearing, Carbon Seal (No. 5 bearing carbon seal guide)
 
11C4265G01
Fixture, Torque - LP Turbine /Fan coupling Nut (coupling nut wrench)
 
11C4266G03
Fixture, Lift - Center of Gravity Low Pressure Turbine (CG lift fixture)
 
11C4271G03
Deleted.
 
11C4272G01
Fixture, Extension - LPT Mid Shaft (extension fixture)
 
11C4292G01
Fixture, Installation - Expansion, No. 5 Bearing Carbon Seal (installation fixture)
 
11C4430G02
Bracket Set, FWD Propulsor, Ground Handling and Shipping (bracket set)
 
11C4858G01
Fixture, Lift and Turn - LPT Module (use with 11C4266G03)
 
11C5003G01
Fixture, Push/Pull - LPT and Fan Modules (push/pull fixture)
 
11C5012G01
Fixture, Torque - Inner Spanner Nut (spanner nut torque fixture)
 
11C5013G01
Fixture Install/Remove - Shaft Mid Fan (installation/removal fixture)
 
9429M17G01
Plate, Anti-Torque - Sweeney Torque Multiplier (anti-torque plate)
 
9429M43G01
Adapter, Overhead Support - Fan Hub Frame (fan frame overhead adapter)
 
9429M45G01
Adapter, Overhead Support - K-Flange (K-flange overhead adapter)
 
9429M47G01
Adapter, Overhead Support - LPT (LPT support overhead adapter)
 
9429M48G01
Adapter, Overhead Support - Bridge Beam (bridge beam adapter)
 
9429M59G02
Fixture, Assembly - Breach Loader (breach loader)
 
9429M71G01
Adapter Set, Flow Check-Frames, Lube System (universal adapter kit)
 
9429M77G04
Fixture, Lift and Turn - General Purpose (lift and turn fixture)
 
9446M40G01
Fixture, LPT Alignment (LPT alignment fixture)
 
9461M40G03
Test Stand, Assembly - Lube System Airflow (air flow test stand) (115 VAC, 50-60 Hz)
 
9461M40G04
Test Stand, Assembly - Lube System Airflow (air flow test stand) (230 VAC, 50-60 Hz)
 
- -
Bumpers, TCF Aft Flange (bumper)
 
- -
Guide Pin, LPT Module to TCF (guide pin)
(2)Standard Tools and Equipment.
 
Description
Manufacturer
 
Customer Overhead Rail System
Local Purcahse
 
Hydra-Set (hydra-set)
Local Purchase
 
Micrometers (various)
Local Purchase
 
Sweeney No. 8200 Torque Multiplier (torque multiplier)
Hydratight Sweeney7330 S. Alton Way Street O Centennial, CO 80112-2311
 
Pump, Hand - Hydraulic (Capacity: 20 Ton)(hydraulic hand pump)
Local Purchase
 
Torpedo Level
Local Purchase
(3)Locally Manufactured Tools. None.
B.Consumable Materials.
 
Code No.
Description
 
C01-007
Deleted
 
C02-019
Oil, Engine Lubricating (engine oil)
 
C02-023
Oil, Engine Lubricating (engine oil)
 
C02-058
Compound, Thread Lubricating (graphite)
 
C04-002
Solvent, General (Stoddard solvent)
 
C04-003
Solvent, General, Federal Specification 0-A51 (acetone)
 
C04-035
Solvent, General (isopropyl alcohol)
 
C05-003
Marking Pens
 
C10-071
Wire, Safety
 
C10-140
Gloves, Film Latex or Nylon/Polyethylene Disposable (Latex Glove)
 
C10-143
Cable, Safety
 
C10-182
Cloth, Cleaning for Aircraft Structural (SAE-AMS 3819, BMS 15-5) (cleaning cloth)
 
--
Ice, Dry (dry ice)
 
--
Cloths, Clean
C.Referenced Procedures. Refer to Engine Manual GEK 114119 unless instructed differently.
 
ATA No.
Description
 
70-11-00
Fastener Retention Procedures
 
70-51-00
Tightening Practices and Torque Values
 
72-00-04
Assembly 001 - Configuration 01
 
72-00-04
Assembly 001 - Configuration 02
 
72-24-00
No. 2 Ball Bearing Assembly - Assembly 001
 
72-25-00
Fan Hub Module Assembly - Assembly 001
 
72-30-00
High Pressure Compressor Module Assembly - Assembly 002
 
72-41-00
Combustor Diffuser Assembly - Assembly 001
 
72-52-00
High Pressure Turbine Stage 2 Nozzle Assembly - Assembly 001
 
72-54-00
Turbine Center Frame Assembly - Assembly 001
 
72-56-00
Assembly 001 - Configuration 01
 
72-56-00
Assembly 001 - Configuration 02
D.Expendable Parts.
 
CSN
Description
 
20-300 , 72-00-02
Preformed Packing (packing)
 
20-335 , 72-00-02
Spacer Shim (shim)
 
45-120 , 72-00-02
Ring Seal
 
45-140 , 72-00-02
Ring Seal (oil seal)
 
45-200 , 72-00-02
Tiedown Strap (strap)
 
45-230 , 72-00-02
Preformed Packing
 
45-250 , 72-00-02
Preformed Packing
 
45-340 , 72-00-02
Preformed Packing
 
45-360 , 72-00-02
Seal Ring (spring seal)
 
01-270 , 72-57-00
Tiedown Strap (strap)
 
