Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 72-32-00-430-003 LPC/Intermediate Case Module - Install The No. 3 Bearing, Internal Gearbox And Support Assembly, Assembly-003
General
This TASK gives the procedure to install the No.3 bearing, internal gearbox and support assembly. For other parts of the LP compressor/intermediate case module, refer to TASK 72-32-00-430-000 (72-32-00 ASSEMBLY-00).
Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.
For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.
For standard torque data and procedures, refer to the SPM TASK 70-41-00-400-501 and TASK 70-41-02-400-501.
To identify, lubricate and install seal rings, refer to the SPM TASK 70-44-01-400-501.
Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.
The abbreviation Intf shows an interference or tight fit. This causes REJECT IF MORE THAN to become REJECT IF IF LESS THAN. The abbreviation Clear shows a clearance fit.
The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.
The No.1 strut, which is the top position strut of the fan frame assembly, is identified by the five pressure tubes on the strut leading edge.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| IAE 1J12024 Special wrench | 0AM53 | IAE 1J12024 | 1 | |
| IAE 1J12326 Vertical sling | 0AM53 | IAE 1J12326 | 1 | |
| IAE 1J12505 0AM53 heater | 0AM53 | IAE 1J12505 | 1 | |
| IAE 6F10027 Heater control unit | 0AM53 | IAE 6F10027 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-149 DRY ICE | LOCAL | CoMat 02-149 | ||
| CoMat 10-077 APPROVED ENGINE OILS | LOCAL | CoMat 10-077 |
Safety Requirements
NONEProcedure
Refer to Figure.
Reference dimensions at location 0308. If required, use the data written as a NOTE in TASK 72-32-03-200-000 (INSPECTION/CHECK-000) and TASK 72-32-22-200-000 (INSPECTION/CHECK-000).
Table 1. Fits and Clearances (all dimensions are in inches) NEW PART WORN PART
DIMENSIONS DIMENSIONS REJECT IF
PART IDENT Size Clearance (Non-select) MORE THAN
LOCATION 0308
No.3 bearing seal support
ENGINE-NO.3 BEARING SEAL SUPPORT (72-32-22, 01-040) and
fan frame Fan Frame Assembly And Related Parts (72-32-03, 03-100)
No.3 bearing seal support
11.3400
outside diameter
11.3439
0.0000
Fan frame bore diameter
11.3381
0.0058
11.3400
Intf
Table 2. Fits and Clearances (all dimensions are in millimeters) NEW PART WORN PART
DIMENSIONS DIMENSIONS REJECT IF
PART IDENT Size Clearance (Non-select) MORE THAN
LOCATION 0308
No.3 bearing seal support
ENGINE-NO.3 BEARING SEAL SUPPORT (72-32-22, 01-040) and
Fan frame Fan Frame Assembly And Related Parts (72-32-03, 03-100)
No.3 bearing seal support
288.036
outside diameter
288.137
0.000
Fan frame bore diameter
287.986
0.151
288.036
Intf
SUBTASK 72-32-00-220-109 Reference Fits and Clearances of the No.3 Bearing Seal Support and Fan Frame at Location 0308
Refer to Figure.
Make sure that the fan frame assembly is installed horizontally on the turnover stand. Refer to TASK 72-32-00-430-002 (Assembly-002).
SUBTASK 72-32-00-430-097 Turn the Fan Frame Assembly Vertical with the Front End Up
Use CoMat 02-149 DRY ICE to cause the PTO inner seal ring Fan Frame Assembly And Related Parts (72-32-03, 03-050) to be cold, Figure.
Install the IAE 1J12505 0AM53 heater 1 off on to the mounting flange.
Connect the cables of the local heater to the IAE 6F10027 Heater control unit 1 off.
Increase the temperature of the mounting flange on the fan frame assembly, Figure.
NOTE
The support assembly is on the work stand and this time. Refer to TASK 72-32-10-440-001 (ASSEMBLY).Install the seal ring (02-495) into the support assembly, Figure.
Install the IAE 1J12326 Vertical sling 1 off on to the support assembly, Figure.
Lubricate "NO.3 BEARING,ROTOR CENTRE & SUPPORT ASSY (72-32-20, 01-100) packing 1 off with CoMat 10-077 APPROVED ENGINE OILS. Install the packing into the groove in the support assembly, Figure.
Move the support assembly from the work stand to the fan frame assembly.
Remove the vertical sling from the support assembly, Figure.
Install an applicable cover sheet over the openings XX and YY of the No.6 strut so that the bolts do not go accidentally into the strut, Figure.
NOTE
Use the IAE 1J12024 Special wrench 1 off to tighten the three bolts at the holes Z.The two bolts (02-350) that attach the oil filter housing No. 2 And No. 3 Bearing Oil Distributor And Tubes (72-32-36, 01-100) are installed into holes X in TASK 72-32-00-430-004 (ASSEMBLY-004).Put the 14 bolts (02-480) into the holes of the mounting flange of the support assembly, but not into holes X and Y. Tighten the bolts lightly.
Install the NF C and NF D brackets (02-466 and 02-468), Figure. on to the mounting flange of the support assembly with the four bolts (02-472) at holes Y. Tighten the bolts lightly.
NOTE
Use the special wrench (1J12024) to torque the three bolts at holes Z.Torque the 18 bolts (02-480 and 02-472) to 180 to 220 1bfin (22.00 and 25.00 Nm). Refer to Figure for the bolt torque sequence.
SUBTASK 72-32-00-430-098 Install the Support Assembly (No. 3 Bearing, Internal Gearbox and Support Assembly) into the Fan Frame Assembly
Figure: Locations for the fits and clearances
Locations for the fits and clearances

Figure: Install the lock pin into position to lock the handle of the turnover stand
Install the lock pin into position to lock the handle of the turnover stand

Figure: Install the No.3 bearing, internal gearbox and support assembly into the fan frame assembly
Install the No.3 bearing, internal gearbox and support assembly into the fan frame assembly

Figure: Use the local heater to increase the temperature of the mounting flange on the fan frame assembly
Use the local heater to increase the temperature of the mounting flange on the fan frame assembly

Figure: Remove the No.3 bearing, internal gearbox and support assembly from the work stand
Remove the No.3 bearing, internal gearbox and support assembly from the work stand

Figure: Install a cover sheet to the openings of the fan frame assembly
Install a cover sheet to the openings of the fan frame assembly

Figure: Position of the NF C and NF D brackets and bolt torque sequence
Position of the NF C and NF D brackets and bolt torque sequence

