TASK 72-41-22-200-002 HPC Stage 8 Stator Vane - Examine, Inspection-002

DMC:V2500-A0-72-41-2208-00A-300A-C|Issue No:004.00|Issue Date:2021-02-01

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 72-41-22-200-002 HPC Stage 8 Stator Vane - Examine, Inspection-002

Effectivity

FIG/ITEM

PART NO.

03-150

6A3409

03-150

6A4250

03-150

6A7486

03-200

6A3407

03-200

6A4246

03-200

6A7487

03-200

6A8774

03-250

6A3408

03-250

6A4248

03-250

6A7488

03-250

6A8775

03-350

6A3410

03-350

6A4249

03-350

6A7489

03-350

6A8776

03-400

6A3267C01

03-400

6A4245C01

03-400

6A7490C01

03-400

6A8772

03-448

6A3267C01

03-448

6A4245C01

03-448

6A7490C01

03-448

6A8772

03-450

6A3267C02

03-450

6A4245C02

03-450

6A7490C02

03-450

6A8773

General

This TASK gives the procedure for the inspection of the HP compressor stage 8 stator vanes.

Nicks and dents 0.005 in. (0.13 mm) or less are acceptable without limit to the airfoil and gas washed surfaces of the platforms.

Fig/item numbers in parentheses in the procedure agree with those used in the EIPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the EIPC.

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.

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 crack 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 can be shown to be necessary at a subsequent 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/SUBTASK numbers are in the SPM.

References

Refer to 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 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 72-41-22-230-052 Examine the Stage 8 Stator Vanes (03-150, 03-200, 03-250, 03-350, 03-400, 03-448 and 03-450) for Cracks

    1. Clean the parts. Refer to TASK 72-41-22-100-000.

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

        PART IDENT

        TASK/SUBTASK

        Stage 8 Stator Vanes

        1. Cracked.

          1. Airfoil tip.

          1. Refer to Step or Step.

          2. All remaining areas.

          1. Reject.

    2. SUBTASK 72-41-22-220-062-001 Examine the Stage 8 Stator Vanes Concave and Convex Airfoil Surfaces at Locations 1 and 2 (Pre SBE 70-0714 and SBE 70-0726)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Nicked.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than the Step.

        1. Reject.

          NOTE

          A Tallysurf measuring instrument must not be used.

      3. Dented.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than in Step.

        1. Reject.

      4. Examine the surface finish of the vanes. Use 10 percent of the vanes that have been removed.

        1. Surface finish not more than 30 micro-inches (0.80 micrometers)

        1. Accept

        2. More than in Step.

        1. Repair, VRS6081 TASK 72-41-22-300-006 (REPAIR-006)

    3. SUBTASK 72-41-22-220-062-002 Examine the Stage 8 Stator Vanes Concave and Convex Airfoil Surfaces at Locations 1 and 2 (SBE 70-0714 and SBE 72-0561)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Nicked

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than in Step.

        1. Reject.

      3. Dented.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than in Step.

        1. Reject.

      4. Surface finish.

        1. Surface finish of 10 micro-inches (0.25 micrometers) or less

        1. Accept

        2. More than in Step.

        1. Repair, VRS6081 TASK 72-41-22-300-006 (REPAIR-006)

    4. SUBTASK 72-41-22-220-063 Examine the Stage 8 Stator Vanes (72-41-22,03-350) Stop Slot at Location 3

    1. Refer to Figure.

      2. Galled

      1. Reject

      3. Damage.

        1. To the corners of the slot

        1. Reject

    5. SUBTASK 72-41-22-220-064 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22-03-448) and (72-41-22,03-450)) Leading and Trailing Edges at Locations 4 and 5

    1. Refer to Figure, Figure, Figure and Figure.

      2. Nicked

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than the Step.

