TASK 79-22-41-200-406 Oil Scavenge Pump - Related Parts - Examine The Drive Gear Assembly, Inspection-006

DMC:V2500-A0-79-22-4100-05A-300A-C|Issue No:001.00|Issue Date:2013-11-01

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 79-22-41-200-406 Oil Scavenge Pump - Related Parts - Examine The Drive Gear Assembly, Inspection-006

Effectivity

FIG/ITEM

PART NO.

01-240

4B7093

01-160

4B7370

General

CAUTION

GEARS MUST BE REPLACED IN MATCHED SETS IF REPLACEMENT OF ONE OF THE TWO IS NECESSARY.

This TASK gives the procedure for the inspection of the drive gear assembly. For the other parts of the oil scavenge pump assembly, refer to Inspection-000 TASK 79-22-41-200-400.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC.

The policy that is necessary for inspection is given in SPM TASK 70-20-01-200-501.

All parts must be visually examined for damage, corrosion and wear. Any defects that are not identified in the procedure must be referred to IAE.

Do not discard any part until you are sure there are no repairs available. Refer to the instructions in repair before a discarded part is used again or oversize parts are installed.

Parts which should be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.

All parts must be examined to make sure that all the repairs have been completed satisfactorily.

The practices and processes referred to in the procedure by the TASK numbers are in the SPM.

References

Refer to the SPM for data on these items.

Definitions of Damage, SPM TASK 70-02-02-350-501.

Record and Control of the Lives of Parts, SPM TASK 70-05-00-220-501.

Inspection of Parts, SPM TASK 70-20-00-200-501.

Some data on these items is contained in this TASK. For more data on these items refer to the SPM.

Method of Testing for Crack Indications,

Chemical Processes,

Surface Protection.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Demagnetizing unitLOCALDemagnetizing unit
Magnetizing unitLOCALMagnetizing unit
Workshop inspection equipmentLOCALWorkshop inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 79-22-41-240-054 Do a Crack Test on the Drive Gear Assembly (Magnetic)

    2. Clean the part. Refer to Cleaning-000 TASK 79-22-41-100-400.

      1. Do the test for cracks on the part that is given below.

        PART IDENT

        PROCEDURE

        CURRENT/INSPECT

        TASK/SUBTASK

        Drive Gear

        TB

        700A

        Refer to SPM TASK 70-24-01-240-501 SUBTASK 70-24-01-240-011

        Coil

        7000 A/T

        Refer to SPM TASK 70-24-01-240-501 SUBTASK 70-24-01-240-014

        1. Cracked

        2. Reject

    1. SUBTASK 79-22-41-220-085 Examine the Drive Gear Assembly Tip of Tooth at Location 4739

    2. Refer to Figure.

      1. Damage to tip of tooth

        1. Remove the sharp edges or high spots which could damage the mating gear teeth surfaces.

        2. Repair, VRS5344 (Repair-010) TASK 79-22-41-300-010.

      1. Diameter

        1. Between 1.7007 and 1.6998 in. (43.2 and 43.175 mm).

        2. Accept

        1. Less than 1.6998 in. (43.175 mm).

        2. Reject

    1. SUBTASK 79-22-41-220-086 Examine the Drive Gear Assembly Teeth on the Face Surface at Location 1

    2. Refer to Figure.

      1. Scored

        1. Lightly remove raised material. A 32 micro-inches (0.8 micro-meter) finish is required.

        2. Repair, VRS5344 (Repair-010) TASK 79-22-41-300-010.

        1. Chipped, flaking or fretting.

        2. Reject

      1. Damage and obvious sign of wear

        1. Measure the dimension over diametrically opposed with diameter 0.315 in. (8 mm) diameter pins.

          1. Between 1.877 and 1.8679 in. (47.676 and 47.444 mm).

          2. Accept

          1. Less than 1.8679 in (47.444 mm).

          2. Reject

    1. SUBTASK 79-33-41-220-087 Examine the Drive Gear Assembly Teeth on End Surface at Location 2

    2. Refer to Figure.

      1. Scored

        1. Not discernible with a 0.04 in. (1 mm) radius spherical-end.

        2. Accept

        1. Remove raised material with a fine stone.

        2. Repair, VRS5344 (Repair-010) TASK 79-22-41-300-010.

    1. SUBTASK 79-22-41-220-088 Examine the Drive Gear Assembly Spline at Location 4770

    2. Refer to Figure.

      1. Damage and obvious sign of wear

        1. Measure the dimension of all teeth between diametrically opposed, 0.0864 in. (2.194 mm) diameter pins.

          1. Between 0.4747 and 0.4795 in. (12.057 and 12.18 mm).

          2. Accept

          1. More than 0.4795 in. (12.18 mm).

          2. Reject

    1. SUBTASK 79-22-41-220-089 Examine the Drive Gear Assembly Rear and Front Journals at Location 4710 and 4714

    2. Refer to Figure.

      1. Scored

        1. Remove raised metal with a fine stone. Scores must have a circumferential direction. A 10 micro-inches (0.25 micro-meter) finish is required.

        2. Repair, VRS5344 (Repair-010) TASK 79-22-41-300-010.

    1. SUBTASK 79-22-41-220-090 Examine the Drive Gear Assembly Front Bush Journal at Location 4710

    2. Refer to Figure.

      1. Diameter

        1. Between 0.8661 and 0.8653 in. (22 and 21.979 mm).

        2. Accept

        1. Less than 0.8653 in. (21.979 mm).

        2. Reject

      1. Concentricity

        1. In 0.0004 in. (0.01 mm) in relation to surface A.

        2. Accept

        1. More than Step.

        2. Reject

    1. SUBTASK 79-22-41-220-091 Examine the Drive Gear Assembly Rear Bush Journal at Location 4714

    2. Refer to Figure.

      1. Diameter

        1. Between 0.8661 and 0.8653 in. (22 and 21.979 mm).

        2. Accept

        1. Less than 0.8653 in. (21.979 mm).

        2. Reject

  1. Figure: Locations on the Drive Gear Assembly

    Locations on the Drive Gear Assembly

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Demagnetizing unit
Tool Name:Demagnetizing unit
Manufacturer Code:LOCAL
Tool Number:Magnetizing unit
Tool Name:Magnetizing unit
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment