TASK 71-00-02-400-003 (A1/A5-PPBU) - Install The Load Share Fittings, Installation-003

DMC:V2500-A0-71-00-0200-02A-720A-B|Issue No:001.00|Issue Date:2014-05-01

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 71-00-02-400-003 (A1/A5-PPBU) - Install The Load Share Fittings, Installation-003

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.

For standard torque data and procedures, refer to the SPM TASK 70-41-00-400-501 and TASK 70-41-02-400-501.

Special torque data and assembly tolerances are included in the procedure.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-039 ENGINE OIL, unless other lubricants are referred to in the procedure.

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.

Transportation covers/blanks must be removed immediately before the installation of the components.

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 10-039 ENGINE OILLOCALCoMat 10-039

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 71-00-02-450-001 Install the Load Share Fittings

    2. Refer to Figure.

    3. Locate the six bolt holes in the engine at PPS 175.18 and 78 degrees, 38 minutes and 24 seconds radial (left side 281 degrees, 21 minutes and 36 seconds radial).

    4. Install the six bolts Thrust Reverser Load Share Fittings (71-00-22, 01-020) and six 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), the shim Thrust Reverser Load Share Fittings (71-00-22, 01-050) and the five shims Thrust Reverser Load Share Fittings (71-00-22, 01-040) to the engine.

    5. Torque the bolts Thrust Reverser Load Share Fittings (71-00-22, 01-020) to between 75 and 85 lbfin (8.5 and 9.6 Nm).

  1. Figure: Install the Load Share Fitting

    Install the Load Share Fitting

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 10-039
Type:sp01
Supply Short Name:
Supply Name:CoMat 10-039 ENGINE OIL
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
LOCAL