        1. Reject.

      3. Dented.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than the Step.

        1. Reject.

    6. SUBTASK 72-41-22-220-066 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) Faces at Locations 8 and 9

    1. Refer to Figure.

      2. Galled.

        1. Not more than 0.002 in. (0.05 mm) in depth. This must not be more than 25 percent of the touch area

        1. Accept

        2. Not more than 0.005 in. (0.13 mm) in depth. This must not be more than 25 percent of the touch area and not less than 0.0787 in. (2.000 mm) from face 10

        1. Accept

        3. More than in Step or Step.

        1. Reject

    7. SUBTASK 72-41-22-220-067 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) Faces at Location 10

    1. Refer to Figure.

      2. Galled.

        1. Not more than 0.006 in. (0.15 mm) in depth, not less than 0.040 in. (1.00 mm) away from the land face

        1. Accept

        2. More than in Step.

        1. Reject

    8. SUBTASK 72-41-22-220-108-A00 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) Airfoil Tips at Location 1058 for Cracks and Rubs (A1 parts only)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Cracked

      1. Repair, VRS6061 TASK 72-41-22-300-008 (REPAIR-008)

      3. Rubbed

      1. Repair, VRS6061 TASK 72-41-22-300-008 (REPAIR-008)

    9. SUBTASK 72-41-22-220-108-B00 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) Airfoil Tips at Location 1058 for Cracks and Rubs (A5 parts only) (Pre SBE 70-0714, SBE 70-0714, SBE 70-0726, SBE 72-0441 and SBE 72-0561)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Cracked

      1. Repair, VRS6061 TASK 72-41-22-300-008 (REPAIR-008) or Repair, VRS9535 TASK 72-41-22-300-026 (REPAIR-026).

      3. Rubbed

        1. Tip radius measurement recorded in TASK 72-41-00-040-001-B00 are in limits

        1. Accept

        2. Vanes identified with radius more than the minimum value in TASK 72-41-00-040-001-B00 or vanes not part of a set

        1. Repair, VRS6061 TASK 72-41-22-300-008 (REPAIR-008) or Repair, VRS9535 TASK 72-41-22-300-026 (REPAIR-026).

    10. SUBTASK 72-41-22-220-068 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) Cheeks at Locations 11 to 16

    1. Refer to Figure, Figure, Figure and Figure.

      2. Galled.

        1. Not more than 0.015 in. (0.38 mm) in depth. This must not be in an area more than 50 percent of each surface

        1. Accept

        2. More than in Step.

        1. Reject

    11. SUBTASK 72-41-22-220-070 Examine the Stage 8 Stator Vanes ((72-41-22,03-150), (72-41-22,03-200), (72-41-22,03-250), (72-41-22,03-350), (72-41-22,03-400), (72-41-22,03-448) and (72-41-22,03-450)) at Locations 1125 and 1127

    1. Refer to Figure.

      2. Location 1125.

        1. If the thickness of the land is between 0.0755 in. to 0.0787 in. (1.920 mm to 2.000 mm)

        1. Accept

        2. If the thickness of the land is between 0.0680 in. to 0.0755 in. (1.730 mm to 1.920 mm) over an area of not more than 25 percent

        1. Accept

        3. If the thickness of the land is between 0.0680 in. to 0.0755 in. (1.730 mm to 1.920 mm) over an area of more than 25 percent

        1. Reject

        4. If the thickness of the land is less than the minimum in Step.

        1. Reject

        5. If less than 10 percent reduction in thickness over an area of less than 25 percent

        1. Accept

        6. More than in Step.

        1. Reject

      3. Location 1127.

        1. If the thickness of the land is between 0.0952 in. to 0.0984 in. (2.420 mm to 2.500 mm)

        1. Accept

        2. If the thickness of the land is between 0.0856 in. to 0.0952 in. (2.180 mm to 2.420 mm) over an area of not more than 25 percent

        1. Accept

        3. If the thickness of the land is between 0.0856 in. to 0.0952 in. (2.180 mm to 2.420 mm) over an area of more than 25 percent

