TASK 79-22-41-200-412-B00 Oil Scavenge Pump - Related Parts - Examine The Spacer Assembly, Inspection-012

DMC:V2500-A0-79-22-4100-11B-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 79-22-41-200-412-B00 Oil Scavenge Pump - Related Parts - Examine The Spacer Assembly, Inspection-012

Effectivity

FIG/ITEM

PART NO.

01-590

4B7322

01-590

4B7346

General

This TASK gives the procedure for the inspection of the spacer 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.

Do dimensional inspections only if the visual inspection or some other condition makes it necessary.

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

A ** following repair referenced in this inspection indicates that the repair is not yet published in the current revision of the manual and the part must be rejected. Contact IAE for additional information concerning FAA approved repair date.

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 79-22-41-230-055 Do a Crack Test on the Spacer Assembly (Fluorescent Penetrant)

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

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

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

          1. Cracked

          1. Reject

          2. Trough porosity

          1. Reject

    2. SUBTASK 79-22-41-220-122 Examine the Spacer Assembly Spacer Face at Location 1

    1. Refer to Figure.

      2. Surface finish

        1. If surface finish does not exceed 40 micro-inches (1 micro-meter).

        1. Accept

          2. More than Step.

          1. Repair, VRS5359 (Repair-022) TASK 79-22-41-300-022.

      3. Pitted

        1. Pits less than 0.01 in. (0.02 mm) are acceptable providing they do not create a by-pass between different pressure areas

        1. Accept

        2. Pits having the appearance of undermining, which might cause the loss of metal in sizable pieces.

        1. Reject

      4. Perpendicularity

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

        1. Accept

          2. More than Step.

          1. Repair, VRS5361 (Repair-024) 79-22-41-300-024**.

      5. Run-out

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

        1. Accept

          2. More than Step

          1. Repair, VRS5361 (Repair-024) 79-22-41-300-024**.

    3. SUBTASK 79-22-41-220-123 Examine the Spacer Assembly Protective Finish

      1. Light corrosion or pitting

      1. Repair, VRS5360 (Repair-023) TASK 79-22-41-300-023.

    4. SUBTASK 79-22-41-220-124 Examine the Spacer Assembly Bush at Location 2

    1. Refer to Figure.

      2. Inner diameter

        1. Between 0.8677 and 0.8683 in. (22.040 and 22.055 mm).

        1. Accept

        2. More than 0.8683 in. (22.055 mm).

        1. Reject

      3. Perpendicularity

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

        1. Accept

        2. More than Step.

        1. Reject

      4. True position

        1. In a diameter of 0.001 in. (0.025 mm) FIR in relation to surface B.

        1. Accept

          2. More than Step.

          1. Reject

    5. Figure: Locations on the Spacer Assembly

    Locations on the Spacer Assembly

Requirements After Job Completion

Follow-On Conditions

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