TASK 75-32-51-200-402 HPC Stage 7 Solenoid Valve - Related Parts - Examine The Bracket, Inspection-002 - Pre SBE 75-0047

DMC:V2500-A0-75-32-5100-01A-300A-C|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 75-32-51-200-402 HPC Stage 7 Solenoid Valve - Related Parts - Examine The Bracket, Inspection-002 - Pre SBE 75-0047

Effectivity

FIG/ITEM

PART NO.

01-150

5W8314

01-150

6A4680

General

Refer to Inspection-000 TASK 75-32-51-200-400 for the other HP compressor stage 7 solenoid valve parts.

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.

All the parts must be cleaned before they are examined. Refer to Cleaning-000 TASK 75-32-51-100-400.

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

Do not discard the part until you are sure there are not repairs available. Refer to the instructions in repair before a discarded part is used again or oversize parts are installed.

Parts which must 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 are completed satisfactorily.

The practices and processes referred to in the procedure by the TASK/SUBTASK number 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 Policy and Inspection of Parts, SPM TASK 70-20-01-200-501

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

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 75-32-51-230-002 Examine the Bracket for Cracks

      1. Do the crack test on the part that is given below. Use the applicable fluorescent penetrant inspection procedure.

        1. Brackets. Refer to SPM TASK 70-23-02-230-501.

          1. Cracked

          1. Reject

    2. SUBTASK 75-32-51-220-059 Examine the Surface of the Bracket

      1. Examine all the surface

        1. Nicked

          1. Nicked to a depth of 0.002 in. (0.05 mm).

          1. Accept

          2. More than in Step.

          1. Reject

        2. Dented

          1. Dented to a depth of 0.150 in. (3.8 mm) with a large surface area.

          1. Accept

          2. More than in Step.

          1. Reject

        3. Scratched

          1. Scratched to a depth of 0.002 in. (0.05 mm)

          1. Accept

          2. More than in Step.

          1. Reject

    3. SUBTASK 75-32-51-220-060 Examine the Bracket Bolt Hole

      1. Bolt hole burred

      1. Reject

      2. Examine the clip position bolt hole

        1. Worn

          1. If the hole diameter is between 0.221 in. (5.60 mm) and 0.279 in. (7.08 mm) with the distance between the edge of the worn hole and the bracket more than 0.203 in. (5.16 mm).

          1. Accept

          2. Other than in Step.

          1. Reject

      3. Examine the mounting flange bolt hole (stepped part of bracket)

        1. Worn

          1. If the hole diameter is between 0.221 in. (5.60 mm) and 0.279 in. (7.08 mm) with the distance between the edge of the worn hole and the bracket more than 0.058 in. (1.46 mm).

          1. Accept

          2. Other than in Step.

          1. Reject

Requirements After Job Completion

Follow-On Conditions

NONE