TASK 79-22-43-200-402 Scavenge Oil Filter Housing - Related Parts - Examine The Casing Assembly, Inspection-002

DMC:V2500-A0-79-22-4300-01A-300A-C|Issue No:002.00|Issue Date:2015-02-01

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 79-22-43-200-402 Scavenge Oil Filter Housing - Related Parts - Examine The Casing Assembly, Inspection-002

Effectivity

FIG/ITEM

PART NO.

01-550

4B7215

01-550

4B7382

General

This TASK gives the procedure for the inspection of the casing assembly. For the other parts of the scavenge oil filter housing assembly, refer to Inspection-000 TASK 79-22-43-200-400.

The policy that is necessary for inspection is given in the 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
Workshop inspection equipmentLOCALWorkshop inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 79-22-43-230-052 Do a Crack Test on the Casing Assembly (Fluorescent Penetrant)

    2. Clean the part. Refer to Cleaning-000 TASK 79-22-43-100-400.

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

        1. Casing Assembly. Refer to SPM TASK 70-23-01-230-501.

          1. Cracked

          2. Reject

          1. Trough porosity

          2. Reject

    1. SUBTASK 79-22-43-220-058 Examine the Casing Assembly All Areas

      1. Evident cracks

      2. Reject

    1. SUBTASK 79-22-43-220-059 Examine the Casing Assembly Rough Surfaces at Location 1

    2. Refer to Figure thru Figure.

      1. Nicked, scored, dented or scratched

        1. Any quantity, any length not more than 0.0138 in. (0.35 mm) in depth.

        2. Accept

        1. More than Step.

        2. Repair, VRS5241 (Repair-003) TASK 79-22-43-300-003.

    1. SUBTASK 79-22-43-220-060 Examine the Casing Assembly Machined Seal Surfaces at Location 2

    2. Refer to Figure thru Figure.

      1. Nicked, scored, dented or scratched

        1. Any quantity, any length not more than 0.004 in. (0.1 mm) in depth not extended across the seal surface.

        2. Accept

        1. More than Step.

        2. Repair, VRS5241 (Repair-003) TASK 79-22-43-300-003.

    1. SUBTASK 79-22-43-220-061 Examine the Casing Assembly Machined Seal Surfaces at Location 3

    2. Refer to Figure thru Figure.

      1. Nicked, scored, dented or scratched

        1. Any quantity, any length not more than 0.008 in. (0.2 mm) in depth.

        2. Accept

        1. More than Step.

        2. Repair, VRS5241 (Repair-003) TASK 79-22-43-300-003.

    1. SUBTASK 79-22-43-220-062 Examine the Casing Assembly Protective Finish

      1. Light corrosion or pitting

      2. Repair, VRS5242 (Repair-004) TASK 79-22-43-300-004.

    1. SUBTASK 79-22-43-220-063 Examine the Casing Assembly Helicoil Inserts

      1. Loose, missing or internal thread damage

      2. Repair, VRS5243 (Repair-009) TASK 79-22-43-300-009, or Repair, VRS5656 (Repair-022) TASK 79-22-43-300-022.

    1. SUBTASK 79-22-43-220-064 Examine the Casing Assembly Tank Tube Seat at Location 4

    2. Refer to Figure thru Figure.

      1. Inner diameter

        1. Between 1.458 and 1.46 in. (37.033 and 37.083 mm).

        2. Accept

        1. More than 1.46 in. (37.083 mm)

        2. Repair, VRS5244 (Repair-010) TASK 79-22-43-300-010.

      1. True position

        1. In a diameter of 0.0098 in. (0.25 mm) FIR in relation to Surfaces C and D.

        2. Accept

        1. More than Step.

        2. Repair, VRS5244 (Reapir-010) TASK 79-22-43-300-010.

    1. SUBTASK 79-22-43-220-065 Examine the Casing Assembly Tank Tube Mating Surface at Location 5

    2. Refer to Figure thru Figure.

      1. Perpendicularity

        1. In 0.002 in. (0.05 mm) FIR or less in relation to Surface E.

        2. Accept

        1. More than Step.

        2. Repair, VRS5245 (Repair-011) TASK 79-22-43-300-011.

    1. SUBTASK 79-22-43-220-066 Examine the Casing Assembly Cover Seat at Location 6

    2. Refer to Figure thru Figure.

