DMC:V2500-A0-72-41-1500-00A-635A-C|Issue No:003|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 72-41-15-300-040 HPC Rotor Blades - (Stages 3 To 12) Restore The Airfoil Surface Condition By Glass/Ceramic Bead Peening, Repair-040 (VRS6150)

Effectivity

FIG/ITEM	PART NO.
01-200	6A3513
01-200	6A3938
01-200	6A8353
01-200	6A8688
01-500	6A3333
01-500	6A3635
01-500	6A3939
01-500	6A4254
Deleted	Deleted
01-500	6A7635
01-500	6A8738
01-800	6A3335
01-800	6A3637
01-800	6A3941
01-800	6A4198
Deleted	Deleted
01-800	6A8449
01-800	6A8451
01-800	6B1346
02-170	6A3338
02-170	6A4902
02-170	6A7406
Deleted	Deleted
02-170	6A8322
02-170	6A8463
02-170	6A8797
02-185	6A3339
02-185	6A4903
02-185	6A7407
Deleted	Deleted
02-185	6A8323
02-185	6A8464
02-185	6A8798
02-200	6A3340C01
02-200	6A4904C01
02-200	6A7405C01
Deleted	Deleted
02-200	6A8320
02-200	6A8461
02-200	6A8732
02-215	6A3340C01
02-215	6A4904C01
02-215	6A7405C01
Deleted	Deleted
02-215	6A8320
02-215	6A8461
02-215	6A8732
02-216	6B1494
02-217	6A3340C02
02-217	6A4904C02
02-217	6A7405C02
Deleted	Deleted
02-217	6A8321
02-217	6A8462
02-217	6A8733
02-270	6A3246
02-270	6A4302
02-270	6A4905
02-270	6A5588
02-270	6A6462
02-270	6A6493
Deleted	Deleted
02-270	6A8314
02-270	6A8743
02-285	6A3247
02-285	6A4906
02-285	6A5589
02-285	6A6463
02-285	6A6494
Deleted	Deleted
02-285	6A8315
02-285	6A8744
02-300	6A3245C01
02-300	6A4907C01
02-300	6A5584C01
02-300	6A6469C01
02-300	6A6492C01
Deleted	Deleted
02-300	6A8312
02-300	6A8741
02-315	6A3245C01
02-315	6A4907C01
02-315	6A5584C01
02-315	6A6469C01
02-315	6A6492C01
Deleted	Deleted
02-315	6A8312
02-315	6A8741
02-316	6B1495
02-317	6A3245C02
02-317	6A4907C02
02-317	6A5584C02
02-317	6A6469C02
02-317	6A6492C02
Deleted	Deleted
02-317	6A8313
02-317	6A8742
02-370	6A3249
02-370	6A4908
02-370	6A5590
02-370	6A6464
02-370	6A6496
Deleted	Deleted
02-370	6A8747
02-385	6A3250
02-385	6A4307
02-385	6A4909
02-385	6A5591
02-385	6A6465
02-385	6A6497
Deleted	Deleted
02-385	6A8748
02-400	6A3248C01
02-400	6A4910C01
02-400	6A5585C01
02-400	6A6470C01
02-400	6A6495C01
Deleted	Deleted
02-400	6A8745
02-415	6A3248C01
02-415	6A4910C01
02-415	6A5585C01
02-415	6A6470C01
02-415	6A6495C01
Deleted	Deleted
02-415	6A8745
02-416	6B1496
02-417	6A3248C02
02-417	6A4910C02
02-417	6A5585C02
02-417	6A6470C02
02-417	6A6495C02
Deleted	Deleted
02-417	6A8746
02-470	6A3252
02-470	6A4366
02-470	6A4420
02-470	6A4726
02-470	6A6566
Deleted	Deleted
02-470	6A8751
02-485	6A3253
02-485	6A4367
02-485	6A4846
02-485	6A5637
02-485	6A5638
02-485	6A5645
Deleted	Deleted
02-485	6A8752
02-500	6A3251C01
02-500	6A4211C01
02-500	6A4365C01
02-500	6A4419C01
Deleted	Deleted
02-500	6A8749
02-515	6A3251C01
02-515	6A4211C01
02-515	6A4365C01
02-515	6A4419C01
Deleted	Deleted
02-515	6A8749
02-517	6A3251C02
02-517	6A4211C02
02-517	6A4365C02
02-517	6A4419C02
Deleted	Deleted
02-517	6A8750
02-570	6A3255
Deleted	Deleted
02-570	6A4727
02-570	6A5639
02-570	6A6563
02-570	6A6567
Deleted	Deleted
02-570	6A8755
02-585	6A3256
02-585	6A4221
02-585	6A5640
02-585	6A5646
Deleted	Deleted
02-585	6A8756
02-600	6A3254C01
02-600	6A4222C01
Deleted	Deleted
02-600	6A8753
02-615	6A3254C01
02-615	6A4222C01
Deleted	Deleted
02-615	6A8753
02-617	6A3254C02
02-617	6A4222C02
Deleted	Deleted
02-617	6A8754
02-670	6A3258
Deleted	Deleted
02-670	6A4728
02-670	6A5641
02-670	6A6564
02-670	6A6568
Deleted	Deleted
02-670	6A8759
02-685	6A3259
02-685	6A4253
02-685	6A5642
02-685	6A5647
Deleted	Deleted
02-685	6A8760
02-700	6A3257C01
02-700	6A4251C01
Deleted	Deleted
02-700	6A8757
02-715	6A3257C01
02-715	6A4251C01
Deleted	Deleted
02-715	6A8757
02-717	6A3257C02
02-717	6A4251C02
Deleted	Deleted
02-717	6A8758
02-770	6A3261
02-770	6A4729
02-770	6A5643
02-770	6A5947
02-770	6A6565
Deleted	Deleted
02-770	6A8763
02-785	6A3262
02-785	6A4206
02-785	6A5644
02-785	6A5648
Deleted	Deleted
02-785	6A8764
02-800	6A3260C01
02-800	6A4207C01
Deleted	Deleted
02-800	6A8761
02-815	6A3260C01
02-815	6A4207C01
Deleted	Deleted
02-815	6A8761
02-817	6A3260C02
02-817	6A4207C02
Deleted	Deleted
02-817	6A8762

Material of component

PART IDENT	RR SYMBOL	MATERIAL
HP Compressor Stage 3 to 8 Blades	TAF or TDY or TTX	Titanium alloy
HP Compressor Stage 9 to 12 Blades	QMP	Nickel alloy

General

This TASK gives the procedure to restore the surface condition of the HP Compressor Stage 3 to 12 Rotor Blade Airfoils by glass bead peening or ceramic bead peening.

This repair must only be done when the instruction to do so is given in the relevant inspection procedures (identified by the applicable part number) located in section 72-41-15.

Each HP Compressor Stage 3 to 12 Blade can only have this repair applied to it three times.

Where reference is made to a SUBTASK within a TASK in the form "TASK, SUBTASK" the operator must read and apply the complete TASK. The SUBTASK is listed only when the TASK gives options for the processing of the component. The specified SUBTASK instructs what option must be used during application of the TASK for the successful completion of the Repair Scheme VRS6150.

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

TASKS identified by SPM TASK are in the Standard Practices Manual (SPM).

Where instructed refer to the following figures for the different stages:

For Stage 3 refer to Figure.

For Stage 4 refer to Figure.

For Stage 5 refer to Figure.

For Stage 6 refer to Figure and Figure.

For Stage 7 refer to Figure and Figure.

For Stage 8 refer to Figure and Figure.

For Stage 9 refer to Figure and Figure.

For Stage 10 refer to Figure and Figure.

For Stage 11 refer to Figure and Figure.

For Stage 12 refer to Figure and Figure.

Price and Availability

Refer to International Aero Engines.

Related Repairs

HP Compressor Stage 3 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-020 (VRS6065).

HP Compressor Stage 4 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-021 (VRS6066).

HP Compressor Stage 5 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-022 (VRS6067).

HP Compressor Stage 6 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-023 (VRS6068).

HP Compressor Stage 7 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-024 (VRS6069).

HP Compressor Stage 8 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-025 (VRS6070).

HP Compressor Stage 9 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-026 (VRS6071).

HP Compressor Stage 10 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-027 (VRS6072).

HP Compressor Stage 11 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-028 (VRS6073).

HP Compressor Stage 12 Rotor Blade - Restore the Surface Finish by Vibro-Polishing, Refer to TASK 72-41-15-300-029 (VRS6074).

