TASK 73-22-51-200-102-B00 P4.9 Air Sensor Tubes and Manifolds - Examine the Connector, Inspection-002

DMC:V2500-A0-73-22-5100-01B-310A-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 73-22-51-200-102-B00 P4.9 Air Sensor Tubes and Manifolds - Examine the Connector, Inspection-002

Effectivity

FIG/ITEM

PART NO.

20-310

2A2362

General

This TASK gives the procedure for the inspection of the pressure control tube connector. For other parts of the P4.9 sensor and manifold, refer to Inspection-000 TASK 73-22-51-200-100.

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 70-20-00-200-501.

All the parts must be cleaned before any part is examined. Refer to SPM TASK 70-10-00-100-501.

The procedure for those parts which must have a crack test is given in SPM TASK 70-23-00-230-501. 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 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 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 73-22-51-230-056-001 Examine the Pressure Control Tube Connector (20-310) for Cracks

    1. Clean the part. Refer to Cleaning-000 TASK 73-22-51-100-100.

      2. Do the test for cracks on the part that is given below. Use the applicable penetrant inspection procedure.

        1. Pressure control tube connector. Refer to SPM TASK 70-23-01-230-501.

          1. Cracked

          1. Reject

    2. SUBTASK 73-22-51-230-056-002 Examine the Pressure Control Tube Connector (20-310) for Cracks

    1. Clean the part. Refer to Cleaning-000 TASK 73-22-51-100-100.

      2. Do the test for cracks on the part that is given below. Use the applicable penetrant inspection procedure.

        1. Pressure control tube connector. Refer to SPM TASK 70-23-02-230-501.

          1. Cracked

          1. Reject

    3. SUBTASK 73-22-51-220-070 Examine the Pressure Control Tube Connector (20-310) for Damage to the Conical Seats

    1. Refer to Figure.

      2. Examine the connector at location 1 for damage to the conical seats.

        1. If there is no high metal in the sealing area.

        1. Accept

        2. Other than Step.

        1. Repair, VRS3278 (Repair-005) TASK 73-22-51-300-005.

    4. SUBTASK 73-22-51-220-071 Examine the Pressure Control Tube Connector (20-310) for Damage to the Threads

    1. Refer to Figure.

      2. Examine the connector at location 2 for damage to the threads.

        1. If there is no high metal and the tube thread turns into the mating part freely.

        1. Accept

        2. Other than Step.

        1. Repair, VRS3278 (Repair-005) TASK 73-22-51-300-005.

    5. SUBTASK 73-22-51-220-072 Examine the Pressure Control Tube Connector (20-310) for Damage to the Seal Ring Sealing Surface

    1. Refer to Figure.

      2. Examine the connector at location 3 for damage to the seal ring sealing surface.

        1. If there is no high metal.

        1. Accept.

        2. Other than Step.

        1. Repair, VRS3278 (Repair-005) TASK 73-22-51-300-005.

    6. SUBTASK 73-22-51-220-073 Examine the Pressure Control Tube Connector (20-310) for Leaks

      1. Examine the tube for leaks by pressure test with air.

        1. Leaks at 100 to 120 psig (689.5 to 827.4 kPa).

        1. Reject

    7. Figure: Pressure Control Tube Connector Inspection Locations

    Pressure Control Tube Connector Inspection Locations

Requirements After Job Completion

Follow-On Conditions

NONE