01-410 , 72-57-00
Tiedown Strap (strap)
* * * FOR ALL
Figure 401   LPT Module Assembly
* * * FOR ALL
Figure 402   Propulsor Assembly Installed in the Customer Overhead Rail System with Engine Module Adapter Assembly, 11C3044
* * * FOR ALL
Figure 403   (Sheet 1 ) LPT Module Assembly Installed in the LPT Module Dolly, 11C3426
* * * FOR ALL
Figure 403   (Sheet 2 ) LPT Module Assembly Installed in the LPT Module Dolly, 11C3426
3 . Procedure.
Subtask 72-00-04-220-026
A.Alternative procedure available. Select and calculate the dimension necessary for the correct thickness of the adjust washer (shim) (20-360 , 72-00-02) (SIN 83070). Refer to Figure 404, Figure 405, and do as follows:
NOTE:
There are nine different sizes of shim that are available. Use this procedure to find the correct size shim to use on the engine.
NOTE:
The alternative procedure uses the original shim size, if dimension R (final) was recorded before the removal of the LPT module and was found to be outside the permitted limit, the initial shim size can be adjusted until dimension R (final) is within limits when installed. Refer to Subtask 72-00-04-020-003 (72-00-04, REMOVAL 001).
(1)Record dimension E104S of the No. 2 bearing assembly (01200). Refer to TASK 72-24-00-440-801 (72-24-00, ASSEMBLY 001).
(2)Record dimension BK of the fan hub frame (FHF) assembly (10-400 , 72-25-00) (SIN 84000), or (10-401 , 72-25-00) (SIN 84000), or (10-402 , 72-25-00) (SIN 84000). Refer to TASK 72-25-00-440-801 (72-25-00, ASSEMBLY 001).
(3)Record dimension GA of the high pressure compressor (HPC) module assembly (33-009 , 72-00-02) (SIN 00108) or (33-010 , 72-00-02) (SIN 00108) or (33-011 , 72-00-02) (SIN 00108) or (33-012 , 72-00-02) (SIN 00108). 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).
(4)Record dimension H123AVG of the combustor diffuser nozzle (CDN) assembly (33-019 , 72-00-02) (SIN 0010A) or (33-020 , 72-00-02) (SIN 0010A). Refer to TASK 72-41-00-440-801 (72-41-00, ASSEMBLY 001, CONFIG 01).
(5)Record dimension H123AVG of the CDN assembly (33-021 , 72-00-02) (SIN 0010A) or (33-021B , 72-00-02) (SIN 0010A). Refer to TASK 72-41-00-440-802 (72-41-00, ASSEMBLY 001, CONFIG 02).
(6)Record dimension H125S of the HPT stage 2 nozzle assembly (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 TASK 72-52-00-440-801 (72-52-00, ASSEMBLY 001, CONFIG 01) and TASK 72-52-00-440-802 (72-52-00, ASSEMBLY 001, CONFIG 02).
(7)Record dimension H132 of the turbine center frame assembly (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). Refer to TASK 72-54-00-440-801 (72-54-00, ASSEMBLY 001, CONFIG 01) or TASK 72-54-00-440-804 (72-54-00, ASSEMBLY 001, CONFIG 02).
(8)Record dimension L01 of the LPT rotor/stator assembly (01-010) (SIN 93000). Refer to TASK 72-56-00-440-801 (72-56-00, ASSEMBLY 001 CONFIG 01).
(9)Record dimension L01 of the LPT rotor/stator assembly (01-010A) (SIN 93000). Refer to TASK 72-56-00-440-802 (72-56-00, ASSEMBLY 001, CONFIG 02).
(10)Record dimension SHL of the mid fan shaft assembly.
NOTE:
There is a mark for dimension SHL on the aft outer flange surface of the mid fan shaft assembly.
(11)Calculate the necessary thickness of the shim on the Record Sheet. Refer to Figure 405.
(12)Find the actual shim that you will use. The available shims and thicknesses are as follows:
(20-360 , 72-00-02) (SIN 83070) = 0.0984 inch (2.499 mm)
(20-370 , 72-00-02) (SIN 83070) = 0.1181 inch (3.000 mm)
(20-380 , 72-00-02) (SIN 83070) = 0.1378 inch (3.500 mm)
(20-390 , 72-00-02) (SIN 83070) = 0.1575 inch (4.000 mm)
(20-400 , 72-00-02) (SIN 83070) = 0.1772 inch (4.501 mm)
(20-410 , 72-00-02) (SIN 83070) = 0.1969 inch (5.001 mm)
(20-420 , 72-00-02) (SIN 83070) = 0.2165 inch (5.499 mm)
(20-430 , 72-00-02) (SIN 83070) = 0.2362 inch (5.999 mm)
(20-440 , 72-00-02) (SIN 83070) = 0.2559 inch (6.500 mm).
(13)Measure and record dimensions AA, B, and BD before installing the LPT module assembly. Refer to Figure 404 and Figure 405.
(14)For dimension BD refer to Subtask 72-00-04-420-122 (paragraph 3.I.).
Subtask 72-00-04-220-035
A.A.Alternative procedure. Select the initial shim (20-360 , 72-00-02) (SIN 83070).
(1)If dimension R (final) was recorded before the removal of the LPT module and found to be outside the permitted limits, the original shim size can be adjusted accordingly until dimension R (final) is within limits when the LPT module is installed. Refer to Subtask 72-00-04-020-003 (72-00-04, REMOVAL 001).
* * * FOR ALL
Figure 404   (Sheet 1 ) Shim Thickness Calculation - Dimensions
* * * FOR ALL
* * * PRE SB   72-0425
Figure 404   (Sheet 2 ) Shim Thickness Calculation - Dimensions
* * * FOR ALL
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
Figure 404   (Sheet 3 ) Shim Thickness Calculation - Dimensions
* * * FOR ALL
Figure 405   Record Sheet - Shim Thickness
Subtask 72-00-04-420-109
B.Install the bumpers (item 4) of the 9446M40   LPT alignment fixture and the 11C3282   guide fixture to 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) aft flange. Refer to Figure 406, Figure 407, and do as follows:
(1)Make sure that the TCF assembly aft flange boltholes are numbered. If necessary, use a C05-003  marking pen and put marks on the boltholes.
(a)The 12:00 o'clock top vertical centerline bolthole is the No. 1 bolthole.
(b)Put a mark at the No. 10 bolthole, aft looking forward in a counterclockwise (CCW) direction.
(c)Put a mark at every 10th bolthole. There are 150 boltholes total.
(2)Install the bumpers (item 4) of the 9446M40   LPT alignment fixture on the TCF assembly aft flange at the 12:00 and 6:00 o'clock positions. Refer to Figure 406 and do as follows:
NOTE:
The bumper (item 4) stops the LPT module assembly from being installed in the propulsor assembly at a distance of approximately 3.00 inches (76.2 mm).
(a)Loosen the knob (item 9) on the locator block (item 2).
(b)Put the locator block (item 2) on the TCF assembly aft flange in the bolthole seat and the bumper (item 4) aft.
(c)Tighten the knob (item 9) to firmly attach the clamp block (item 3) to the TCF assembly flange.
(3)Install one guide arm (item 2) approximately at the 10:30 o'clock position of the TCF assembly.
(a)The pins on the guide arm bracket will fit into the No. 143 and No. 149 boltholes.
(b)Attach the guide arm to the TCF assembly flange with two capscrews (item 11) at the No. 142 and No. 149 boltholes. Attach a capscrew (item 11) and washer (item 12) on the forward side of the TCF assembly flange and a nut (item 13) on the aft side of the guide arm. Hand-tighten the capscrews (item 11).
(4)Install one guide arm (item 2) approximately at the 4:30 o'clock position on the TCF assembly as follows:
(a)The pins on the guide arm bracket will fit into the No. 74 and No. 79 boltholes.
(b)Attach the guide arm to the TCF assembly flange with two capscrews (item 11) at the No. 75 and No. 78 boltholes. Attach a capscrew (item 11) and washer (item 12) on the forward side of the TCF assembly flange and a nut (item 13) on the aft side of the guide arm. Hand-tighten the capscrews (item 11).
(5)Make sure that the locating pins (item 6) and the holes are engaged between the guide arms (item 2).
(6)Attach the guide arms (item 2) to the shaft guide liner (item 5) with the hand knobs (item 16). Make sure the shaft guide liner is aligned with the centerline of the opening on the aft side of the TCF assembly.
(7)Tighten the nuts (item 15) and capscrews (item 13) fully against the TCF assembly flange. Do not torque the nuts.
* * * FOR ALL
Figure 406   Installation of the LPT Alignment Fixture, 9446M40, on the LPT Module Assembly and the TCF Assembly
* * * FOR ALL
Figure 407   Installation of the Guide Fixture, 11C3282, on the TCF Assembly
Subtask 72-00-04-420-110
C.Alternative Procedure Available. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C3084   fan disk protector and the 11C3327   LPT mid-shaft guide fixture on the fan rotor disk (01-050 , 72-22-00) (SIN 830A0). Refer to Figure 408 and do as follows:
(1)Prepare to install the 11C3327   LPT mid-shaft guide fixture on the fan rotor disk as follows:
CAUTION:
MAKE SURE THAT THE ROD FOOT ARE IN THE LOCKED POSITION. THE ROD FOOT TABS CAN DAMAGE THE FAN ROTOR DISK.
NOTE:
(HES)Install the 11C3327 LPT mid-shaft guide fixture according to 11C3327G01 TDS. Refer to Case #02096312.
(a)Make sure the slot on the rod foot (items 4 and 7) are in the LOCKED position or you can damage the fan rotor disk. If not, align as follows:
1Loosen the nut (item 13) one turn and turn the 18 rod foot (items 4 and 7), align the slot to the UN-LOCKED position on the support frame (item 2).
2Tighten the nut (item 13) one turn.
Subtask 72-00-04-420-111
(2)Prepare to use the 9429M59   breach loader as follows. Refer to Figure 409.
NOTE:
Refer to the manufacturer's manual to operate the lift base (item 7).
(a)Install the cradle adapter (item 6) as follows:
1If necessary, remove the nylon adapter (item 3) from the tube adapter (item 2).
2Attach an overhead hoist to the eye bolt (item 8) on the cradle adapter (item 6).
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.
3Lift the cradle adapter (item 6), install on the tube adapter (item 2) and safely attach.
(b)Install the nylon tube (item 3) on the tube adapter (item 2) as follows:
1Put the nylon tube (item 3) onto the tube adapter (item 2) and secure with capscrews (item 10) at four locations.
2Put the nylon cover (item 4) on the tube adapter (item 2) and secure with the capscrew (item 9).
3Lift the nylon tube (item 3) and install on the tube adapter (item 2) and safely attach.
(c)Attach the tube adapter (item 2) to the lift base (item 7) with the lift base retaining pin.
CAUTION:
ALWAYS FOLLOW THE MANUFACTURER'S INSTRUCTIONS WHEN YOU OPERATE THE LIFT BASE (ITEM 7) TO PREVENT DAMAGE TO PARTS OR INJURY TO PERSONNEL.
(d)Operate the lift base (item 7) as instructed in the lift base manufacturer's instructions.
1Make sure you lock the lift base (item 7) to prevent movement of the lift.
2Do not lift a load unless there are a minimum of three wraps of cable around the winch drum of the lift base (item 7).
Subtask 72-00-04-420-112
(3)Put the 11C3084   fan disk protector in the support frame (item 2) of the 11C3327   LPT mid-shaft guide 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.
CAUTION:
OPERATE THE 9429M59   BREACH LOADER ON A LEVEL SURFACE ONLY.
(4)Lift the 11C3327   LPT mid-shaft guide fixture with the nylon tube (item 3) of the 9429M59   breach loader.
(5)Install the 11C3327   LPT mid-shaft guide fixture in the fan rotor disk (830A0) as follows:
(a)Lift the 11C3327   LPT mid-shaft guide fixture.
(b)Carefully install the 11C3327   LPT mid-shaft guide fixture into the dovetail slots of the fan rotor disk.
(c)Secure the support frame (item 2) to the fan rotor disk as follows:
1Loosen the nuts (item 13) and turn the rod foot (items 4 and 7) to align the slot with the LOCKED mark on the support frame (item 2). Make sure the rod foot is attached to the fan rotor disk.
2Tighten the nuts (item 13).
(6)Make sure that the feet on the rod foot (items 4 and 7) at 18 locations are in the locked position.
(7)Make sure that the rod foot (items 4 and 7) are in the locked position.
* * * FOR ALL
Figure 408   (Sheet 1 ) Installation of the Fan Disk Protector, 11C3084, and the LPT Mid-Shaft Guide Fixture, 11C3327, to the Forward Fan Shaft
* * * FOR ALL
Figure 408   (Sheet 2 ) Installation of the Fan Disk Protector, 11C3084, and the LPT Mid-Shaft Guide Fixture, 11C3327, to the Forward Fan Shaft
* * * FOR ALL
Figure 409   Breach Loader, 9429M59
Subtask 72-00-04-420-113
(8)Install the adapter guide (item 8) of the 11C5003   push/pull fixture in the 11C3327   LPT mid-shaft guide fixture. Refer to Figure 410 and do as follows:
CAUTION:
OPERATE THE 9429M59 BREACH LOADER ON A LEVEL SURFACE ONLY.
(a)Lift the adapter guide (item 8) of the 11C5003   push/pull fixture with the nylon tube (item 3) of the 9429M59   breach loader. Refer to Figure 409.
(9)Slide the adapter guide (item 8) of the 11C5003   push/pull fixture into the support frame (item 2) of the 11C3327   LPT mid-shaft guide fixture. Refer to Figure 410.
(10)Safety the adapter guide (item 8) of the 11C5003   push/pull fixture with the capscrews (item 9) of the 11C3327   LPT mid-shaft guide fixture at nine locations. Tighten the capscrews.
* * * FOR ALL
Figure 410   (Sheet 1 ) Installation of the Push/Pull Fixture, 11C5003, and the Extension Fixture, 11C3283
* * * FOR ALL
Figure 410   (Sheet 2 ) Installation of the Push/Pull Fixture, 11C5003, and the Extension Fixture, 11C3283
Subtask 72-00-04-420-163
C.A.Alternative Procedure. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has not been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C3084   fan disk protector and the 11C5013   installation/removal fixture to the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002). Refer to Figure 411 and do as follows:
(1)Install the 11C5013   installation/removal fixture as follows:
(a)Install the two nut plates (item 3) and the two nut plates (item 4) of the 11C5013   installation/removal fixture to the aft side of the forward fan shaft forward flange with four 5/8 capscrews (item 26). Torque the capscrews to 100 ft lb. (140 Nm).
NOTE:
There is only one threaded hole on each nut plate and is located on one of the ends. The threaded holes must be 90 degrees apart when the nut plates are fully installed.
(b)Install the protector (item 8) of the 11C3084   fan disk protector in the bore of the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002).
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)Use a hoist and applicable nylon strap to install the guide adapter (item 5) of the 11C5013   installation/removal fixture on the forward side of the forward fan shaft forward flange with 12 capscrews (item 32).
(d)Torque the cap screws (item 32) to 100 ft lb. (140 Nm).
* * * FOR ALL
Figure 411   (Sheet 1 ) Installation of the Installation/Removal Fixture, 11C5013, on the Forward Fan Shaft
* * * FOR ALL
Figure 411   (Sheet 2 ) Installation of the Installation/Removal Fixture, 11C5013, on the Forward Fan Shaft
Subtask 72-00-04-420-114
D.Alternative Procedure Available. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Prepare the LPT module assembly for installation into the propulsor assembly as follows:
(1)Remove the 11C3296   fan shaft protector from the front of the mid fan shaft assembly. Refer to Figure 412 and Figure 414.
(2)Put the shim (20-360 , 72-00-02) (SIN 83070) on the forward end of the mid fan shaft assembly.
(3)Install the extension tube (item 2) of the 11C3283   extension fixture onto the mid fan shaft assembly of the LPT module 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.
(a)Use a lift hoist with two lift straps to lift the extension tube (item 2).
(b)Carefully align the threaded end of the extension tube (item 2) with the forward end of the mid fan shaft assembly by hand.
CAUTION:
MAKE SURE NOT TO DAMAGE THE THREADS ON THE MID FAN SHAFT ASSEMBLY.
(c)Slowly rotate the extension tube (item 2) clockwise (CW) to engage the threads.
(d)Tighten the extension tube (item 2) onto the mid fan shaft assembly. Make sure that the extension tube is fully on the mid fan shaft assembly.
(e)Install the guide tip (item 3) on the extension tube (item 2) and secure with the capscrew (item 4).
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 THESE PRODUCTS.
(4)Lubricate the splines of the mid fan shaft assembly with C02-019  engine oil or C02-023  engine oil.
(5)Use a level to make sure the propulsor assembly is level at the TCF assembly aft flange. Make the necessary corrections to make the propulsor assembly level.
(6)Do a visual inspection of the TCF assembly aft cavity and LPT forward cavity for foreign object damage (FOD) or damage.
(7)Remove all protective caps or plugs from oil lines or the brush seal in the aft TCF assembly.
* * * FOR ALL
Figure 412   Installation of the Extension Fixture, 11C3283, onto the Mid Fan Shaft Assembly
Subtask 72-00-04-420-164
D.A.Alternative Procedure. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has not been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Prepare the LPT module assembly for installation into the propulsor assembly as follows:
(1)Remove the 11C3296   fan shaft protector from the front of the mid fan shaft assembly. Refer to Figure 413 and Figure 414.
(2)Put the shim (20-360 , 72-00-02) (SIN 83070) on the forward end of the mid fan shaft assembly.
Subtask 72-00-04-160-005
* * * SB   72-0114( Mid Fan Shaft with Molydag Lubricant Dry Film and Engine Oil Lubricant Assembly )
(3)Clean the 11C4272   extension fixture before installation on the mid fan shaft assembly (45-010A , 72-00-02) (SIN 81000) or (45-011A , 72-00-02) (SIN 81000) as follows:
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 THESE PRODUCTS.
CAUTION:
MAKE SURE TO CLEAN ANY GRAPHITE GREASE FROM TOOL 11C4272 TO PREVENT CONTAMINATION, OR DAMAGE TO THE ENGINE CAN OCCUR.
(a)Clean all graphite grease from the 11C4272   extension fixture with a C10-182  cleaning cloth moist with C02-019  engine oil or C02-023  engine oil.