      1. Inner diameter

        1. Between 1.4181 and 1.4197 in. (36.02 and 36.06 mm).

        2. Accept

        1. More than 1.4197 in. (36.06 mm)

        2. Repair, VRS5246 (Repair-012) TASK 79-22-43-300-012.

      1. True position

        1. In a diameter of 0.0098 in. (0.25 mm) FIR in relation to Surfaces C and D.

        2. Accept

        1. More than Step.

        2. Repair, VRS5246 (Repair-012) TASK 79-22-43-300-012.

    1. SUBTASK 79-22-43-220-069 Examine the Casing Assembly Filter Cover Mating Surface at Location 7

    2. Refer to Figure thru Figure.

      1. Perpendicularity

        1. In 0.0059 in. (0.15 mm) FIR or less in relation to Surface H.

        2. Accept

        1. More than Step.

        2. Repair, VRS5251 (Repair-015) TASK 79-22-43-300-015.

    1. SUBTASK 79-22-43-220-070 Examine the Casing Assembly Filter Cover Seat at Location 8

    2. Refer to Figure thru Figure.

      1. Inner diameter

        1. Between 3.978 and 3.9795 in. (101.08 and 101.08 mm).

        2. Accept

        1. More than 3.9795 in. (101.04 mm).

        2. Repair, VRS5252 (Repair-016) TASK 79-22-43-300-016.

      1. True position

        1. In a diameter of 0.0098 in. (0.25 mm) FIR in relation to Surface H.

        2. Accept

        1. More than Step.

        2. Repair, VRS5252 (Repair-016) TASK 79-22-43-300-016.

      1. Perpendicularity

        1. Less than 0.002 in. (0,05 mm) FIR in relation to Surface D.

        2. Accept

        1. More than Step.

        2. Repair, VRS5252 (Repair-016) TASK 79-22-43-300-016.

    1. SUBTASK 79-22-43-220-071 Examine the Casing Assembly Scavenge Tube Seat at Location 9

    2. Refer to Figure.

      1. Inner diameter

        1. Between 1.458 and 1.46 in. (37.033 and 37.083 mm).

        2. Accept

        1. More than 1.46 in. (37.083 mm).

        2. Repair, VRS5249 (Repair-017) TASK 79-22-43-300-017.

      1. True position

        1. In a diameter of 0.0098 in. (0.25 mm) FIR in relation to surface H

        2. Accept

        1. More than Step.

        2. Repair, VRS5249 (Repair-017) TASK 79-22-43-300-017.

    1. SUBTASK 79-22-43-220-072 Examine the Casing Assembly Scavenge Tube Mating Surface at Location 10

    2. Refer to Figure thru Figure.

      1. Perpendicularity

        1. Less than 0.002 in. (0.05 mm) FIR in relation to Surface G

        2. Accept

        1. More than Step.

        2. Repair, VRS5250 (Repair-018) TASK 79-22-43-300-018.

    1. SUBTASK 79-22-43-220-075 Examine the Casing Assembly Magnetic Chip Detector Housing Seat at Location 11

    2. Refer to Figure thru Figure.

      1. Internal thread damage

      2. Repair, VRS5431 (Repair-020) TASK 79-22-43-300-020.

    1. SUBTASK 79-22-43-220-076 Examine the Casing Assembly Filter Mating Face at Location 12

    2. Refer to Figure thru Figure.

      1. Wear

        1. All quantity all length not more than 0.004 in. (0.1 mm) in depth and 0.098 in. (2.5 mm) in width.

        2. Accept

        1. More than Step.

        2. Repair, VRS5651 (Repair-021) TASK 79-22-43-300-021.

  1. Figure: Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Figure: Oil Filter Casing Assembly (post SBE 79-0101)

    Oil Filter Casing Assembly (post SBE 79-0101)

    Figure: Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Figure: Locations on the Oil Filter Casing Assembly (Post SBE 79-0101)

    Locations on the Oil Filter Casing Assembly (Post SBE 79-0101)

    Figure: Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Locations on the Oil Filter Casing Assembly (pre SBE 79-0101)

    Figure: Locations on the Oil Filter Casing Assembly (post SBE 79-0101)

    Locations on the Oil Filter Casing Assembly (post SBE 79-0101)

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Updated part numbers. Revised figure to add SBE 79-0101 configuration. (EA14VF868)

Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment