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 71-00-02-000-025 (A1/A5-PPBU) - Remove The Load Share Fittings, Removal-025
General
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.
Apply the approved CoMat 10-058 PENETRATING OIL before the removal of threaded parts and parts with an interference fit. Let the parts soak before removal.
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.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 10-058 PENETRATING OIL | 0AM53 | CoMat 10-058 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Remove the six bolts Thrust Reverser Load Share Fittings (71-00-22, 01-020) and washers Thrust Reverser Load Share Fittings (71-00-22, 01-030) that attach the load share fitting Thrust Reverser Load Share Fittings (71-00-22, 01-010) to the engine at approximately PPS175 and 78 degrees radial (left side approximately 282 degrees radial).
Remove the load share fitting Thrust Reverser Load Share Fittings (71-00-22, 01-010) and the shims Thrust Reverser Load Share Fittings (71-00-22, 01-040) and Thrust Reverser Load Share Fittings (71-00-22, 01-050).
SUBTASK 71-00-02-050-022 Remove the Load Share Fittings
Figure: Remove the Load Share Fitting
Remove the Load Share Fitting