(b)Continue the cleaning to remove all residual graphite grease from the 11C4272   extension fixture with a C10-182  cleaning cloth moist with C04-003  acetone .
(c)Do a close visual inspection to make sure that all the graphite grease was removed to prevent contamination.
NOTE:
PRE SB 72-0114 does not use this step.
* * * END SB   72-0114
Subtask 72-00-04-420-171
(4)Install the extension tube (item 2) of the 11C4272   extension fixture on the mid fan shaft 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.
(a)Use a lift hoist with two lift straps to lift the extension tube (item 2).
(b)Manually align the threaded end of the extension tube (item 2) with the forward end of the mid fan shaft assembly.
CAUTION:
MAKE SURE NOT TO DAMAGE THE THREADS ON THE MID FAN SHAFT ASSEMBLY.
(c)Slowly turn the extension tube (item 2) CW to engage the threads.
(d)Tighten the extension tube (item 2) onto the mid fan shaft assembly. Make sure that the extension tube is fully seated on the mid fan shaft assembly.
(e)Install the guide tip (item 3) on the extension tube (item 2) and secure with the capscrew (item 4).
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 THESE PRODUCTS.
(5)Lubricate the splines of the mid fan shaft assembly with C02-019  engine oil or C02-023  engine oil.
(6)Use a level to make sure the propulsor assembly is level at the TCF assembly aft flange. Make the necessary corrections to make the propulsor assembly level.
(7)Do a visual inspection of the TCF assembly aft cavity and LPT forward cavity for FOD or damage.
(8)Remove all protective caps or plugs from oil lines in the aft TCF assembly.
* * * FOR ALL
Figure 413   Installation of the Extension Fixture, 11C4272, on the Mid Fan Shaft Assembly
Subtask 72-00-04-420-115
E.Alternative Procedure Available. Remove the LPT module assembly from the 11C3426   LPT module dolly. Refer to Figure 414 and do as follows:
(1)Move the 11C3426   LPT module dolly and put the LPT module assembly directly behind the propulsor assembly.
(2)Make sure that the LPT module assembly is aligned with the centerline of the propulsor assembly and below the middle center of the hoist.
CAUTION:
FLOOR LOCKS MUST REMAIN EXTENDED TO THE FLOOR AT ALL TIMES EXCEPT WHEN REQUIRED TO MOVE THE DOLLY. THE CASTERS DO NOT PROVIDE SUFFICIENT STABILITY TO ALLOW FOR SAFE WORKING CONDITIONS.
(3)Put the floor locks (item 23) of the 11C3426   LPT module dolly against the floor.
(4)Adjust the 9C1147   VCG lift fixture to approximately 9.25 inches (235.0 mm).
(5)Attach the lift eye (item 65) of the 9C1147   VCG lift fixture to the load positioner.
CAUTION:
DO NOT USE THE LOAD INDICATOR DOWN HANDLE. USE THE HOIST OR THE 9C1147 VCG LIFT FIXTURE TO MOVE THE LPT MODULE ASSEMBLY DOWN.
(6)Put a torpedo level approximately in the middle of the mid fan shaft assembly and make sure that the LPT module assembly is level.
(7)Extend the load positioner 3.0 inches (76 mm) down after you lift the LPT module assembly so you have sufficient lift clearance.
(8)Make sure that the 11C3277   LPT restrain fixture is correctly installed. Make sure that the adjusting nut (item 5) and the three stop blocks (item 7) are in the correct position. Refer to TASK 72-00-04-430-801 (72-00-04, ASSEMBLY 001, CONFIG 01) or TASK 72-00-04-430-802 (72-00-04, ASSEMBLY 001, CONFIG 02).
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.
(9)Apply a lift pressure to the LPT module assembly.
NOTE:
The 11C3283   extension fixture or the 11C4272   extension fixture will be installed on the forward end of the mid fan shaft assembly.
(10)Remove the nuts (item 10) of the 11C3426   LPT module dolly from the slave bolts at 12 locations. Refer to Figure 414.
(11)Lift the LPT module assembly from the 11C3426   LPT module dolly.
(12)Extend the hydra-set down 3.00 inches (76.2 mm) to make room to lift up.
(13)Use a level at approximately the middle of the mid fan shaft assembly to make sure that it is level and that the LPT module assembly is parallel to the TCF assembly. Make the necessary corrections to level the mid fan shaft assembly as follows:
CAUTION:
DO NOT USE THE DOWN HANDLE ON THE HYDRA-SET TO ADJUST THE LPT MODULE ASSEMBLY DOWN. THE LPT MODULE ASSEMBLY CAN DROP QUICKLY AND DAMAGE THE LPT MODULE ASSEMBLY.
(a)Use the overhead hoist to adjust the down height of the LPT module assembly. Do not use the hydra-set to adjust the LPT module assembly down.
(b)Adjust the LPT module assembly with the 9C1147   VCG lift fixture to level the mid fan shaft assembly.
(c)When you use the up handle, the LPT module assembly will move up 0.005 inch (0.13 mm) each time you use the up handle.
(14)Make a record of the weight of the LPT module assembly. You will monitor the weight of the LPT module assembly on the load indicator when you install the LPT module assembly into the propulsor assembly.
NOTE:
The weight of the LPT module assembly is approximately 5000 lb (2270 kg).
Subtask 72-00-04-420-154
E.A.Alternative Procedure. Remove the LPT module assembly from the 11C3426   LPT module dolly. Refer to Figure 414 and do as follows:
(1)Prepare the lift hoist as follows:
(a)Install the load indicator to the overhead hoist.
(b)Attach the hydra-set to the load indicator. The hydra-set gives movement in increments of 0.005 inch (0.13 mm).
(c)Adjust the hydra-set down 3.0 inches (76 mm) to give room to lift the LPT module assembly and to give a full range of movement.
(2)Move the 11C3426   LPT module dolly directly behind the propulsor assembly. Make sure the LPT module assembly is aligned with the centerline of the propulsor assembly and is centered below the overhead hoist.
CAUTION:
THE FLOOR LOCKS (ITEM 23) MUST STAY AGAINST THE FLOOR AT ALL TIMES, BUT NOT WHEN YOU MOVE THE DOLLY. THE FLOOR LOCKS WILL PREVENT MOVEMENT AND DAMAGE TO THE 11C3426 LPT MODULE DOLLY AND LPT MODULE ASSEMBLY.
(3)Put the floor locks (item 23) of the 11C3426   LPT module dolly against the floor to prevent movement and equipment damage.
(4)Prepare the 9429M77   lift and turn fixture as follows:
(a)Attach two wires (length: 51.2 inches (1300 mm)) of the9429M77   lift and turn fixture to the pivot trunnions located on the aft side of the 11C4266   CG lift fixture.
(b)Attach two wires (length: 45.3 inches (1151 mm)) with the turnbuckle of the 9429M77   lift and turn fixture to the pivot trunnions located on the forward side of the 11C4266   CG lift fixture.
(c)Use turnbuckle to initially adjust CG of the LPT module.
(5)Install the hydra-set to the LPT module assembly as follows:
(a)Attach the hydra-set to an overhead crane hook.
(b)Attach the 9429M77   lift and turn fixture to the hydra-set.
(6)Make sure the 11C3277   LPT restrain fixture is installed correctly. Refer to TASK 72-00-04-430-801 (72-00-04, ASSEMBLY 001, CONFIG 01) or TASK 72-00-04-430-802 (72-00-04, ASSEMBLY 001, CONFIG 02).
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 INJURY OR KILL YOU.
(7)Apply a lift pressure to the LPT module assembly with the overhead hoist. The weight of the LPT module assembly is approximately 4025 lb (1826 kg).
NOTE:
The 11C3283   extension fixture or the 11C4272   extension fixture is installed on the forward end of the mid fan shaft assembly.
(8)Remove the ball-lock pins (item 54) of the 11C3426   LPT module dolly from the forward case supports (item 51) and (item 52).
(9)Lift the LPT module assembly from the aft pads (item 48) with the LPT case adapter plate (item 11) attached to the LPT module assembly.
(10)Remove the nuts (item 10) from the 0.250-28UNF slave bolts at 12 locations on the LPT case adapter plate (item 11), and use two people to remove the forward case supports (item 51) and (item 52).
(11)Move the 11C3426   LPT module dolly away from the LPT module assembly.
(12)Put a level on the mid fan shaft assembly to make sure that the LPT module assembly is level.
(13)If necessary, adjust the center of gravity (CG) on the 9429M77   lift and turn fixture with the turnbuckles (item 28) on the forward hoists.
(14)Make a record of the weight of the LPT module assembly. You will monitor the weight of the LPT module assembly on the load indicator when you install the LPT module assembly into the propulsor assembly.
CAUTION:
DO NOT USE THE DOWN HANDLE ON THE HYDRA-SET TO ADJUST THE LPT MODULE ASSEMBLY DOWN. THE LPT MODULE ASSEMBLY CAN DROP QUICKLY AND DAMAGE THE LPT MODULE ASSEMBLY.
(15)Use the overhead hoist to adjust the down height of the LPT module assembly in increments more than 0.10 inch (2.5 mm) and not the hydra-set to prevent damage to the LPT module assembly.
Subtask 72-00-04-420-195
E.B.Alternate Procedure. Remove the LPT module assembly from the 11C3426   LPT module dolly. Refer to Figure 414 and do as follows:
(1)Prepare the lift hoist and 11C4858   lift and turn fixture as follows:
(a)Install the load indicator to the overhead hoist.
(b)Attach the hydra-set to the load indicator. The hydra-set gives movement in increments of 0.005 inch (0.13 mm).
(c)Adjust the hydra-set down 3.0 inches (76 mm) to give room to lift the LPT module assembly and to give full range of movement.
(d)Attach 11C4858   lift and turn fixture lifting plate (item 2) to the hydra-set.
(e)Prepare two long sling assemblies by assembling a shackle (item 6) and swivel hook (item 9) to the cable assembly (item 4).
(f)Adjust the length of the two turnbuckles (item 8) to 20 inches (508 mm) between the bolt pin centers.
(g)Prepare two short sling assemblies by assembling a shackle (item 6) and swivel hook (item 9) to one end of the turnbuckle (item 8) and the cable assembly (item 5) to the opposite end.
(h)Connect each of the short and long sling assemblies to the lift plate (item 2) with shackle (item 7) on each side.
(2)Move the 11C3426   LPT module dolly directly behind the propulsor assembly. Make sure the LPT module assembly is aligned with the centerline of the propulsor assembly and is centered below the overhead hoist.
CAUTION:
THE FLOOR LOCKS (ITEM 23) MUST STAY AGAINST THE FLOOR AT ALL TIMES, BUT NOT WHEN YOU MOVE THE DOLLY. THE FLOOR LOCKS WILL PREVENT MOVEMENT AND DAMAGE TO THE 11C3426 LPT MODULE DOLLY AND LPT MODULE ASSEMBLY.
(3)Put the floor locks (item 23) of the 11C3426   LPT module dolly against the floor to prevent movement and equipment damage.
(4)Install the 11C4858   lift and turn fixture to the LPT module as follows:
(a)Attach each cable assembly swivel hook (item 9) to the pivot trunnions located on the forward side of the 11C4266   CG lift fixture.
(b)Attach each cable assembly swivel hook (item 9) to the pivot trunnions located on the aft side of the 11C4266   CG lift fixture.
(c)Use the turnbuckles to initially adjust CG of the LPT module if necessary.
(5)Make sure the 11C3277   LPT restrain fixture is installed correctly. Refer to TASK 72-00-04-430-801 (72-00-04, ASSEMBLY 001, CONFIG 01) or TASK 72-00-04-430-802 (72-00-04, ASSEMBLY 001, CONFIG 02).
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 INJURY OR KILL YOU.
(6)Apply a lift pressure to the LPT module assembly with the overhead hoist. The weight of the LPT module assembly is approximately 4025 lb (1826 kg).
NOTE:
The 11C3283   extension fixture or the 11C4272   extension fixture is installed on the forward end of the mid fan shaft assembly.
(7)Remove the ball-lock pins (item 54) of the 11C3426   LPT module dolly from the forward case supports (item 51) and (item 52).
(8)Lift the LPT module assembly from the aft pads (item 48) with the LPT case adapter plate (item 11) attached to the LPT module assembly.
(9)Remove the nuts (item 10) from the 0.250-28UNF slave bolts at 12 locations on the LPT case adapter plate (item 11), and use two persons to remove forward case supports (item 51) and (item 52).
(10)Move the 11C3426   LPT module dolly away from the LPT module assembly.
(11)Put a level on the mid fan shaft assembly to make sure that the LPT module assembly is level.
(12)If necessary, adjust the center of gravity (CG) on the 11C4858   lift and turn fixture with the turnbuckles (item 8) on the forward end of the 11C4266   CG lift fixture.
(13)Make a record of the weight of the LPT module assembly. You will monitor the weight of the LPT module assembly on the load indicator when you install the LPT module assembly into the propulsor assembly.
CAUTION:
DO NOT USE THE DOWN HANDLE ON THE HYDRA-SET TO ADJUST THE LPT MODULE ASSEMBLY DOWN. THE LPT MODULE ASSEMBLY CAN DROP QUICKLY AND DAMAGE THE LPT MODULE ASSEMBLY.
(14)Use the overhead hoist to adjust the down height of the LPT module assembly in increments more than 0.10 inch (2.5 mm) and not the hydra-set to prevent damage to the LPT module assembly.
* * * FOR ALL
Figure 414   (Sheet 1 ) Removal of the LPT Module Assembly from the LPT Module Dolly, 11C3426
* * * FOR ALL
Figure 414   (Sheet 2 ) Removal of the LPT Module Assembly from the LPT Module Dolly, 11C3426
* * * FOR ALL
Figure 414   (Sheet 3 ) Removal of the LPT Module Assembly from the LPT Module Dolly, 11C3426
* * * FOR ALL
Figure 414   (Sheet 4 ) Removal of the LPT Module Assembly from the LPT Module Dolly, 11C3426
Subtask 72-00-04-420-116
F.Install the LPT module assembly into the propulsor assembly as follows:
(1)Number the boltholes on the aft flange of 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) from the 12:00 o'clock position, ALF. Use a C05-003   marking pen and number every 10 boltholes. Refer to Figure 415.
(2)Install guide pins on the forward flange of the LPT module assembly at boltholes No. 25, 60, 95, and 134.
(3)Install the studs (93520) on the forward flange of the LPT module assembly (ALF), except at boltholes No. 25, 60, 95, and 134 where the guide pins are installed. Tighten hand-tight until seated.
NOTE:
The hex flange surface on the stud goes forward.
WARNING:
DELETED.
(4)Deleted.
CAUTION:
MAKE SURE YOU READ THE COMPLETE INSTALLATION SEQUENCE BEFORE YOU ATTEMPT TO INSTALL THE LPT MODULE ASSEMBLY. OTHERWISE, DAMAGE TO ENGINE PARTS OR AN INJURY CAN OCCUR.
NOTE:
Monitor the weight of the LPT module assembly during the installation procedure. Make sure the weight of the LPT module assembly does not change by plus or minus 50 lbs (22.7 kg).
NOTE:
During this procedure, you will slowly push the LPT module assembly into the propulsor assembly, and stop at several checkpoints to complete additional necessary steps.
(5)Align the mid fan shaft assembly with the center of the 11C3282   guide fixture on the aft side of the TCF assembly.
(6)Slowly push the LPT module assembly forward into the propulsor assembly. Monitor the space between the TCF assembly aft flange and the LPT module assembly forward flange.
(7)When the space between the flanges is approximately 3 feet (914 mm), stop the LPT module assembly.
(8)Remove the 11C3282   guide fixture as follows. Refer to Figure 407.
(a)Remove the nuts (item 13), capscrews (item 11), and washers (item 12) that attach the guide arms (item 2) to the TCF assembly.
(b)Remove the guide arms (item 2).
(c)Make sure the weight of the LPT module assembly did not change more than plus or minus 50 lbs (22.7 kg).
(9)Make sure that the mid fan shaft assembly is in the center of the No. 4 bearing stationary seal (15-060 , 72-54-00) (SIN 01407) as follows:
(a)Use a 6.0 inch (152 mm) scale, and measure at four equally spaced locations, to make sure that the mid fan shaft assembly is in the center of the seal. All four measurements must be within 0.03125 inch (0.7938 mm) of each other.
(b)If the measurements are not within the limits, adjust the LPT module assembly as necessary to put the mid fan shaft assembly in the center of the seal.
(10)Slowly push the LPT module assembly forward into the propulsor assembly and monitor the space between the TCF assembly aft flange and the LPT forward flange.
(11)When the distance between the flanges is approximately 6.50 inches (165.1 mm), do as follows:
(a)Monitor the mid fan shaft assembly and the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002) for a hard hit.
CAUTION:
BE CAREFUL WHEN YOU ROTATE THE FORWARD FAN SHAFT TO ENGAGE THE SPLINES. EXCESSIVE ROTATIONAL MOVEMENT CAN DAMAGE THE SPLINES.
(b)If you feel a hard hit, slowly turn the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002) to engage the splines.
(c)Continue to install the LPT module assembly into the core module assembly.
Subtask 72-00-04-420-155
(12)Alternative Procedure Available. When the distance between the flanges is approximately 3.00 inches (76.2 mm), the bumpers (item 4) of the 9446M40   LPT alignment fixture will make contact with the LPT module assembly. Adjust as follows:
(a)Measure the distance between the flanges around at the 12:00 and 6:00 o'clock positions. The difference must be within 0.100 in. (2.54 mm).
CAUTION:
MAKE SURE THAT THERE IS NO BINDING CONDITION THAT AFFECTS THE PINS AND SHAFT WHEN YOU ADJUST THE LPT MODULE ASSEMBLY CENTER OF GRAVITY. DAMAGE TO THE PINS OR SHAFT CAN OCCUR.
(b)If the difference is more than 0.100 in. (2.54), adjust the 9C1147   VCG lift fixture and do the inspection again. Make sure that the overhead hoist stays in the center above the shackle point of the 9C1147   VCG lift fixture.
(c)Monitor the LPT module assembly for a change in weight. Make sure the weight of the LPT module assembly does not change by plus or minus 50 lbs (22.7 kg).
Subtask 72-00-04-420-156
(12).A.Alternative Procedure. When the distance between the flanges is approximately 3.00 inches (76.2 mm), the bumpers (item 4) of the 9446M40   LPT alignment fixture will make contact with the LPT module assembly. Adjust as follows:
(a)Measure the distance between the flanges at the 12:00 and 6:00 o'clock positions. The difference must be within 0.100 in. (2.54 mm).
(b)If the difference is more than 0.100 in. (2.54), adjust the center of gravity on the 9429M77   lift and turn fixture and do the inspection again. Make sure that the overhead hoist stays in the center above the shackle point of the 9429M77   lift and turn fixture.
(c)Monitor the LPT module assembly for a change in weight. Make sure the weight of the LPT module assembly does not change by ±50 lb (23 kg).
Subtask 72-00-04-420-196
(12).B.Alternative Procedure. When the distance between the flanges is approximately 3.00 inches (76.2 mm), the bumpers (item 4) of the 9446M40   LPT alignment fixture will make contact with the LPT module assembly. Adjust as follows:
(a)Measure the distance between the flanges at the 12:00 and 6:00 o'clock positions. The difference must be in 0.100 in. (2.54 mm).
(b)If the difference is more than 0.100 in. (2.54), adjust the center of gravity on the 11C4858   lift and turn fixture and do the inspection again. Make sure that the overhead hoist stays in the center above the shackle point of the 11C4858   lift and turn fixture.
(c)Monitor the LPT module assembly for a change in weight. Make sure the weight of the LPT module assembly does not change by ±50 lb (23 kg).
Subtask 72-00-04-420-157
(13)Remove the bumpers (item 4) of the 9446M40   LPT alignment fixture.
(14)Remove the guide pins item (6) and install the studs (93520) at boltholes No. 25, 60, 95, and 134. Refer to Figure 415.
(15)Continue to install the LPT module assembly into the core module assembly.
(16)When you feel that the core module assembly and the LPT module assembly touch, do as follows:
(a)Use a 6.00 inches (152.4 mm) scale and measure the distance between the flanges at the 3:00 o'clock and the 9:00 o'clock positions. Apply manual pressure to the core to make sure that the core module assembly and the LPT module assembly touch when you measure the distance. The distance between the flanges must not be more than 0.90 inch (22.9 mm).
(b)If the difference between the two measurements is more than 0.90 inch (22.9 mm), do as follows:
1Remove the LPT module assembly from the core module assembly.
Subtask 72-00-04-420-117
(18)Install the LPT module assembly into the core module assembly again. Refer to Subtask 72-00-04-420-116 (paragraph 3.F.(10) thru (16).
(19)Make sure the LPT studs (93520) and the guide pins do not go in at angle in the TCF assembly aft flange boltholes.
* * * FOR ALL
Figure 415   Installation of the LPT Module Assembly into the Guide Fixture, 11C3282
Subtask 72-00-04-420-118
G.Alternative Procedure Available. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C5003   push/pull fixture to seat the LPT module assembly on the propulsor assembly and do as follows:
(1)Remove the capscrew (item 4) of the 11C3283   extension fixture from the guide tip (item 3). Refer to Figure 412.
(2)Remove the guide tip (item 3) from the extension tube (item 2). Use your hand and rotate the guide tip CCW to remove it from the extension tube (item 2).
(3)Make sure that the extension tube (item 2) is fully seated to the mid fan shaft assembly.
(4)Install the 11C5003   push/pull fixture to install the LPT module assembly. Refer to Figure 410 and do as follows:
(a)Install the spacer (item 23) on the 10-ton cylinder adapter (item 2) at two locations.
(b)Thread the 10-ton cylinder adapter (item 2) onto the extension tube (item 2) of the 11C3283   extension fixture.
(c)Install the 10-ton cylinder (item 12) of the 11C5003   push/pull fixture at two locations on the 10-ton cylinder adapter (item 2).
(5)Connect the hydraulic hand pump to the 10-ton cylinder (item 12).
(6)Before you apply hydraulic pressure, use a 6.00 inches (152.4 mm) scale and measure the distance between the flanges at the 3:00 o'clock and the 9:00 o'clock positions. Apply manual pressure to the core to make sure that the core module assembly and the LPT module assembly touch when you measure the distance. The distance between the flanges must not be more than 0.90 inch (22.9 mm).
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE 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:
MAKE SURE THAT THE STUDS (93520) OF THE LPT MODULE ASSEMBLY ARE ALIGNED WITH THE BOLTHOLES OF THE TCF ASSEMBLY. DAMAGE CAN OCCUR TO THE HARDWARE IF THEY ARE NOT CORRECTLY ALIGNED.
CAUTION:
WHEN YOU ENERGIZE THE HYDRAULIC CYLINDER, MAKE SURE THAT IT DOES NOT INCREASE IN INCREMENTS MORE THAN 1000 PSIG (6895 KPA GAGE). FOR EXAMPLE, IF THE GAUGE IS SET ON 1000 PSIG (6895 KPA GAGE), IT CANNOT INCREASE TO 2500 PSIG (17238 KPA GAGE) IN ONE MOVEMENT. DAMAGE TO THE ENGINE HARDWARE AND TOOLING CAN OCCUR IF YOU INCREASE THE PRESSURE IN LARGE INCREMENTS.
(7)Operate the hydraulic hand pump in 1000 psig (6895 kPa gage) increments until the distance between the TCF assembly aft flange and LPT forward flange is approximately 0.060-0.080 inch (1.52-2.03 mm). Do a manual examination of all of the LPT studs (35-020 , 72-00-02) (SIN 93520) to make sure that they continue to move freely as you pull the LPT module assembly into position.
NOTE:
It will be necessary to use 2000-8000 psig (13790-55160 kPa gage) to make the distance between the TCF assembly aft flange and the LPT forward flange approximately 0.060-0.080 inch (1.52-2.03 mm).
(8)When the distance between the aft flange of the TCF assembly and the forward flange of the LPT module assembly is approximately 0.060-0.080 inch (1.52-2.03 mm), unlock the three stop blocks (item 7) of the 11C3277   LPT restrain fixture installed on the TRF assembly. Refer to Figure 416 and do as follows:
(a)Loosen each set of two capscrews (item 12).
(b)Slide the stop blocks (item 7) radially outward to the unlock position.
(c)Tighten each set of capscrews (item 12) on the washer (item 15).
(9)Apply hydraulic pressure in 1000 psig (6895 kPa gage) increments until the LPT is fully seated against the TCF assembly aft flange. Do a manual examination of all the LPT studs (35-020 , 72-00-02) (SIN 93520) to make sure that they continue to move freely as you pull the LPT module assembly into position.
(10)It will be necessary to use 2000-8000 psig (13790-55158 kPa gage) to fully seat the LPT against the TCF assembly aft flange.
* * * FOR ALL
Figure 416   Movement of the Stop Blocks of the LPT Restrain Fixture, 11C3277, to the Unlock Position
Subtask 72-00-04-420-165
G.A.Alternative Procedure. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has not been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C5013   installation/removal fixture to seat the LPT module assembly on the propulsor assembly as follows:
(1)Remove the capscrew (item 4) of the 11C4272   extension fixture from the guide tip (item 3). Refer to Figure 413.
(2)Remove the guide tip (item 3) from the extension tube (item 2).
(3)Manually turn the guide tip (item 3) CCW to remove it from the extension tube (item 2).
(4)Make sure that the extension tube (item 2) is fully seated to the mid fan shaft assembly.
(5)Install the 11C5013   installation/removal fixture to install the LPT module assembly as follows. Refer to Figure 417.
(a)Two people should manually thread the 10 ton cylinder adapter (item 6) and the 10 ton single acting cylinder (item 16) assembly to the forward end of the 11C4272   extension fixture.
(b)Make sure that the 11C4272   extension fixture is fully locked and seated to the mid fan shaft assembly.
(c)Make sure that the 10 ton cylinder adapter (item 6) is fully engaged to the 11C4272   extension fixture.
(6)Connect the hydraulic hand pump to the 10 ton single acting cylinder (item 16).
(7)Before applying hydraulic pressure, use a 6.00 inches (152.4 mm) scale and measure the distance between the flanges at the 3:00 o'clock and the 9:00 o'clock positions.
(8)Apply manual pressure to the core to make sure that the core module assembly and the LPT module assembly touch when measuring the distance. The distance between the flanges must not be more than 0.90 inch (22.9 mm).
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE 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:
MAKE SURE THAT THE STUDS (93520) OF THE LPT MODULE ASSEMBLY ARE ALIGNED WITH THE BOLTHOLES OF THE TCF ASSEMBLY. DAMAGE CAN OCCUR TO THE HARDWARE IF THEY ARE NOT CORRECTLY ALIGNED.
CAUTION:
WHEN YOU ENERGIZE THE HYDRAULIC CYLINDER, MAKE SURE THAT IT DOES NOT INCREASE IN INCREMENTS MORE THAN 1000 PSIG (6895 KPA GAGE). FOR EXAMPLE, IF THE GAUGE IS SET ON 1000 PSIG (6895 KPA GAGE), IT CANNOT INCREASE TO 2500 PSIG (17238 KPA GAGE) IN ONE MOVEMENT. DAMAGE TO THE ENGINE HARDWARE AND TOOLING CAN OCCUR IF YOU INCREASE THE PRESSURE IN LARGE INCREMENTS.
(9)Operate the hydraulic hand pump in 1000 psig (6895 kPa gage) increments until the distance between the TCF assembly aft flange and LPT forward flange is approximately 0.060-0.080 inch (1.52-2.03 mm).
(10)Do a manual examination of all of the LPT studs (93520) to make sure that they continue to move freely as pulling the LPT module assembly into position.
NOTE:
It will be necessary to use 2000-8000 psig (13790-55160 kPa gage) to make the distance between the TCF assembly aft flange and the LPT forward flange approximately 0.060-0.080 inch (1.52-2.03 mm).
(11)When the distance between the aft flange of the TCF assembly and the forward flange of the LPT module assembly is approximately 0.060-0.080 inch (1.52-2.03 mm), unlock the three stop blocks (item 7) of the 11C3277   LPT restrain fixture installed on the TRF assembly. Refer to Figure 416 and do as follows:
(a)Loosen each set of two capscrews (item 12).
(b)Move the stop blocks (item 7) radially outward to the unlock position.
(c)Tighten each set of capscrews (item 12) on the washer (item 15).
(12)Apply hydraulic pressure in 1000 psig (6895 kPa gage) increments until the LPT is fully seated against the TCF assembly aft flange.
(13)Do a manual examination of all the LPT studs (93520) to make sure that they continue to move freely as pulling the LPT module assembly into position.
(14)Apply 2000-8000 psig (13790-55158 kPa gage) to fully install the LPT against the TCF assembly aft flange.
* * * FOR ALL
Figure 417   (Sheet 1 ) Installation of the Installation/Removal Fixture, 11C5013, and the Extension Fixture, 11C4272
* * * FOR ALL
Figure 417   (Sheet 2 ) Installation of the Installation/Removal Fixture, 11C5013, and the Extension Fixture, 11C4272
Subtask 72-00-04-420-119
H.Attach the forward flange of the LPT module assembly to the aft flange of 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) as follows:
(1)Install the LPT lockplates (93580, 93581) on the LPT studs (93520) as follows. Refer to Figure 415.
WARNING:
LUBRICANT IS AN IRRITANT. DO NOT LET THESE MATERIALS TOUCH YOU. DO NOT EAT OR DRINK. USE PERSONAL PROTECTION EQUIPMENT. ALLERGEN.
CAUTION:
MAKE SURE ALL STUDS HAVE A LOCKPLATE INSTALLED. IF YOU FIND A NUT ON A STUD WITHOUT A LOCKPLATE, THE STUD WILL THREAD INTO THE TCF ASSEMBLY, AND WILL HAVE TO BE RESET TO THE CORRECT DEPTH.
(a)If not previously done, apply C02-058  graphite to the threads of the studs (93520).
NOTE:
A minimum quantity of lubricant necessary for assembly can be used. After assembly, remove all remaining lubricant with a clean cloth.
(b)Put the LPT lockplate (93581) on the two studs that span the No. 1 and 150 boltholes. Attach the lockplate with two nuts (93541) and two spacers (93571).
(c)Put the lockplates (93580) on two studs (93520) on the forward side of the TCF and LPT module assembly flange. Example: Put a lockplate on the studs at boltholes No. 2 and 3, 4 and 5, and continue on to 148 and 149.
(2)Install the brackets on the TCF and the LPT module assembly flange as follows. Refer to Figure 418.
(a)Install the support bracket (62212), tab pointing forward, at boltholes No. 35 and 36, with nuts (93541).
(b)Install the LPT ACC supply support duct bracket (6221E), tab pointing forward, at boltholes No. 38-40, 42, and 43, with nuts (93541).
(c)Install the support bracket (35-200 , 72-00-02) (SIN 48910) or (35-211 , 72-00-02) (SIN 48910), tab pointing forward, at boltholes No. 73 and 74, with nuts (35-030 , 72-00-02) (SIN 93541).
(d)Install the transient bleed support bracket (61A18), tab facing forward, at bolthole locations No. 111-116, with nuts (93541).
(3)Install the nuts (93541) and the spacers (93571) on the studs (93520) at the non-bracket bolthole locations 2-4, 6, 8-15, 19-22, 25-34, 37, 41, 44, 47-52, 54, 55, 57, 58, 62-69, 72, 75-79, 81, 83, 87-90, 94, 99-106, 110, 117, 121-128, 131-132, 134, 137-144, 147-149. Tighten the nuts finger tight.
(4)Torque the nuts (93541) in the following sequence:
(a)Torque 15 nuts (93541) at bolthole locations No. 1, 11, 21, 31, 41, 51, 62, 72, 81, 94, 101, 110, 121, 131, and 141 in a criss-cross pattern to 80-95 lb in. (9.0-10.7 N.m) to pull the TCF and LPT flanges together.
(b)Torque the nuts (93541) in a criss-cross pattern to 106-124 lb in. (12.0-14.0 N.m).
(5)Release the hydraulic pressure applied to the 10 ton cylinder. Refer to Figure 410.
Subtask 72-00-04-420-166
(6)Alternative Procedure Available. Remove the 11C3283   extension fixture and 11C5003   push/pull fixture from the mid fan shaft assembly. Refer to Figure 412 and do as follows:
CAUTION:
MAKE SURE NOT TO DAMAGE THE THREADS ON THE MID FAN SHAFT ASSEMBLY.
(a)Manually turn the extension tube (item 2) of the 11C3283   extension fixture CCW and remove it from the mid fan shaft assembly. Pull it forward, away from the engine.
(b)Install the guide tip (item 3) on the front of the extension tube (item 2) and secure with the capscrew (item 4).
(c)Remove the 11C5003   push/pull fixture from the 11C3327   LPT mid-shaft guide fixture. Refer to Figure 410.
(d)Remove the 11C3277   LPT restrain fixture from the TRF.
Subtask 72-00-04-420-167
(6).A.Alternative Procedure. Remove the 11C4272   extension fixture and the 11C5013   installation/removal fixture from the mid fan shaft assembly. Refer to Figure 417 and do as follows:
CAUTION:
MAKE SURE NOT TO DAMAGE THE THREADS ON THE MID FAN SHAFT ASSEMBLY.
(a)Remove the cylinder adapter (item 6) of the 11C5013   installation/removal fixture.
(b)Manually turn the extension tube (item 2) of the 11C4272   extension fixture CCW and remove it from the mid fan shaft assembly. Pull it forward, away from the engine.
(c)Install the guide tip (item 3) on the front of the extension tube (item 2) and secure with the capscrew (item 4).
(d)Remove the 11C3277   LPT restrain fixture from the TRF as follows:
1Disengage the pilot tube (item 17) from the nut housing (item 19).
2Remove the pilot tube (item 17) from the restrain fixture assembly (item 2).
3Remove restrain fixture assembly (item 2).
4Remove the nut housing (item 19) from the LPT module assembly.
* * * FOR ALL
Figure 418   (Sheet 1 ) Installation of the Brackets on the TCF and the LPT Module Assembly Flange
* * * FOR ALL
Figure 418   (Sheet 2 ) Installation of the Brackets on the TCF and the LPT Module Assembly Flange
* * * FOR ALL
Figure 418   (Sheet 3 ) Installation of the Brackets on the TCF and the LPT Module Assembly Flange
* * * FOR ALL
Figure 418   (Sheet 4 ) Installation of the Brackets on the TCF and the LPT Module Assembly Flange
* * * FOR ALL
Figure 418   (Sheet 5 ) Installation of the Brackets on the TCF and the LPT Module Assembly Flange
Subtask 72-00-04-420-122
I.Install the forward lock nut onto the mid fan shaft assembly. Refer to Figure 419 and do as follows:
Subtask 72-00-04-420-174
* * * SB   72-0114( Mid Fan Shaft with Molydag Lubricant Dry Film and Engine Oil Lubricant Assembly )
(1)Clean the mating surfaces of the mid fan shaft assembly (45-010A , 72-00-02) (SIN 81000) or (45-011A , 72-00-02) (SIN 81000) and the forward lock nut (20-330A , 72-00-02) (SIN 83006) or (20-331 , 72-00-02) (SIN 83006) as follows:
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 THIS PRODUCT.
(a)Use C04-003  acetone to clean the forward lock nut.
(b)Use C04-003  acetone to clean the threads of the mid fan shaft assembly.
* * * END SB   72-0114
Subtask 72-00-04-160-007
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
(2)Clean the shim (20-335 , 72-00-02) (SIN 81072) as follows:
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 THIS PRODUCT.
(a)Use C04-003  acetone to clean the shim.
* * * END SB   72-0425
Subtask 72-00-04-420-175
(3)Measure dimension BD for the forward lock nut as follows:
(a)Use a micrometer and measure the distance from the tops of the castellations of the nut to the aft face.
(b)Measure Dimension BD at four equally-spaced locations. Record of the average Dimension BD.
Subtask 72-00-04-420-180
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
(4)Measure the dimension BE for the shim (20-335 , 72-00-02) (SIN 81072) as follows:
(a)Use a micrometer and measure the thickness of the shim.
(b)Measure the dimension BE at four equally-spaced locations. Record the average of dimension BE.
* * * END SB   72-0425
Subtask 72-00-04-640-016
(5)Deleted.
Subtask 72-00-04-640-030
* * * SB   72-0114( Mid Fan Shaft with Molydag Lubricant Dry Film and Engine Oil Lubricant Assembly )
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.
CAUTION:
ONLY C02-019 ENGINE OIL OR C02-023 ENGINE OIL CAN BE USED FOR LUBRICATION. DO NOT USE C02-058 LUBRICANT TO LUBRICATE THE THREADS OF THE MID FAN SHAFT AND FORWARD LOCK NUT, OR DAMAGE TO THE ENGINE CAN OCCUR.
(6)Lubricate the threads of the mid fan shaft assembly (45-010A , 72-00-02) (SIN 81000) or (45-011A , 72-00-02) (SIN 81000) and the threads and aft face of the forward lock nut (20-330A , 72-00-02) (SIN 83006) or (20-331 , 72-00-02) (SIN 83006) with C02-019   engine oil or C02-023  engine oil.
* * * END SB   72-0114
Subtask 72-00-04-420-181
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
(7)Put the shim (20-335 , 72-00-02) (SIN 81072) on the forward lock nut.
* * * END SB   72-0425
* * * FOR ALL
* * * PRE SB   72-0425
Figure 419   (Sheet 1 ) Installation of the Forward Lock Nut
* * * FOR ALL
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
Figure 419   (Sheet 2 ) Installation of the Forward Lock Nut
Subtask 72-00-04-420-123
(8)Alternative Procedure Available. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C3423   coupling nut torque fixture. Refer to Figure 420 and do as follows:
Subtask 72-00-04-160-006
* * * SB   72-0114( Mid Fan Shaft with Molydag Lubricant Dry Film and Engine Oil Lubricant Assembly )
(a)Clean the 11C3423   coupling nut torque fixture before the installation of the forward lock nut (20-330A , 72-00-02) (SIN 83006) or (20-331 , 72-00-02) (SIN 83006) as follows:
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.
CAUTION:
MAKE SURE TO CLEAN ANY GRAPHITE GREASE FROM THE TOOL 11C3423 TO PREVENT CONTAMINATION, OR DAMAGE TO THE ENGINE CAN OCCUR.
1Clean all graphite grease from the 11C3423   coupling nut torque fixture with a C10-182  cleaning cloth moist with C02-019  engine oil or C02-023  engine oil.
2Continue the cleaning to remove all residual graphite grease from the 11C3423   coupling nut torque fixture with a C10-182  cleaning cloth moist with C04-003  acetone.
3Do a close visual inspection to make sure that the cleaning removed all the graphite grease to prevent contamination.
NOTE:
PRE SB 72-0114 does not use this step.
* * * END SB   72-0114
Subtask 72-00-04-420-172
(b)Put the guide tube (item 16) into the 11C3327   LPT mid-shaft guide fixture and secure with capscrews (item 14) of the 11C3423   coupling nut torque fixture at the 2:30 and 9:30 o'clock positions.
(c)Put the anti-torque plate (item 5) onto the guide tube (item 16) at the 2:30 and 9:30 o'clock positions.
(d)Secure the anti-torque plate (item 5) with the capscrews (item 14) at seven locations.
(e)Set the torque tube (item 17) and the locking nut tube in a horizontal position.
(f)Install the lift ring (item 10) onto the torque tube (item 17) and tighten the setscrews (item 11) into the slot of the torque tube.
(g)Install the rod handles (item 8) onto the lock cap (item 7).
(h)Put the lock cap (item 7) onto the locking nut tube (item 19).
Subtask 72-00-04-420-183
* * * PRE SB   72-0425
(i)Install the forward lock nut into the torque tube (item 17).
* * * END PRE SB   72-0425
Subtask 72-00-04-420-184
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
(i).A.Install the forward lock nut with the shim (20-335 , 72-00-02) (SIN 81072) on it, into the torque tube (item 17).
* * * END SB   72-0425
Subtask 72-00-04-420-185
(j)Hold the torque tube (item 17) and rotate the lock cap (item 7) and the locking nut tube (item 19), in relation to the torque tube (item 17), to the locked position.
(k)Make sure the plungers (items 13) lock into position in the torque tube (item 17).
(l)Remove the two handles (item 8) from the lock cap.
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:
OPERATE THE 9429M59 BREACH LOADER ON A LEVEL SURFACE ONLY.
(m)Lift the torque tube assemblies that contain items 17, 19, 7, and 10. Use the 9429M59   breach loader. Refer to Figure 409.
(n)Insert the torque tube assemblies into the anti torque plate (item 5) and push aft.
(o)Remove the 9429M59   breach loader.
(p)Install the rod handles (item 8) onto the lock cap (item 7).
Subtask 72-00-04-420-186
* * * PRE SB   72-0425
CAUTION:
DO NOT CROSS-THREAD THE FORWARD LOCK NUT. DAMAGE TO THE NUT AND THE MID FAN SHAFT CAN OCCUR.
(q)Turn the torque tube assemblies CW to thread the forward lock nut onto the mid fan shaft assembly. Refer to Figure 419.
* * * END PRE SB   72-0425
Subtask 72-00-04-420-187
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
CAUTION:
DO NOT CROSS-THREAD THE FORWARD LOCK NUT. DAMAGE TO THE NUT AND THE MID FAN SHAFT CAN OCCUR.
(q).A.Turn the torque tube assemblies CW to thread the forward lock nut with the shim (20-335 , 72-00-02) (SIN 81072) on it, onto the mid fan shaft assembly. Refer to Figure 419.
* * * END SB   72-0425
Subtask 72-00-04-420-182
(r)Make sure that the locking nut tube (item 19) of the 11C3423   coupling nut torque fixture turns freely.
(s)Deleted.
(t)Turn the lock cap handles (item 8) to finish threading on the coupling nut.
(u)Retract the three plungers (item 13) to remove the lock cap (item 7).
(v)Remove the lift ring (item 10).
(w)Attach a hoist to the 8200torque multiplier and lift the torque multiplier.
(x)Align the 8200torque multiplier with the torque tube (item 17) and engage the splines on the lift ring (item 10).
(y)Turn the 8200torque multiplier slightly to find the pins of the torque multiplier with the forward end of the anti-torque plate (item 5).
* * * FOR ALL
Figure 420   (Sheet 1 ) Installation of the Coupling Nut Torque Fixture, 11C3423
* * * FOR ALL
Figure 420   (Sheet 2 ) Installation of the Coupling Nut Torque Fixture, 11C3423
Subtask 72-00-04-420-168
(8).G.Alternative Procedure. Use this procedure when the fan booster assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000) has not been installed to the fan hub module (25-010 , 72-00-02) (SIN 00102), or (25-011 , 72-00-02) (SIN 00102), or (25-012 , 72-00-02) (SIN 00102). Install the 11C5013   installation/removal fixture. Refer to Figure 421 and do as follows:
(a)Remove the 22 capscrews (item 32) from the adapter guide (item 5).
(b)Remove adapter guide (item 5) from the nut plates (item 3 and 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.
(c)Use a hoist and applicable nylon strap to install the guide adapter (item 2) of the 11C5013 installation/removal fixture on the forward side of the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002) forward flange with 18 capscrews (item 32).
(d)Torque the capscrews (item 32) to 100 ft lb. (140 Nm).
Subtask 72-00-04-420-188
* * * PRE SB   72-0425
(e)Install the forward lock nut in the coupling nut wrench (item 10).
* * * END PRE SB   72-0425
Subtask 72-00-04-420-189
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
(e).A.Install the forward lock nut with a shim (20-335 , 72-00-02) (SIN 81072) on it, in the coupling nut wrench (item 10).
* * * END SB   72-0425
Subtask 72-00-04-420-190
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.
(f)Use lift assistance and a two-legged sling to install the coupling nut wrench (item 10) into the guide adapter (item 2).
Subtask 72-00-04-420-191
* * * PRE SB   72-0425
CAUTION:
DO NOT CROSS-THREAD THE FORWARD LOCK NUT. DAMAGE TO THE NUT AND THE MID FAN SHAFT CAN OCCUR.
(g)Turn the torque tube assemblies CW to turn the forward lock nut on the mid fan shaft assembly.
* * * END PRE SB   72-0425
Subtask 72-00-04-420-192
* * * SB   72-0425( Introduction of New Forward Fan Shaft with Metallic Shim )
CAUTION:
DO NOT CROSS-THREAD THE FORWARD LOCK NUT. DAMAGE TO THE NUT AND THE MID FAN SHAFT CAN OCCUR.
(g).A.Turn the torque tube assemblies CW to turn the forward lock nut with the shim (20-335 , 72-00-02) (SIN 81072) on it, on the mid fan shaft assembly.
* * * END SB   72-0425
Subtask 72-00-04-420-193
(h)Unthread the lock bolts (item 15) from the adapter (item 2) while keeping them in place.
(i)Attach a hoist to the torque multiplier and lift the torque multiplier.
(j)Align the torque multiplier with the coupling nut wrench (item 10) and engage the splines on the coupling nut wrench (item 10).
(k)Align and insert the reaction pins of the torque multiplier with the holes in adapter (item 2).
(l)Attach firmly the reaction pins of the torque multiplier by tightening the locking bolts (item 15).
* * * FOR ALL
Figure 421   (Sheet 1 ) Installation of the Installation/Removal Fixture, 11C5013, and the Coupling Nut Wrench
* * * FOR ALL
Figure 421   (Sheet 2 ) Installation of the Installation/Removal Fixture, 11C5013, and the Coupling Nut Wrench
Subtask 72-00-04-420-124
* * * SB   72-0114( Mid Fan Shaft with Molydag Lubricant Dry Film and Engine Oil Lubricant Assembly )
(9)Apply an initial torque of 1100 to 1260 lb ft (1491 to 1708 Nm) to the forward lock nut (20-330A , 72-00-02) (SIN 83006) or (20-331 , 72-00-02) (SIN 83006).
(10)Do the final torque of the forward lock nut as follows:
CAUTION:
DO NOT APPLY MORE THAN 24 DEGREES OR 8,300 LB FT (11253 N.M) OF TORQUE OR DAMAGE TO THE ENGINE PARTS CAN OCCUR.
(a)Torque the forward lock nut another 20 degrees past the initial torque.
(b)Deleted.
NOTE:
Deleted.
(c)Record the final torque value. Refer to Figure 422.
(d)Record the final angle.
* * * END SB   72-0114
Subtask 72-00-04-420-173
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.
(11)Remove the 8200torque multiplier.
(12)Attach the lift ring (item 10) to the torque tube (item 17) and tighten the setscrews (item 11).
Subtask 72-00-04-420-169
(13)Alternative Procedure Available. Remove the 11C3423   coupling nut torque fixture from the 11C3327   LPT mid-shaft guide fixture with the 9429M59   breach loader. Do not remove the tube guide (item 16) of the 11C3423   coupling nut torque fixture.
Subtask 72-00-04-420-170
(13).A.Alternative Procedure. Remove the coupling nut wrench (item 10) and the 11C5013   installation/removal 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.
(a)Use lift assistance and a two-legged sling to remove the coupling nut wrench from the 11C5013   installation/removal fixture.
(b)Remove the 18 capscrews (item 32) that hold the adapter (item 2) to the nut plates.
(c)Use lift assistance and a nylon sling to remove the adapter (item 2).
(d)Remove the 4 capscrews (item 26) that hold the nut plates (item 3 and item 4) to the forward fan shaft.
* * * FOR ALL
Figure 422   Forward Lock Nut - Record Sheet
Subtask 72-00-04-220-027
(14)Measure the mid fan shaft assembly distance to the forward lock nut. Refer to Figure 423 and do as follows:
(a)Install the 11C3424   mid fan shaft gage in the tube guide (item 16) of the 11C3423   coupling nut torque fixture installed in the 11C3327   LPT mid-shaft guide fixture as follows:
1Remove the ball lock pins (item 11) and the clamps (item 2) to separate the set master (item 9) from the aft end of the tool.
2Verify the transducers (item 10) and the indicators (item 19) are functioning properly by turning the power on and pushing the tips through their range.
NOTE:
Indicators (item 19) are battery operated. When the plunger tip is depressed (forward to engine orientation), the value must increase (+), and when the plunger tip is permitted to go back (aft to engine orientation), the value must decrease (-). If the values are opposite, the gauges polarities must be moved in the opposite direction.
3Zero the indicators by setting the gage into the set master (item 9) and aligning the centering block (item 8) with the hole in the bottom of the set master. The pins at 6:00 and 12:00 o'clock position must be in place. The clamps at the 3:00 and 9:00 o'clock position must be fully secured.
4Zero the indicators while supporting the gage. The centerline of the gage should be vertical for an accurate setpoint.
5Align the centering blocks (item 8) with the holes in the set master (item 9).
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
6Use C04-035  isopropyl alcohol and clean the set master (item 9) aft surface where it will contact the forward lock nut.
7Lift the sleeve (item 3) and put the aft end into the guide tube (item 16) of the 11C3423   coupling nut torque fixture.
CAUTION:
DO NOT USE EXCESSIVE FORCE TO SLIDE 11C3424 MID FAN SHAFT GAGE AFT. THE TRANSDUCERS CAN BE DAMAGED.
8Slowly slide the sleeve (item 3) of the 11C3424   mid fan shaft gage aft. The diametrical clearance between the insert and the sleeve (item 3) decreases at the forward and aft ends of the insert to provide alignment and support. Extreme care must be taken not to force the tool. When a resistance is detected, stop sliding the sleeve aft.
9The centering block (item 8) should be contacting the shaft. The spring force of the springs (item 20) behind the blocks should be detectable. Move the gage in and out about a tenth of an inch to get the feel of the springs.
10Gently rotate the gage while applying light pressure so that the centering block will engage one of the slots of the shaft. A rotational resistance will be felt when the centering block (item 8) enters a slot. There is a slot every 22.5 degrees and you can rotate the gage in either direction.
11Check a second time to ensure the alignment tab is engaged into a slot. The indicator points will read closer to zero when they are engaged into the slots if the gage is forward enough.
NOTE:
A borescope can be installed through the center of the tube to observe the position of the alignment pin.
12Engage the positioning screw (item 5) into the threads of the sleeve (item 3) of the 11C3424   mid fan shaft gage and tighten by hand.
(b)Record the indications of the tranducers (item 10) as ABFINAL1, ABFINAL2, and ABFINAL3. The indicator (item 19) will give the dimension to the forward lock nut from the end of the mid fan shaft assembly.
NOTE:
A positive value is forward and a negative value is aft of the mid fan shaft assembly.
(c)Calculate the average of the readings and record as ABAVG. Refer to Figure 419.
(15)Calculate for ABFINAL. If there is an error in the ABFINAL calculation, it may be necessary to remove the LPT module assembly to determine the cause of the error. Contact local assembly engineer for a recommended course of action if the ABFINAL calculation is not within tolerance.
Subtask 72-00-04-420-125
(16)Remove the positioning screw (item 5) and pull the sleeve (item 3) forward.
(17)Install the set master (item 9) on the forward end of the sleeve (item 3).
(18)Install the ball-lock pins (item 11) and the clamps (item 2).
(19)Remove the 11C3424   mid fan shaft gage from the fan rotor disk (830A0) with the 9429M59   breach loader.
(20)Remove the guide tube (item 16) of the 11C3423   coupling nut torque fixture from the fan rotor disk (830A0).
(21)Remove the 11C3084   fan disk protector from the fan rotor disk (830A0).
(22)Remove the 11C3327   LPT mid-shaft guide fixture from the fan rotor disk (830A0).
* * * FOR ALL
Figure 423   (Sheet 1 ) Installation of the Mid Fan Shaft Gage, 11C3424, in the Forward Fan Shaft
* * * FOR ALL
Figure 423   (Sheet 2 ) Installation of the Mid Fan Shaft Gage, 11C3424, in the Forward Fan Shaft
Subtask 72-00-04-220-028
J.Measure the final Dimension R on the No. 5 bearing housing (01501) and the LPT cone shaft (930D1) as follows. Refer to Figure 424.
(1)Measure at four equally spaced locations adjacent to the spacers on the aft flange of the No. 5 bearing housing (01501).
(2)Measure from the aft face of the No. 5 bearing housing (01-050 , 72-57-00) (SIN 01501) to the aft inner diameter of the LPT cone shaft (01-050 , 72-56-00) (SIN 930D1). Refer to Figure 424.
(3)Calculate the average of the four measurements and record it as dimension R (final) in the record table. Refer to Figure 405.
(4)Use one of the procedures below to make sure that the LPT rotor is in the correct axial setting.
Subtask 72-00-04-220-036
(a)Alternative Procedure Available. If dimension R (preliminary) is known, calculate the difference between R (final) and the result of R (preliminary) and shim difference. The difference must be no more than plus or minus 0.015 inch (0.38 mm). Refer to Subtask 72-00-04-220-017 (72-00-04, ASSEMBLY 001, CONFIG 01) or Subtask 72-00-04-220-033 (72-00-04, ASSEMBLY 001, CONFIG 02).
1Record the results in the record sheet. Refer to Figure 405.
Subtask 72-00-04-220-037
(a).A.Alternative Procedure. If dimension R (preliminary) is not known, dimension R (final) must be within 1.806 to 1.858 inches (45.88 to 47.19 mm).
1Record the results in the record sheet. Refer to Figure 405.
* * * FOR ALL
Figure 424   Final Measurement of Dimension R
Subtask 72-00-04-420-126