        1. Reject

        4. If the thickness of the land is less than the minimum in Step.

        1. Reject

        5. If less than 10 percent reduction in thickness over an area of less than 25 percent

        1. Accept

        6. More than in Step.

        1. Reject

    12. SUBTASK 72-41-22-220-109 Examine the Stage 8 Stator Vanes ((72-41-22,03-200) and (72-41-22,03-250)) Borescope Hole at Location 17

    1. Refer to Figure.

      2. Galled.

        1. Not more than 0.002 in. (0.05 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject

      3. Scored/Scratched.

        1. Not more than 0.002 in. (0.05 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject

    13. SUBTASK 72-41-22-220-215 Examine the Stage 8 Stator Vanes Platform (Annulus Surface) at Location 19 (SBE 70-0714 and SBE 72-0561)

      NOTE

      Class identification marks as scores.

    1. Refer to Figure, Figure, Figure and Figure.

      2. Surface finish.

        1. Surface finish of 16 micro-inches (0.40 micrometers) or less

        1. Accept

        2. More than in Step.

        1. Reject

      3. Nicked.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than Step.

        1. Reject.

      4. Dented.

        1. Up to 0.005 in. (0.13 mm) in depth.

        1. Accept.

        2. More than in Step.

        1. Reject.

      5. Scored/Scratched.

        1. More than 0.005 in. (0.13 mm) in depth

        1. Reject

        2. Not more than 0.005 in. (0.13 mm) in depth

        1. Accept

        3. Airfoil fillet radius

        1. Reject

        4. On face edge

        1. Refer to SPM TASK 70-35-03-300-501 to remove score

        5. Remaining face

        1. Accept

    14. SUBTASK 72-41-22-220-235 Examine the Stage 8 Stator Vanes Platform (Bottom Face)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Part marking and repair symbol location 20.

        1. On face edge

        1. Refer to SPM TASK 70-35-03-300-501 to remove score

        2. Remaining face

        1. Accept

          NOTE

          Class identification marks as scores.

      3. Examine the stage 8 stator vane at location 21.

        1. On face edge

        1. Refer to SPM TASK 70-35-03-300-501 to remove score.

        2. Remaining face

        1. Accept

    15. SUBTASK 72-41-22-220-110 Examine the Stage 8 Stator Vanes (03-150, 03-200, 03-250, 03-350, 03-400, 03-448 and 03-450) all Remaining Surfaces

      1. Nicked, dented or scored/scratched.

        1. Up to 0.005 in. (0.13 mm) in depth

        1. Accept

        2. More than in Step.

        1. Reject

    16. SUBTASK 72-41-22-220-258 Examine the Stage 8 Stator Vanes Chordal Width (A5 only) (Pre SBE 70-0714, SBE 70-0714, SBE 70-0726, SBE 72-0441 and SBE 72-0561)

    1. Refer to Figure.

      2. Minimum chord at Z1 and Z2 at location A and B to the value of X

      1. Accept

      3. Less than value X

      1. Reject

    17. Figure: Stage 8 Stator Vanes - Inspection Locations

    Sheet 1

    Legend
    Stage 8 Stator Vanes - Inspection Locations

    Sheet 1

    Close

    Figure: Stage 8 Stator Vanes - Inspection Locations

    Sheet 2

    Legend
    Stage 8 Stator Vanes - Inspection Locations

    Sheet 2

    Close

    Figure: Stage 8 Stator Vanes - Inspection Locations

    Sheet 3

    Legend
    Stage 8 Stator Vanes - Inspection Locations

    Sheet 3

    Close

    Figure: Stage 8 Stator Vanes - Inspection Locations

    Sheet 4

    Legend
    Stage 8 Stator Vanes - Inspection Locations

    Sheet 4

    Close

    Figure: Stage 8 Stator Vanes - Inspection Locations

    Sheet 5

    Legend
    Stage 8 Stator Vanes - Inspection Locations

    Sheet 5

    Close

    Figure: Stage 8 Stator Vanes - Chordal Checks

    Sheet 6

    Legend
    Stage 8 Stator Vanes - Chordal Checks

    Sheet 6

    Close

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedural steps to add repair reference. (19VG308)