TASK 72-32-71-200-005 LPC Bleed Valve Pin Stud - Examine, Inspection-005

DMC:V2500-A0-72-32-7163-00A-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 72-32-71-200-005 LPC Bleed Valve Pin Stud - Examine, Inspection-005

Effectivity

FIG/ITEM

PART NO.

01-500

5A3690

01-550

5A3684

General

This TASK gives the procedure for the inspection of the stud pin. For the other bleed valve and support arms parts, refer to TASK 72-32-71-200-000 (INSPECTION-000).

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 the SPM TASK 70-20-01-200-501.

All the parts must be cleaned before any part is examined. Refer to TASK 72-32-71-100-000 (CLEANING-000).

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

The procedure for those parts which must have a crack test is given in Step. Do the test before the part is visually examined.

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 the 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

Inspection of Parts, SPM TASK 70-20-01-200-501

Some data on these items are 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
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent penetrant inspection equipment

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-71-230-058 Examine the Stud Pin (01-500 and 01-550) for Cracks

    2. Clean the parts. Refer to TASK 72-32-71-100-000 (CLEANING-000).

      1. Do the test for cracks on the parts that are given below.

        PART IDENT

        TASK/SUBTASK

        Stud pin

        1. Cracked

        2. Reject

    1. SUBTASK 72-32-71-220-076 Examine the Stud Pin (01-500) Stem at Location 1

    2. Refer to Figure.

      1. Worn.

        1. If the diameter is not less than 0.312 in. (7.923 mm)

        2. Accept

        1. If the diameter is less than 0.312 in. (7.923 mm)

        2. Reject

    1. SUBTASK 72-32-71-220-077 Examine the Stud Pin (01-550) Stem at Location 1

    2. Refer to Figure

      1. Worn.

        1. If the diameter is not less than 0.500 in. (12.682 mm)

        2. Accept

        1. If the diameter is less than 0.500 in. (12.682 mm)

        2. Reject

    1. SUBTASK 72-32-71-220-078 Examine the Stud Pin (01-500 and 01-550) Face at Location 2

    2. Refer to Figure and Figure.

      1. Worn.

        1. Up to 0.012 in. (0.31 mm) in depth

        2. Accept

        1. More than in Step

        2. Reject

    1. SUBTASK 72-32-71-220-079 Examine the Stud Pin (01-500 and 01-550) Thread at Location 3

    2. Refer to Figure and Figure.

      1. Crossed

      2. Reject

      1. Stripped

      2. Reject

    1. SUBTASK 72-32-71-220-080 Examine the Stud Pin (01-500 and 01-550) Groove at Location 4

    2. Refer to Figure

      1. Worn.

        1. If the width of groove is between 0.039 and 0.042 in. (0.99 and 1.07 mm)

        2. Accept

        1. More than 0.042 in. (1.07 mm)

        2. Reject

    1. SUBTASK 72-32-71-220-145 Examine the Stud Pin (01-500 and 01-550) Groove at Location 4

    2. Refer to Figure.

      1. Crossed

      2. Reject

      1. Stripped

      2. Reject

  1. Figure: Locations on the stud pin (For 5A3690)

    Locations on the stud pin (For 5A3690)

    Figure: Locations on the stud pin (For 5A3684)

    Locations on the stud pin (For 5A3684)

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Fluorescent penetrant inspection equipment
Tool Name:Fluorescent Penetrant Inspection Equipment