K.Install the brackets on the LPT module assembly forward flange and the TCF aft flange on the propulsor assembly as follows. Put the brackets on the forward side of the flange. Refer to Figure 418.
Subtask 72-00-04-640-017
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.
(1)Lubricate the threads of 56 nuts (93541) with C02-019  engine oil or C02-023  engine oil.
Subtask 72-00-04-420-127
(2)Install the LPT ACC bracket (62216) at bolthole locations No. 5 and No. 7 with nuts (93541) the tab aft.
(3)Install the LPT ACC bracket (62211) at bolthole locations No. 16 and No. 18 with nuts (93541) with the tab aft.
(4)Install the LPT ACC bracket (62215) at bolthole locations No. 23 and No. 24 with nuts (93541) with the tab aft.
(5)Install the LPT ACC bracket (62215) at bolthole locations No. 45 and No. 46 with nuts (93541) with the tab aft.
(6)Install the support bracket (66210) at bolthole locations No. 53 and No. 56 with nuts (93541) with the tab aft.
(7)Install the LPT ACC bracket (66211) at bolthole locations No. 59-61 with three nuts (93541) with the tab aft.
(8)Install the LPT ACC bracket (66214) at bolthole locations No. 70 and No. 71 with nuts (93541) with the tab forward.
(9)Install the LPT ACC bracket (66216) at bolthole locations No. 80 and No. 82 with nuts (93541) with the tab aft.
(10)Install the support bracket (44317) at bolthole locations No. 84-86 with nuts (93541) with the tab forward.
(11)Install the LPT bracket (66211) at bolthole locations No. 91-93 with three nuts (93541) with the tab aft.
(12)Install the support bracket (44313) at bolthole locations No. 95 and 96 with nuts (93541) with the tab forward.
(13)Install the LPT bracket (62215) at bolthole locations No. 97 and No. 98 with nuts (93541) with the tab aft.
(14)Install the LPT bracket (62213) at bolthole locations No. 107-109 with three nuts (93541) with the tab forward.
(15)Install the support bracket (62218) at bolthole locations No. 118-120 with three nuts (93541) with the tab aft.
(16)Install the LPT ACC bracket (62215) at bolthole locations No. 129 and No. 130 with nuts (93541) with the tab aft.
(17)Install the LPT ACC bracket (62217) at bolthole locations No. 133, 135, and 136 with three nuts (93541) with the tab aft.
(18)Install the LPT ACC bracket (62214) at bolthole locations No. 145 and No. 146 with nuts (93541) with the tab forward.
(19)Torque the nuts (93541) at the TCF-LPT flange in a criss-cross pattern to 79-93 lb in. (8.9-10.5 N.m).
(20)Torque the nuts (93541) again at the TCF-LPT flange in criss-cross pattern to 106-124 lb in. (12.0-14.0 N.m).
(21)Torque the nuts (93541) at the TCF-LPT flange in circular pattern to 106-124 lb in. (12.0-14.0 N.m).
Subtask 72-00-04-420-128
L.Install the lock plate (20-320 , 72-00-02) (SIN 83092) and the retainer ring (20-310 , 72-00-02) (SIN 83091) onto the forward lock nut. Refer to Figure 425 and do as follows:
(1)Prepare the 11C3304   forward retainer fixture to install the lock plate (83092) and the retainer ring (83091) as follows:
NOTE:
When the 11C3304G02 forward retainer fixture is used, the threaded guide (guide) (item 2), lockplate installer (item 4), and snap ring holder (item 6) must slide together.
(a)Install the guide (item 2) or (item 15) of the 11C3304   forward retainer fixture through the fan rotor disk (01-050 , 72-22-00) (SIN 830A0) and into the forward end of the mid fan shaft assembly.
(b)Turn the guide (item 2) or (item 15) into the inner threads of the mid fan shaft assembly and tighten it until the aft end of the guide (item 2) or (item 15) seats against the A/O vent center tube (center vent duct) (01-020 , 72-58-00) (SIN 810A1) in the mid fan shaft assembly.
(2)Install the lock plate (20-320 , 72-00-02) (SIN 83092) onto the four tabs on the lockplate holder (item 10). The lockplate holder is attached to the lockplate installer (item 4) or (item 16) with the capscrews (item 13).
(3)Install the lockplate installer (item 4) or (item 16), the lockplate holder (item 10), and the lock plate (20-320 , 72-00-02) (SIN 83092) over the guide (item 2) or (item 15). Align the outer diameter tabs with the castellations on the forward lock nut, and the inner diameter tabs with the castellations on the mid fan shaft. If necessary, rotate the lock plate in order to find the correct alignment.
(4)Install the lockplate installer nut (nut) (item 5) on the forward threaded end of the guide (item 2) or (item 15) until the lockplate installer (item 4) or (item 16) and the lock plate (20-320 , 72-00-02) (SIN 83092) are against the forward lock nut.
(5)Compress the retainer ring (20-310 , 72-00-02) (SIN 83091) outside diameter and put in the groove on the aft end of the snap ring holder (item 6) or (item 17).
(6)Install the snap ring holder (item 6) or (item 17) onto the lockplate installer (item 4) or (item 16).
(7)Thread the snap ring nut (item 7) onto the forward end of the guide (item 2) or (item 15) to seat the snap ring holder (item 6) or (item 17) against the forward end of the forward lock nut.
(8)Install the snap ring pusher (pusher) (item 14) on the snap ring holder (item 6) or (item 17) as follows:
(a)Align the pusher so the 12 pins on the aft end go through the 12 clearance holes in the snap ring holder (item 6) or (item 17).
(b)Slide the pusher (item 14) aft until the threads on the guide (item 2) or (item 15) are visible.
(9)Install the pusher nut (item 9) on the forward end of the guide (item 2) or (item 15).
(10)Tighten the pusher nut (item 9) until the 12 pins push the retainer ring (20-310 , 72-00-02) (SIN 83091) out of the snap ring holder (item 6) or (item 17) groove and it expands into the groove in the forward end of the forward lock nut.
(11)Make sure the lock plate (20-320 , 72-00-02) (SIN 83092) and retainer ring (20-310 , 72-00-02) (SIN 83091) are correctly installed and that they prevent the rotation of the forward lock nut.
(12)Remove the 11C3304   forward retainer fixture.
(13)Do a visual inspection of the fan shaft bore for FOD.
* * * FOR ALL
Figure 425   Installation of the Lock Plate and the Retainer Ring with the Forward Retainer Fixture, 11C3304
Subtask 72-00-04-420-129
M.Install the forward fan shaft cover (20-290 , 72-00-02) (SIN 81003) in forward fan shaft of the fan stator module assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000). Refer to Figure 426 and do as follows:
NOTE:
The 11C3421G03   fan shaft cover fixture installs the fan shaft cover with or without the aft support ring installed and the 11C3421G02   fan shaft cover fixture only operates with the aft support ring removed.
Subtask 72-00-04-640-018
(1)Install the 11C3084   fan disk protector into the bore of the fan rotor disk (01-050 , 72-22-00) (SIN 830A0) and the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002) or aft support ring (20-100 , 72-00-00) (SIN 8300A). Refer to Figure 427.
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.
(2)Lubricate the lead-in chamfer and inner diameter of the forward fan shaft with C02-019  engine oil or C02-023  engine oil.
(3)Lubricate the packing (20-300 , 72-00-02) (SIN 81050) with C02-019   engine oil or C02-023  engine oil.
Subtask 72-00-04-420-130
(4)Install the packing (20-300 , 72-00-02) (SIN 81050) onto the outer groove of the fan shaft cover (81003).
CAUTION:
MAKE SURE THAT THE PACKING (20-300 , 72-00-02) (SIN 81050) IS FULLY SEATED IN THE OUTER GROOVE OF THE FORWARD FAN SHAFT COVER (20-290 , 72-00-02) (SIN 81003). IF NOT CORRECTLY SEATED, THE PACKING CAN BE DAMAGED WHEN THE COVER IS CAREFULLY PUSHED INTO PLACE IN THE FORWARD FAN SHAFT.
(5)Install the fan shaft cover (81003) on the 11C3421   fan shaft cover fixture as follows:
NOTE:
Items 3, 13, and 16 are not used to install the fan shaft cover.
(a)Align the tabs on the fan shaft cover with the open slots on the removal cover (item 2).
(b)Turn until the tabs touch the pins on the removal cover (item 2).
(6)Lift the fan shaft cover (20-290 , 72-00-02) (SIN 81003) with the removal cover (item 2) and put the fan shaft cover in the fan stator module assembly (20-010 , 72-00-02) (SIN 80000) or (20-011 , 72-00-02) (SIN 80000).
(7)Push on the center fan shaft cover (81003) with the 11C3421   fan shaft cover fixture to deflect and to install.
(8)Use a shop light to do an inspection of the packing (20-300 , 72-00-02) (SIN 81050) to make sure that it is in the correct position.
(9)Install the retaining ring (20-280 , 72-00-02) (SIN 81082) into the groove inside the bore of the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002). Compress the retaining ring slightly and let it expand into the groove.
(10)Remove the removal cover (item 2) from the forward fan shaft cover.
(11)Remove the 11C3084   fan disk protector from the bore of the fan rotor disk and the forward fan shaft (01-170 , 72-24-00) (SIN 81002) or (01-171 , 72-24-00) (SIN 81002).
* * * FOR ALL
Figure 426   Installation of the Forward Fan Shaft Cover With the Fan Shaft Cover Fixture, 11C3421
* * * FOR ALL
Figure 427   (Sheet 1 ) Installation of the Retainer Rings and Fan Shaft Cover with the Aft Support Ring Installed
* * * FOR ALL
Figure 427   (Sheet 2 ) Installation of the Retainer Rings and Fan Shaft Cover with the Aft Support Ring Installed
Subtask 72-00-04-420-131
N.Install the 9429M47   LPT support overhead adapter on the LPT module assembly. Refer to Figure 428 and do as follows:
NOTE:
The 9429M47   LPT support overhead adapter is a part of the 11C3044   engine module adapter assembly.
(1)If necessary, install the TRF bootstrap brackets (01-160) (SIN 941E1) to the LPT module assembly flanges of the TRF assembly at boltholes 16-19 and 60-63 (ALF). Refer to TASK 72-00-04-430-801 (72-00-04, ASSEMBLY 001, CONFIG 01) or TASK 72-00-04-430-802 (72-00-04, ASSEMBLY 001, CONFIG 02).
(2)Put a level on the rear flange of the TRF assembly and level the propulsor assembly.
CAUTION:
DO NOT USE SUPPORT ADAPTERS THAT ARE NOT APPROVED. THE USE OF SUPPORT ADAPTERS THAT ARE NOT APPROVED CAN DAMAGE THE PROPULSOR ASSEMBLY.
(3)Attach the hook of the 9429M47   LPT support overhead adapter to the customer overhead hanger assembly.
(4)Adjust the turnbuckles upwards or downwards until the holes on the jaw end turnbuckle are aligned with the holes on the TRF bootstrap brackets (941E1).
(5)Attach the hook of the 9429M47   LPT support overhead adapter to the TRF bootstrap brackets (941E1) with the adapter pins.
(6)Adjust the turnbuckles to tighten the 9429M47   LPT support overhead adapter.
(7)Remove the 9429M45   K-flange overhead adapter from the propulsor assembly.
* * * FOR ALL
Figure 428   Propulsor Assembly Installed in the Customer Overhead Rail System with the Engine Module Adapter Assembly, 11C3044
Subtask 72-00-04-420-132
(8)Install the brackets on the extension case (10-080 , 72-30-00) (SIN 080AL) and the combustor case (01-079 , 72-41-00) (SIN 12001) or (01-080 , 72-41-00) (SIN 12001) flanges or the combustor case (01-230 , 72-41-00) (SIN 12001) or (01-230A , 72-41-00) (SIN 12001) flanges where the 9429M45   K-flange overhead adapter was removed. Refer to TASK 72-00-02-430-817 (72-00-02, ASSEMBLY 002, CONFIG 01) or TASK 72-00-02-430-820 (72-00-02, ASSEMBLY 002, CONFIG 02) and do as follows:
NOTE:
Put the bolt heads forward unless you are instructed differently.
Subtask 72-00-04-640-019
(a)Lubricate all the threads and bearing surfaces of the bolts (12022) with C02-058  graphite.
Subtask 72-00-04-420-133
(b)Install the accelerometer cable bracket (34210) in boltholes 9-11 with the bolts (12022) and nuts (12040). Put the bracket on the forward side of the flanges. Tighten the nuts hand-tight.
Subtask 72-00-04-420-176
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
* * * PRE SB   72-0161( Propulsor Module - Non PIP2 Configuration )
(c)Install the support bracket (33-310 , 72-00-02) (SIN 6101V) in boltholes 123-126 with the bolts (33-070 , 72-00-02) (SIN 12022) and nuts (33-080 , 72-00-02) (SIN 12040). Put the bracket on the forward side of the flanges. Tighten the nuts hand-tight.
1Attach the support bracket (33-310 , 72-00-02) (SIN 6101V) to the bracket (25-580 , 72-00-02) (SIN 6101Y) with bolts (33-300 , 72-00-02) (SIN 6102G). Tighten the bolts hand-tight.
NOTE:
SB 72-0161 does not use this step. SB 72-0161 introduces a new bracket (30-700 , 72-00-02) (SIN 6101V) that is installed at a different location.
* * * END PRE SB   72-0161
Subtask 72-00-04-420-177
* * * FOR ALL
(d)Install the support bracket (34111) in boltholes 120 and 121 with the bolts (12022) and nuts (12040). Put the bracket on the aft side of the flanges. Tighten the nuts hand-tight.
Subtask 72-00-04-420-178
* * * FOR 1B/P/G03.1B/P/G04.1B/P1/G01
* * * PRE SB   72-0161( Propulsor Module - Non PIP2 Configuration )
(e)Install the tube control support bracket (33-100 , 72-00-02) (SIN 61010) in boltholes 129 and 130 with the bolts (33-070 , 72-00-02) (SIN 12022) and nuts (33-080 , 72-00-02) (SIN 12040). Put the bracket on the forward side of the flanges. Tighten the nuts hand-tight.
NOTE:
SB 72-0161 does not use this step. SB 72-0161 introduces a new bracket (33-101 , 72-00-02) (SIN 61010) that is installed at a different location.
* * * END PRE SB   72-0161
Subtask 72-00-04-420-179
* * * FOR ALL
(f)Install the bolts (12022) and nuts (12040) in any holes that remain. Tighten the nuts hand-tight.
(g)Torque the nuts (12040) at equally spaced locations in a criss-cross pattern to 276-324 lb in. (31.2-36.6 N.m).
(h)Torque the nuts (12040) at equally spaced locations in a criss-cross pattern to 368-432 lb in. (41.6-48.8 N.m).
(i)Torque the bolts (6102G) to 106-124 lb in. (12.0-14.0 N.m).
Subtask 72-00-04-420-158
CAUTION:
BE CAREFUL WHEN YOU REMOVE TOOLING FROM THE TRF ASSEMBLY ON THE PROPULSOR ASSEMBLY. THE TRF ASSEMBLY CAN BE DAMAGED.
(11)Alternative Procedure Available. Remove the 11C3165   strongback fixture from the TRF assembly on the aft end of the propulsor assembly. Refer to Figure 414.
Subtask 72-00-04-420-159
CAUTION:
BE CAREFUL WHEN YOU REMOVE TOOLING FROM THE TRF ASSEMBLY ON THE PROPULSOR ASSEMBLY. THE TRF ASSEMBLY CAN BE DAMAGED.
(11).D.Alternative Procedure. Remove the 11C4266   CG lift fixture from the TRF assembly on the aft end of the propulsor assembly. Refer to Figure 403.
(a)Install the machine bolts (bolts) (01-050) (SIN 94020) and (01-070) (SIN 94022) and self-locking nuts (nuts) (01-060) (SIN 94040) that were removed from the LPT module assembly/TRF assembly flanges during installation of the 11C4266   CG lift fixture as follows:
NOTE:
Six bolts on the right side ALF and seven bolts on the left side ALF.
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.
1Apply C02-058  graphite to the threads and friction surfaces of the bolts and nuts.
aUse the minimum quantity of lubricant necessary for the assembly.
bRemove the remaining lubricant with a clean cloth.
2Torque the bolts to 161-179 lb in. (18.2-20.2 N.m).
Subtask 72-00-04-420-135
O.Install the No. 5 bearing carbon seal runner (seal runner) (0155A) as follows:
CAUTION:
WEAR LATEX GLOVES WHEN HANDLING THE SEAL RUNNER (0155A). DO NOT TOUCH THE SEAL RUNNER WITH YOUR BARE HANDS. DAMAGE TO THE CARBON SEAL CAN OCCUR.
(1)Measure dimension T at four equally-spaced locations. Make a record of the minimum and maximum dimensions. Wear C10-140  latex glove to prevent damage to the seal runner. Refer to Figure 429.
(2)Install the guide ring (item 13) of the 11C3328   install/remove tool on the aft flange studs of the No. 5 bearing housing (01501) and attach it with the nuts (item 26) at 20 locations. Refer to Figure 430.
(3)Install the housing (item 32) into the guide ring (item 13). Turn the housing (item 32) CW to thread into the LPT cone shaft (930D1).
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.
CAUTION:
DO NOT FREEZE THE COMPLETE PART. APPLY DRY ICE ONLY TO THE FORWARD FLANGE OF THE SEAL RUNNER. DAMAGE TO THE CARBON SEAL CAN OCCUR.
(4)Decrease the temperature of the forward flange of the seal runner (0155A) as follows:
(a)Put the seal runner forward end down on dry ice.
(b)Keep the part on the dry ice for 20 minutes.
(5)Install the 11C3328   install/remove tool on the seal runner as follows:
(a)Align the tabs on the push/pull tube (item 12) with the slots in the seal runner.
(b)Install the tabs of the push/pull tube (item 12) through the slots in the seal runner. Turn the push/pull tube 1/2 tooth to engage the seal runner.
(c)Move the seal locking tube (item 11) forward and engage the tabs of the seal locking tubes with the slots in the seal runner.
(d)Attach the hydraulic hand pump to the hydraulic cylinder (item 21) and fully retract the piston. Disconnect the hydraulic pump.
(6)Install the seal runner (0155A) as follows:
(a)Install the seal runner and 11C3328   install/remove tool through the bore of the housing (item 32) and on the LPT cone shaft (930D1). Refer to Figure 430.
(b)Install the hydraulic cylinder (item 21) on the push/pull tube rod. Make sure the piston of the cylinder pushes aft as the pressure increases.
(c)Attach the cylinder support (item 16) to the housing (item 32) with two ball lock pins (item 19).
WARNING:
BE CAREFUL WHEN YOU USE THE PUSHER/PULLER TO APPLY PRESSURE. MAKE SURE YOU DO NOT USE 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 USE MORE THAN THE MAXIMUM INSTALLATION PRESSURE OF 2,500 PSI (17236 KPA). OTHERWISE, DAMAGE TO THE ENGINE PARTS CAN OCCUR.
(7)Attach the hydraulic hand pump and apply 2,000 psi (13789 kPa) hydraulic pressure to seat the seal runner.
NOTE:
Leave the the 11C3328 install/remove tool in position and let the part normalize for a minimum of 20 minutes.
(8)Remove the seal runner tooling as follows:
(a)Release the hydraulic pressure. Disconnect the hydraulic hand pump from the hydraulic cylinder.
(b)Remove the two ball lock pins (item 19) and remove the cylinder support (item 16).
(c)Remove the hydraulic cylinder (item 21)
(d)Move the seal locking tube (item 11) aft and remove it.
(e)Turn the push/pull tube (item 12) 1/2 tooth to align the tabs with the slots on the seal runner. Remove the push/pull tube.
(f)Turn the housing (item 32) CCW (ALF) and remove it.
(g)Loosen and remove the nuts (item 26) and remove the guide ring (item 13).
(9)Remove the tape from the seal teeth at the aft end of the A/O extension duct (45-270 , 72-00-02) (SIN 810A8).
* * * FOR ALL
Figure 429   Measurement of Dimension T on the No. 5 Bearing Carbon Seal Runner
* * * FOR ALL
Figure 430   (Sheet 1 ) Installation of the 11C3328 Install/Remove Tool on the Seal Runner
* * * FOR ALL
Figure 430   (Sheet 2 ) Installation of the 11C3328 Install/Remove Tool on the Seal Runner
Subtask 72-00-04-220-031
P.Do a seating check of the seal runner (0155A) as follows:
(1)Measure from the aft castellations of the LPT cone shaft to the aft side of the forward flange of the seal runner. Refer to Figure 431.
(2)Measure Dimension V at four equally-spaced locations. Record the average Dimension V.
(3)Calculate dimension V as follows:
Dimension V = Dimension S - Dimension T
(4)Compare the calculated dimension V with the measured dimension V. The difference between the calculated and measured dimensions must be less than 0.002 inch (0.05 mm)
* * * FOR ALL
Figure 431   Seating Check of the Seal Runner
Subtask 72-00-04-420-136
Q.Install the carbon seal coupling nut (01545) as follows. Refer to Figure 432.
(1)Prepare the carbon seal coupling nut (coupling nut) (01545) for installation as follows:
Subtask 72-00-04-160-003
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(a)Clean the threads of the coupling nut (01545) and the LPT cone shaft (930D1). Clean the mating face of the coupling nut and the No. 5 bearing carbon seal runner. Use C04-035  isopropyl alcohol.
Subtask 72-00-04-640-020
(b)Apply C02-058  graphite to the threads of the coupling nut (01545) and the LPT cone shaft (930D1).
Subtask 72-00-04-420-137
(2)Install the locking inserts (01580) on the coupling nut (01545) at four locations.
(3)Install the coupling nut (01545) on the LPT cone shaft (930D1).
* * * FOR ALL
Figure 432   Installation of the No. 5 Bearing Locknut and the Coupling Nut
Subtask 72-00-04-420-138
(4)Install the 11C3277   LPT restrain fixture as follows:
(a)Attach the 9C1017   VCG fixture to the restrain fixture (item 2) of the 11C3277   LPT restrain fixture. Refer to Figure 433.
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 hoist to the 9C1017   VCG fixture and lift the restrain fixture (item 2). Adjust the center of gravity on the 9C1017   VCG fixture to keep the 11C3277   LPT restrain fixture level.
(c)Attach the ring (item 8) to the turbine rear frame with nuts (item 13), washers (item 14), and cap screws (item 11) at nine equally-spaced locations.
* * * FOR ALL
Figure 433   Installation of the LPT Restraining Fixture, 11C3277
Subtask 72-00-04-420-139
(5)Install the 11C5012   spanner nut torque fixture. Refer to Figure 434 and do as follows:
(a)Install the 11C3288   carbon runner seal protector on the No. 5 bearing carbon seal runner (0155A).
(b)Install the guide tube (item 18) of the 11C5012   spanner nut torque fixture into the bore of the restrain fixture (item 2) of the 11C3277   LPT restrain fixture.
(c)Align the holes in the guide tube with the holes in the restrain fixture and attach the guide tube with six capscrews (item 15). Refer to Figure 434.
(d)Install the anti-torque tube (item 3) of the 11C5012   spanner nut torque fixture and the torque tube (item 4) assembly in the aft end of the anti-torque hub (item 5).
(e)Align the two holes in the flange of the anti-torque tube (item 3) with the threaded holes in the aft flange of the anti-torque hub (item 5).
(f)Attach the anti-torque tube (item 3) to the anti-torque hub (item 5) with capscrews (item 10).
CAUTION:
MAKE SURE THE TORQUE TUBE (ITEM 4) IS AGAINST THE AFT STOP RING (ITEM 7).
(g)Pull the torque tube (item 4) aft until it is against the aft stop ring (item 7). Make sure the torque tube (item 4) is against the aft stop ring (item 7).
CAUTION:
OPERATE THE 9429M59   BREACH LOADER ON A LEVEL SURFACE ONLY.
(h)Lift the 11C5012   spanner nut torque fixture tube assembly with the 9429M59   breach loader and align it with the guide tube (item 18) of the 11C5012   spanner nut torque fixture. Refer to Figure 409.
(i)Install the tube assembly into the guide tube (item 18). Move the tube assembly forward until the teeth on the forward end of the anti-torque tube (item 3) engage the slots in the aft end of the LPT cone shaft (01-050 , 72-56-00) (SIN 930D1).
(j)Move the anti-torque hub (item 5) forward and align the holes in the anti-torque hub with the holes in the flange of the guide tube (item 18).
(k)Attach the anti-torque hub (item 5) to the guide tube (item 2) with two ball-lock pins (item 8) at the 3:00 o'clock and 9:00 o'clock positions.
(l)Install two capscrews (item 11) at the 12:00 o'clock and 6:00 o'clock positions.
* * * FOR ALL
Figure 434   Installation of the Spanner Nut Torque Fixture, 11C5012
Subtask 72-00-04-420-140
(6)Install the 8200torque multiplier on the 11C5012   spanner nut torque fixture. Refer to Figure 435 and do as follows:
CAUTION:
MAKE SURE THAT THE THREADED PINS (ITEM 19) ON THE 11C5012 SPANNER NUT TORQUE FIXTURE ARE LOOSENED ENOUGH TO PERMIT THE REACTION PINS TO BE PLACED INTO THE ANTI-TORQUE HUB (ITEM 5) BEFORE THE TORQUE MULTIPLIER IS INSTALLED.
(a)Loosen the two threaded pins (item 19) on the 11C5012   spanner nut torque fixture.
(b)Install the 8200torque multiplier on the anti-torque hub (item 5) of the 11C5012   spanner nut torque fixture.
(c)Push the 8200torque multiplier forward and slide onto the splines of the torque tube (item 4) of the 11C5012   spanner nut torque fixture.
(d)Align the pins with the holes in the anti-torque hub (item 5) and seat the 8200torque multiplier against the anti-torque hub.
(e)Tighten the two threaded pins (item 19) on the 11C5012   spanner nut torque fixture.
(7)Torque the coupling nut (01545) to initial seat the coupling nut as follows:
NOTE:
Calculate the torque with the torque ratio of the torque multiplier.
CAUTION:
DO NOT APPLY MORE THAN 127 LB FT (172.2 N.M) OF TORQUE.
(a)Rotate the handle on the torque multiplier to seat the coupling nut to 127 lb ft (172.2 N.m).
(b)Break the torque on the coupling nut. Turn the nut a minimum of three turns.
(c)Record the run-on torque as follows:
CAUTION:
DO NOT APPLY MORE THAN 127 LB FT (172.2 N.M) OF TORQUE.
1Rotate the handle on the torque multiplier to seat the coupling nut to 127 lb ft (172.2 N.m).
2Record the run-on torque of the coupling nut (01545).
3If the run-on torque is not more than 23 lb ft (31.2 N.m), remove the coupling nut (01545) and replace the locking inserts (01580).
(8)Calculate the final torque and apply a final torque of 600-727 lb ft (814-986 N.m) to the coupling nut (01545). Do not apply more than maximum torque of 727 lb ft (986 N.m).
(9)Remove the 8200torque multiplier from the 11C5012   spanner nut torque fixture.
(10)Remove the 11C5012   spanner nut torque fixture from the 11C3277   LPT restrain fixture as follows:
WARNING:
BALANCE THE PARTS TO BE LIFTED BEFORE YOU OPERATE THE EQUIPMENT. DO NOT STAY BELOW THE EQUIPMENT WHEN YOU LIFT THE PART. DO NOT LIFT MORE THAN THE SPECIFIED WEIGHT. IF THE PARTS ACCIDENTALLY MOVE OR FALL, A BAD INJURY CAN OCCUR.
(a)Loosen two threaded pins (item 19) and remove torque multiplier with the aid of appropriate lifting device.
(b)Remove the anti-torque hub (item 5) from guide tube (item 18) by removing two ball-lock pins (item 8) and two bolts (item 11).
(c)Use the 9429M59   breach loader or a two-legged sling to carefully remove the shaft assembly (items 3-8, item 10, item 13, item 14, item 19, and item 20) from guide tube (item 18). Make sure that certain tool is properly supported while withdrawing.
(d)Remove the guide tube (item 18) of the 11C5012   spanner nut torque fixture from the 11C3277   LPT restrain fixture by removing six hex head capscrews (item 15)
Subtask 72-00-04-420-141
R.Install the No. 5 bearing locknut (01503), the retaining ring (01593), and the lockplate (01592) on the LPT cone shaft (930D1) as follows. Refer to Figure 432.
(1)Prepare the No. 5 bearing locknut (01503) as follows:
Subtask 72-00-04-160-004
WARNING:
ISOPROPYL ALCOHOL IS TOXIC AND FLAMMABLE. USE PERSONAL PROTECTION EQUIPMENT. USE IN A WELL-VENTILATED AREA.
(a)Clean the threads and the seating surface of the No. 5 bearing locknut (01503) with C04-035  isopropyl alcohol.
(b)Clean the threads of the LPT cone shaft (930D1) with C04-035  isopropyl alcohol.
Subtask 72-00-04-640-021
(c)Apply C02-058  graphite to the threads and the seating surface of the locknut (01503).
(d)Apply C02-058  graphite to the threads of the LPT cone shaft (930D1).
Subtask 72-00-04-420-142
(2)Install the No. 5 bearing locknut (01503) on the LPT cone shaft (930D1) by hand.
(3)Install the 11C3334   No. 5 bearing locknut torque fixture on the 11C3277   LPT restrain fixture as follows. Refer to Figure 435.
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:
OPERATE THE 9429M59   BREACH LOADER ON A LEVEL SURFACE ONLY.
(a)Lift the 11C3334   No. 5 bearing locknut torque fixture with the cradle adapter (item 6) of the 9429M59   breach loader. Refer to Figure 409.
(b)Insert the torque tube (item 2) of the 11C3334   No. 5 bearing locknut torque fixture smoothly into the 11C3277   LPT restrain fixture on the engine centerline.
(c)Insert the anti-torque tube (item 3) of the 11C3334   No. 5 bearing locknut torque fixture smoothly into the torque tube (item 2) on the engine centerline.
* * * FOR ALL
Figure 435   Installation of the No. 5 Bearing Locknut Torque Fixture, 11C3334
Subtask 72-00-04-420-143
(4)Slide the torque tube (item 2) and the anti-torque tube (item 3) of the 11C3334   No. 5 bearing locknut torque fixture forward.
(5)Turn to engage the tabs of the torque tube (item 2) in the tabs of the No. 5 bearing locknut (01503).
(6)Turn to engage the tabs of the anti-torque tube (item 3) in the tabs of the LPT cone shaft (930D1).
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.
(7)Install the 8200torque multiplier over the splines of the anti-torque tube (item 3) of the 11C3334   No. 5 bearing locknut torque fixture.
(8)Install the 9429M17   anti-torque plate onto the splines of the torque tube (item 2) of the 11C3334   No. 5 bearing locknut torque fixture.
(9)Torque the No. 5 bearing locknut (01503) as follows:
NOTE:
Calculate the torque with the torque ratio of the torque multiplier.
(a)Torque the locknut to 880 lb ft (1193.3 N.m).
CAUTION:
DO NOT APPLY MORE THAN 1050 LB FT (1423.8 N.M) OF TORQUE.
(b)Check to see if a scribe line on the torque tube (item 2) of the 11C3334   No. 5 bearing locknut torque fixture is aligned with a scribe line on the anti-torque tube (item 3). If not, continue to torque the No. 5 bearing locknut (01503) until the scribe lines are aligned. Do not apply more than 1050 lb ft (1423.8 N.m) of torque.
(c)Remove the 9429M17   anti-torque plate from the torque multiplier.
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)Remove the 8200torque multiplier.
(e)Use a clean cloth to remove excess lubricant from the locknut.
(10)Slide the torque tube (item 2) of the 11C3334   No. 5 bearing locknut torque fixture and the anti-torque tube (item 3) aft.
(11)Record the torque value of the No. 5 bearing locknut (01503).
(12)Install the No. 5 bearing lock plate (lockplate) (01592). Two tabs on the outside diameter of the lock plate will fit into castellations on the No. 5 bearing locknut (01503). Two tabs on the inner diameter of the lock plate will fit into castellations on the inner shaft. You may have to rotate the lock plate (01592) or try different positions for it to correctly align with the No. 5 bearing locknut (01503). Refer to Figure 432.
(13)Install the retaining ring (01593) directly aft of the lockplate (01592). Compress the retaining ring radially inward and let it to expand into the groove inside the castellations of the No. 5 bearing locknut (01503).
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:
OPERATE THE 9429M59   BREACH LOADER ON A LEVEL SURFACE ONLY.
(14)Remove the 11C3334   No. 5 bearing locknut torque fixture with the cradle adapter (item 6) of the 9429M59   breach loader.
(15)Remove the 11C3277   LPT restrain fixture as follows:
(a)Disengage the pilot tube (item 17) from the nut housing (item 19).
(b)Remove the pilot tube (item 17) from the restrain fixture assembly (item 2).
(c)Remove restrain fixture assembly (item 2).
(d)Remove the nut housing (item 19) from the LPT module assembly.
Subtask 72-00-04-420-144
CAUTION:
WEAR C10-143 LATEX GLOVE WHEN HANDLING THE CARBON SEAL. DO NOT TOUCH THE CARBON SEAL WITH YOUR BARE HANDS. DAMAGE TO THE CARBON SEAL CAN OCCUR.
S.Install the No. 5 bearing carbon seal (carbon seal) (45-350 , 72-00-02) (SIN 01558) in the TRF assembly. Refer to Figure 436 and do as follows:
Subtask 72-00-04-640-022
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 THESE PRODUCTS.
(1)Lubricate the preformed packing (45-340 , 72-00-02) (SIN 01551) with C02-019   engine oil or C02-023  engine oil.
(2)Lubricate with C02-019  engine oil or C02-023  engine oil the chamfer of the TRF assembly where the preformed packing (45-340 , 72-00-02) (SIN 01551) will be installed.
Subtask 72-00-04-420-145
(3)Install the preformed packing (45-340 , 72-00-02) (SIN 01551) in the forward side of the carbon seal (01558).
(4)Install the 11C3474   No. 5 bearing carbon seal guide on the A/O extension duct (45-270 , 72-00-02) (SIN 810A8). Refer to Figure 437.
CAUTION:
WEAR C10-143 LATEX GLOVE WHEN HANDLING THE CARBON SEAL. DO NOT TOUCH THE CARBON SEAL WITH YOUR BARE HANDS. DAMAGE TO THE CARBON SEAL CAN OCCUR.
(5)Install the carbon seal (45-350 , 72-00-02) (SIN 01558) in the TRF assembly.
(6)Install the installation nuts (item 2) of the 11C4292   installation fixture at four equally spaced locations.
(7)Tighten in a criss-cross pattern to seat the carbon seal (01558).
(8)Remove the 11C4292   installation fixture.
(9)Remove the 11C3474   No. 5 bearing carbon seal guide from the A/O extension duct (45-270 , 72-00-02) (SIN 810A8).
Subtask 72-00-04-780-005
(10)Do a flow check of the carbon seal (01558) as follows:
(a)Install the cover cap (item 2) of the 11C3287   air flow test stand on the carbon seal.
(b)Secure with nuts (item 4) at six locations.
WARNING:
BE CAREFUL WHEN YOU APPLY PRESSURE. MAKE SURE YOU DO NOT USE MORE THAN THE MAXIMUM PRESSURE. ALWAYS USE SAFETY SHIELDS DURING THE TEST. RELEASE PRESSURE BEFORE YOU DISCONNECT THE LINES AND FITTINGS. A MALFUNCTION CAN CAUSE AN INJURY OR CAN KILL YOU.
(c)Attach a supply of clean, dry, compressed air to a 9461M40   air flow test stand. Refer to Figure 438.
(d)Connect the 9429M71   universal adapter kit to the connector (item 7) of the 11C3287   flow cover.
(e)Attach the 9461M40   air flow test stand to the 9429M71   universal adapter kit.
(f)Turn on the 9461M40   air flow test stand.
(g)Allow 20 minutes for the 9461M40   air flow test stand to warm up.
(h)Set the pressure to 8-10 psig (55.2-69.0 Kpa gage) across the carbon seal. The maximum air flow permitted is 0.22 SCFM (0.0001038284 cms).
(i)When the test is completed, release the pressure from the 9461M36   test stand.
(j)Disconnect the 9461M40   air flow test stand and 9429M71   universal adapter kit from the 11C3287   flow cover.
* * * FOR ALL
Figure 436   (Sheet 1 ) Installation of the Carbon Seal and C-Sump Cover
* * * FOR ALL
* * * PRE SB   72-0039( Old Oil Nozzle Design )
Figure 436   (Sheet 2 ) Installation of the Carbon Seal and C-Sump Cover
* * * FOR ALL
* * * SB   72-0039( New Oil Nozzle Design )
Figure 436   (Sheet 3 ) Installation of the Carbon Seal and C-Sump Cover
* * * FOR ALL
Figure 436   (Sheet 4 ) Installation of the Carbon Seal and the C-Sump Cover
* * * FOR ALL
Figure 437   (Sheet 1 ) No. 5 Bearing Carbon Seal Guide, 11C3474
* * * FOR ALL
Figure 437   (Sheet 2 ) Deleted
* * * FOR ALL
Figure 438   Typical Air Flow Test Stand, 9461M40
Subtask 72-00-04-420-146
T.Install the C-sump cover (0150C), the lube nozzle (01509), the oil nozzle (01510), and the eductor nozzle (45-130 , 72-00-02) (SIN 015K3) as follows. Refer to Figure 436.
(1)Prepare to install the C-sump cover (0150C), the lube nozzle (01509), the oil nozzle (01510), and the eductor nozzle (45-130 , 72-00-02) (SIN 015K3) as follows:
Subtask 72-00-04-640-023
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.
(a)Lubricate the ring seal (spring seal) (45-360 , 72-00-02) (SIN 01550) with C02-019  engine oil or C02-023  engine oil.
(b)Lubricate the groove on the forward side of the C-sump cover (0150C) with C02-019  engine oil or C02-023  engine oil.
(c)Lubricate the threads of the nuts (01544) with C02-058  graphite.
(d)Lubricate the preformed packing (45-250 , 72-00-02) (SIN 0155B) with C02-019  engine oil or C02-023  engine oil.
(e)Lubricate the oil nozzle (01510) with C02-019  engine oil or C02-023  engine oil.
(f)Lubricate the preformed packing (45-230 , 72-00-02) (SIN 01555) with C02-019  engine oil or C02-023  engine oil.
(g)Lubricate the lube nozzle (01509) with C02-019   engine oil or C02-023  engine oil.
(h)Lubricate the threads of slabbed-head bolts (bolt) (91250) with C02-058  graphite.
(i)Lubricate the threads of the bolts (015F1) with C02-058  graphite.
Subtask 72-00-04-420-147
(2)Install the C-sump cover (0150C) as follows:
CAUTION:
MAKE SURE THAT YOU INSTALL THE SPRING SEAL (45-360 , 72-00-02) (SIN 01550) WITH THE SPRING SIDE FORWARD.
CAUTION:
DO NOT REMOVE THE NUTS THAT SECURE THE AFT SUMP TO THE TRF.
(a)Install the spring seal (45-360 , 72-00-02) (SIN 01550) into the groove of the No. 5 bearing housing (01501) with the spring side forward. Refer to Figure 436.
(b)Remove the nuts (item 2) of the 11C4292   installation fixture at four locations that seat the carbon seal (01558).
(c)Align the C-sump cover (0150C) with the lube nozzle holes and install it over the carbon seal (01558).
CAUTION:
NO CLEARANCE BETWEEN THE FLANGE OF THE OIL NOZZLE (01510) AND THE C-SUMP COVER (0150C) IS PERMITTED. IMPROPER INSTALLATION OF THE OIL NOZZLE (01510) CAN CAUSE ENGINE FAILURE.
(d)Use a 0.001 inch (0.03 mm) shim to make sure that there is no clearance between the flange of the oil nozzle (01510) and the C-sump cover (0150C).
(e)If a clearance is found, replace the oil nozzle (01510).
(f)Install the nuts (01544) at 12 locations on the bolts (01522), and tighten hand-tight. Do not torque the nuts at this time. Do not install the nuts (01544) at four locations on either side of the location where you will install the connector supply tubes 2 and 3 (443A2, 443A3).
Subtask 72-00-04-420-160
* * * PRE SB   72-0039( Old Oil Nozzle Design )
(3)Install the No. 5 bearing carbon seal oil nozzle (oil nozzle) (45-240 , 72-00-02) as follows:
(a)Install the preformed packing (45-250 , 72-00-02) (SIN 0155B) on the forward side of the oil nozzle.
(b)Install the oil nozzle over the studs of the C-sump cover (0150C) at approximately the 7:00 o'clock position AFT.
(c)Attach the oil nozzle to the C-sump cover with two nuts (01544). Hand tighten the nuts. Do not torque the nuts at this time.
* * * END PRE SB   72-0039
Subtask 72-00-04-420-161
* * * SB   72-0039( New Oil Nozzle Design )
(3).A.Install the oil nozzle (45-241 , 72-00-02) as follows:
(a)Install the preformed packing (45-250 , 72-00-02) (SIN 0155B) on the forward side of the oil nozzle.
(b)Install the oil nozzle on the studs of the C-sump cover (0150C) at the 7:00 o'clock position ALF approximately.
(c)Attach the oil nozzle to the C-sump cover with a nut (01544). Hand tighten the nut. Do not torque the nut at this time.
(d)Install the nut (01544) on the remaining bolt (01522). Hand tighten the nut. Do not torque the nut at this time.
* * * END SB   72-0039
Subtask 72-00-04-420-162
(4)Install the No. 5 bearing assembly oil nozzle (lube nozzle) (01509) as follows:
(a)Install the preformed packing (45-230 , 72-00-02) (SIN 01555) on the forward side of the lube nozzle (01509).
(b)Install the lube nozzle (01509) over the studs of the C-sump cover (0150C) at approximately the 5:00 o'clock position (aft looking forward).
(c)Make sure that the oil jet holes of the lube nozzle are facing inward.
(d)Attach the lube nozzle to the C-sump cover with two nuts (01544). Tighten the nuts hand-tight.
(5)Torque the nuts (01544) at 16 locations in a criss-cross pattern to 202-238 lb in. (22.8-26.9 N.m).
(6)Torque the nuts (01544) again at 16 locations in a criss-cross pattern to 203-238 lb in. (22.8-26.9 N.m).
(7)Torque the nuts (01544) at 16 locations in a circular pattern to 203-238 lb in. (22.8-26.9 N.m).
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 THIS PRODUCT.
(8)Apply C02-058  graphite to the threads and friction surfaces of self-locking nuts (nuts) (45-380 , 72-00-02) (SIN 912K1) or (45-384 , 72-00-02) (SIN 912K1).
(9)Install the slab-head bolt (bolt) (45-370 , 72-00-02) (SIN 912F0) with the push on nuts (45-480 , 72-00-02) (SIN 912K0) and the nuts (45-380 , 72-00-02) (SIN 912K1) or (45-384 , 72-00-02) (SIN 912K1) to the C-sump cover (45-210 , 72-00-02) (SIN 0150C) aft flange as follows:
NOTE:
The 12 nuts (45-380, 72-00-02) (SIN 912K1) or (45-384, 72-00-02) (SIN 912K1) may not be present, they are part of a ship loose kit, P/N 738L558G01, and may have been removed and kept with the exhaust CVTE or received separately. Refer to GEnx-1B SB 72-0410.
(a)Install the bolts (45-370 , 72-00-02) (SIN 912F0), the push on nuts (45-480 , 72-00-02) (SIN 912K0), and the nuts (45-380 , 72-00-02) (SIN 912K1) or (45-384 , 72-00-02) (SIN 912K1) at 12 locations on the aft flange of the C-sump cover. Make sure the boltheads are forward and the flats of the bolts face inward.
(b)Do not tighten the nuts (45-380 , 72-00-02) (SIN 912K1) or (45-384 , 72-00-02) (SIN 912K1) on the bolts (45-370 , 72-00-02) (SIN 912F0) if they are present and they are not being shipped loose.
(10)Install the eductor nozzle (45-130 , 72-00-02) (SIN 015K3) as follows:
NOTE:
SB 72-0090 eductor nozzle has an alignment tab to prevent incorrect installation.
(a)Install the oil seal (45-140 , 72-00-02) (SIN 015K4) into the opening at the 12:00 o'clock position on the C-sump cover (0150C).
CAUTION:
MAKE SURE THAT YOU INSTALL THE EDUCTOR NOZZLE WITH THE NOZZLE POINTING AFT. AN INCORRECT ORIENTATION CAN RESULT IN OIL LEAKS.
(b)Install the eductor nozzle in the oil seal and down through the C-sump cover and out the aft end.
(c)Make sure that the eductor nozzle is installed with the nozzle pointing in the aft direction. Refer to Figure 439.
(d)Attach the eductor nozzle to the C-sump cover with the bolts (015F1) at two locations.
(e)Torque the bolts (015F1) to 106-124 lb in. (12.0-14.0 N.m).
* * * FOR ALL
Figure 439   (Sheet 1 ) Installation of the Eductor Nozzle on the C-Sump Cover
* * * FOR ALL
* * * PRE SB   72-0090( Eductor Nozzle without Installation Tab )
Figure 439   (Sheet 2 ) Installation of the Eductor Nozzle on the C-Sump Cover
* * * FOR ALL
* * * SB   72-0090( Eductor Nozzle with Installation Tab )
Figure 439   (Sheet 3 ) Installation of the Eductor Nozzle on the C-Sump Cover
Subtask 72-00-04-420-148
U.Install the aft sump tubes in the TRF assembly. Refer to Figure 440 and do as follows:
(1)Install the bracket (61BE0) to the TRF assembly as follows:
(a)Attach the bracket (61BE0) to the TRF assembly with two bolts (61BF0).
(b)Torque the two bolts (61BF0) to 106-124 lb in. (12.0-14.0 N.m).
(c)Attach bracket (61BE2) to bracket (61BE0) with two bolts (61BF4). Tighten the bolts hand-tight.
(2)Install the eductor air tube (61BA1) as follows:
(a)Connect the eductor air tube (45-030 , 72-00-02) (SIN 61BA1) to the TRF (01-010 , 72-57-00) (SIN 940A0) or (01-011 , 72-57-00) (SIN 940A0) strut No. 3 internal tube, CCW from the 12:00 o'clock position (aft looking forward). Tighten the B-nut hand-tight.
(b)Install the ring seal (45-120 , 72-00-02) (SIN 61BN0) between the eductor air tube and the eductor nozzle (45-130 , 72-00-02) (SIN 015K3).
(c)Install the coupling clamp (61BV1) around the eductor air tube and the eductor nozzle. Make sure the hinge is aligned so the nut is pointing in the 3:00 o'clock direction (aft looking forward).
(3)Attach the eductor air tube (61BA1) to the bracket (61BE0) with a retaining strap (61BV0) and two bolts (61BF4).
(4)Torque the connectors as follows:
(a)Torque the B-nut on the eductor air tube (61BA1) as follows:
1Torque the B-nut to 110-130 lb ft (149.7-175.7 N.m).
2Loosen the B-nut and torque it again to 110-130 lb ft (149.7-175.7 N.m).
3Re-apply torque to 110 to 130 lb ft (149.7 to 175.7 N.m).
(b)Torque the nut on the clamp (61BV1) to 60-70 lb in. (6.8-7.9 N.m).
(c)Torque the four bolts (61BF4) to 106-124 lb in. (12.0-14.0 N.m).
(5)Install the connector supply tube 2 (supply tube 2) (45-160 , 72-00-02) (SIN 443A2) or (45-160A , 72-00-02) (SIN 443A2) and connector supply tube 3 (supply tube 3) (45-170 , 72-00-02) (SIN 443A3) as follows:
(a)If the LPT module assembly was removed to make access easier to other areas of the engine, without an overhaul of the TRF assembly during the engine shop visit, make sure to do a check of the installation torque between the parts that follow. Refer to TASK 72-57-00-440-801 (72-57-00, ASSEMBLY 001).
No. 5 bearing housing (01-050 , 72-57-00) (SIN 01501) and tube (01-160 , 72-57-00) (SIN 443A0)
Tube (01-160 , 72-57-00) (SIN 443A0) and supply assembly tube (oil supply tube) (01-170 , 72-57-00) (SIN 443A1)
No. 5 bearing housing (01-050 , 72-57-00) (SIN 01501) and tube (01-330 , 72-57-00) (SIN 452A0)
Tube (01-330 , 72-57-00) (SIN 452A0) and scavenge assembly tube (01-340 , 72-57-00) (SIN 452A1).
(b)Connect the B-nut of the A/O seal nozzle (oil nozzle) (45-241 , 72-00-02) (SIN 01510) at the 7:00 o'clock position to the supply tube 2 (45-160 , 72-00-02) (SIN 443A2).
(c)Connect the B-nut of the supply tube 2 (45-160 , 72-00-02) (SIN 443A2) to the oil supply tube (01-160 , 72-57-00) (SIN 443A0).
(d)Connect the B-nut of the supply tube 3 (45-170 , 72-00-02) (SIN 443A3) to the supply tube 2 (45-160 , 72-00-02) (SIN 443A2).
(e)Connect the B-nut of the A/O No. 5 nozzle (lube nozzle) (45-220 , 72-00-02) (SIN 01509) at the 5:00 o'clock position to the supply tube 3 (45-170 , 72-00-02) (SIN 443A3).
(f)Torque the B-nut of the oil nozzle (45-241 , 72-00-02) (SIN 01510) to the supply tube 2 (45-160 , 72-00-02) (SIN 443A2) as follows:
1Torque the B-nut to 262 to 308 lb in. (29.6 to 34.8 Nm).
2Loosen the B-nut and torque again to 262 to 308 lb in. (29.6 to 34.8 Nm).
3Torque the B-nut again to 262 to 308 lb in. (29.6 to 34.8 Nm).
(g)Torque the B-nut of the lube nozzle (45-220 , 72-00-02) (SIN 01509) to the supply tube 3 (45-170 , 72-00-02) (SIN 443A3) as follows:
1Torque the B-nut to 262 to 308 lb in. (29.6 to 34.8 Nm).
2Loosen the B-nut and torque again to 262 to 308 lb in. (29.6 to 34.8 Nm).
3Torque the B-nut again to 262 to 308 lb in. (29.6 to 34.8 Nm).
(h)Torque the B-nut of the supply tube 2 (45-160 , 72-00-02) (SIN 443A2) to the oil supply tube (01-160 , 72-57-00) (SIN 443A0) as follows:
1Torque the B-nut to 262 to 308 lb in. (29.6 to 34.8 Nm).
2Loosen the B-nut and torque again to 262 to 308 lb in. (29.6 to 34.8 Nm).
3Torque the B-nut again to 262 to 308 lb in. (29.6 to 34.8 Nm).
NOTE:
(HES)Torque the B-nut of the supply tube 3 (45-170, 72-00-02) (SIN 443A3) to the supply tube 2 (45-160, 72-00-02) (SIN 443A2) as follows. Refer to Case No. 02106621.
1 Torque the B-nut to 262 to 308 lb in. (29.6 to 34.8 Nm).
2 Loosen the B-nut and torque again to 262 to 308 lb in. (29.6 to 34.8 Nm).
3 Torque the B-nut again to 262 to 308 lb in. (29.6 to 34.8 Nm).
* * * FOR ALL
Figure 440   (Sheet 1 ) Installation of the Aft Sump Tubes
* * * FOR ALL
Figure 440   (Sheet 2 ) Installation of the Aft Sump Tubes
* * * FOR ALL
Figure 440   (Sheet 3 ) Installation of the Aft Sump Tubes
Subtask 72-00-04-780-006
WARNING:
BE CAREFUL WHEN YOU APPLY PRESSURE. MAKE SURE YOU DO NOT USE MORE THAN THE MAXIMUM PRESSURE. ALWAYS USE SAFETY SHIELDS DURING THE TEST. RELEASE PRESSURE BEFORE YOU DISCONNECT THE LINES AND FITTINGS. A MALFUNCTION CAN CAUSE AN INJURY OR CAN KILL YOU.
(6)Pressure check the aft oil supply system as follows:
(a)Attach a supply of clean, dry compressed air to the oil supply tube (443A1) fitting at 6:00 o'clock on the TRF. Refer to Figure 442.
(b)Apply and keep a minimum air pressure of 10 PSIG (69.0 Kpa gage) to the oil supply system.
(c)Apply a leak detection fluid to the aft oil supply lines inside the TRF and on the three fittings on the tubes (443A1, 443A2).
(d)When the test is completed, release the pressure and remove any test hoses from the aft oil supply system.
(e)Deleted.
CAUTION:
YOU MUST INSTALL THE FACTORY CRIMPED END OF THE C10-143   SAFETY CABLE ON THE TUBE BOSS HOLE. DO NOT INSTALL THE FACTORY CRIMPED END ON THE B-NUT SIDE OF THE TUBE OR ENGINE DAMAGE CAN OCCUR.
(f)Safety the B-nuts with C10-143   safety cable. Install the factory crimped end of the safety cable on the tube boss hole. Do not install the factory crimped end on the B-Nut side of the tube.
(7)Flow check the aft oil supply system as follows:
(a)Attach a supply of clean, dry, compressed air to the 9461M40   air flow test stand. Refer to Figure 438.
(b)Connect the 9429M71   universal adapter kit to the oil supply tube (443A1) fitting at the 6:00 o'clock position on the TRF assembly.
(c)Attach the 9461M40   air flow test stand to the 9429M71   universal adapter kit.
(d)Apply and keep a pressure of 9.5-10.5 psig (65.5-72.4 kPa gage). The flow rate must be 1.9-4.3 SCFM (54-122 Lpm) at ambient conditions 50°F-100°F (10°C-38°C) and 14.2-15.2 psia.
(e)When the test is completed, release the pressure from the 9461M40   air flow test stand.
(f)Disconnect the 9461M40   air flow test stand and 9429M71   universal adapter kit from the TRF.
Subtask 72-00-04-420-149
(8)Install the insulation blankets (443W4, 443W5) on tube (443A3) as follows:
WARNING:
DELETED.
WARNING:
DELETED.
(a)Deleted.
WARNING:
DELETED.
(b)Deleted.
(c)Deleted.
WARNING:
DELETED.
(d)Deleted.
(e)Install the insulation blanket (45-180 , 72-00-02) (SIN 443W4) to the top of the tube (45-170 , 72-00-02) (SIN 443A3).
(f)Install the insulation blanket (45-190 , 72-00-02) (SIN 443W5) to the bottom of the tube (45-170 , 72-00-02) (SIN 443A3).
(g)Attach the insulation blankets (443W4, 443W5) to the tube (443A3) with two tiedown straps (45-200 , 72-00-02) (SIN 443Y0). Fully tighten the tiedown straps.
(h)Deleted.
(9)Install the supply insulations (insulation blankets) (443W8, 443W9) on the tube (443A2) as follows. Refer to Figure 440.
WARNING:
DELETED.
WARNING:
DELETED.
(a)Deleted.
WARNING:
DELETED.
(b)Deleted.
(c)Deleted.
WARNING:
DELETED.
(d)Deleted.
(e)Install the insulation blanket (45-460 , 72-00-02) (SIN 443W8) to the top of the tube (45-160 , 72-00-02) (SIN 443A2).
(f)Install the insulation blanket (45-470 , 72-00-02) (SIN 443W9) to the bottom of tube (45-160 , 72-00-02) (SIN 443A2).
(g)Attach the insulation blankets to the tube (443A2) with two tiedown straps (45-200 , 72-00-02) (SIN 443Y0). Fully tighten the tiedown straps.
(h)Deleted.
(10)Install the supply insulation blankets (insulation blankets) (443W0, 443W1, 443W2, 443W3) on the connector supply 1 assembly tube (tube) (443A0) as follows. Refer to Figure 441.
WARNING:
DELETED.
WARNING:
DELETED.
(a)Deleted.
WARNING:
DELETED.
(b)Deleted.
(c)Deleted.
WARNING:
DELETED.
(d)Deleted.
(e)Install the insulation blankets (01-230 , 72-57-00) (SIN 443W0) and (01-250 , 72-57-00) (SIN 443W2) to the top of the tube (01-160 , 72-57-00) (SIN 443A0).
(f)Install the insulation blankets (01-240 , 72-57-00) (SIN 443W1) and (01-260 , 72-57-00) (SIN 443W3) to the bottom of the tube (01-160 , 72-57-00) (SIN 443A0).
(g)Attach the insulation blankets to the tube (443A0) with two tiedown straps (45-200 , 72-00-02) (SIN 443Y0). Fully tighten the tiedown straps.
(h)Deleted.
(11)Install the supply insulations (insulation blankets) (443W6, 443W7) on tube 443A0 as follows. Refer to Figure 441.
(a)Install insulation blanket (443W6) to the top of the tube (443A0).
(b)Install insulation blanket (443W7) to the bottom of the tube (443A0).
(c)Attach the insulation blankets to the tube (443A0) with two tiedown straps (45-200 , 72-00-02) (SIN 443Y0).
(12)Install the insulation scavenge blankets (insulation blankets) (452W0, 452W1, 452W2, 452W3) on the connector scavenge assembly tube (tube) (452A0) as follows. Refer to Figure 441.
WARNING:
DELETED.
WARNING:
DELETED.
(a)Deleted.
WARNING:
DELETED.
(b)Deleted.
(c)Deleted.
WARNING:
DELETED.
(d)Deleted.
(e)Install the insulation blankets (01-370 , 72-57-00) (SIN 452W0) and (01-390 , 72-57-00) (SIN 452W2) to the top of the tube (01-330 , 72-57-00) (SIN 452A0).
(f)Install the insulation blankets (01-380 , 72-57-00) (SIN 452W1) and (01-400 , 72-57-00) (SIN 452W3) to the bottom of the tube (01-330 , 72-57-00) (SIN 452A0).
(g)Attach the insulation blankets to the tube (452A0) with two tiedown straps (452Y0). Fully tighten the tiedown straps.
(h)Deleted.
* * * FOR ALL
Figure 441   (Sheet 1 ) Tubes and Connector Drain Assembly Tube
* * * FOR ALL
Figure 441   (Sheet 2 ) TRF Oil Supply, Oil Scavenge, and Vent Drain
* * * FOR ALL
Figure 441   (Sheet 3 ) TRF Oil Supply, Oil Scavenge, and Vent Drain
* * * FOR ALL
Figure 442   Pressure Check at the TRF Oil Supply Fitting