NOTE

Equipment and materials necessary to do this repair are in the SPM TASKs given below:

SPM TASK 70-09-00-400-501

SPM TASK 70-11-03-300-503

SPM TASK 70-38-04-300-503

NOTE

It is possible that some materials in the Consumable Materials chart cannot be used for some or all of the necessary applications. Before you use the materials, make sure the types, quantities and applications of the materials necessary are legally permitted in your location. All persons must obey all applicable federal, state, local and provincial laws and regulations when it is necessary to work with these materials.
To identify the consumable materials, refer to the Overhaul Processes and Consumables Index (PCI).
Other necessary consumable materials are referred to in the SPM TASKs.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification
Abrasive Blast Equipment	LOCAL	Abrasive Blast Equipment
Ceramic bead peening equipment	LOCAL	Ceramic bead peening equipment
Chemical cleaning equipment	LOCAL	Chemical cleaning equipment
Glass bead peening equipment	LOCAL	Glass bead peening equipment
Surface finish measuring equipment	LOCAL	Surface finish measuring equipment
Vibrating Marking Pencil	LOCAL	Vibrating Marking Pencil

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 01-293 GLASS BEADS	LOCAL	CoMat 01-293
CoMat 05-140 ABRASIVE STONE SILICON CARBIDE	LOCAL	CoMat 05-140
CoMat 05-184 CERAMIC BEADS	IE460	CoMat 05-184

Spares

NONE

Safety Requirements

NONE

Procedure

1. Refer to the relevant figures listed in Paragraph.
2. 1. Examine the component for the repair identification symbol, 2 and any suffixes.
    If 2 and /2 is engraved adjacent to the part number.
    Reject.
    If there is no repair identification symbol or if 2 is engraved with /1 or with no suffix.
    Continue with the repair.
1. 1. Refer to SPM TASK 70-11-03-300-503.
  2. Use Chemical cleaning equipment.
1. Refer to the relevant figures listed in Paragraph.
2. 1. Refer to SPM TASK 70-38-04-300-503, SUBTASK 70-38-04-300-002.
  2. Use CoMat 01-293 GLASS BEADS.
  3. The glass bead peening process must achieve a datum coverage of 200 percent on the indicated surface(s).
  4. The glass bead peening process should have an Almen intensity of 0.007 in.- 0.011 in. (0.18 mm - 0.28 mm) using Almen strip N.
  5. Use Glass bead peening equipment.
3. Remove and discard the masking tape, if necessary.
1. Refer to the relevant figures listed in Paragraph.
2. 1. Refer to SPM TASK 70-38-04-300-503, SUBTASK 70-38-04-300-001.
  2. Use CoMat 05-184 CERAMIC BEADS.
  3. The ceramic bead peening process must achieve a datum coverage of 200 percent on the indicated surface(s).
  4. The ceramic bead peening process should have an almen intensity of 0.007 in. - 0.011 in. (0.18 mm - 0.28 mm) using Almen strip N.
  5. Use Glass bead peening equipment.
3. Remove and discard the masking tape, if necessary.
1. Deleted.
1. 1. For Stage 3 refer to repair, VRS6065 TASK 72-41-15-300-020 (REPAIR-020).
  2. For Stage 4 refer to repair, VRS6066 TASK 72-41-15-300-021 (REPAIR-021).
  3. For Stage 5 refer to repair, VRS6067 TASK 72-41-15-300-022 (REPAIR-022).
  4. For Stage 6 refer to repair, VRS6068 TASK 72-41-15-300-023 (REPAIR-023).
  5. For Stage 7 refer to repair, VRS6069 TASK 72-41-15-300-024 (REPAIR-024).
  6. For Stage 8 refer to repair, VRS6070 TASK 72-41-15-300-025 (REPAIR-025).
  7. For Stage 9 refer to repair, VRS6071 TASK 72-41-15-300-026 (REPAIR-026).
  8. For Stage 10 refer to repair, VRS6072 TASK 72-41-15-300-027 (REPAIR-027).
  9. For Stage 11 refer to repair, VRS6073 TASK 72-41-15-300-028 (REPAIR-028).
  10. For Stage 12 refer to repair, VRS6074 TASK 72-41-15-300-029 (REPAIR-029).
1. Refer to the relevant figures listed in Paragraph.
  NOTE
  If the HP Compressor Stage 3 to 12 Rotor Blades is already identified with the repair identification symbol, 2 , from a previous repair application, only the suffix number needs to be updated.
2. 1. Refer to SPM TASK 70-09-00-400-501 SUBTASK 70-09-00-400-001.
  2. Use a Vibrating Marking Pencil.
3. 1. If this is the first application of the repair.
    No suffix number is required.
  2. If this is the second application of the repair scheme.
    Vibro-engrave /1 adjacent to the repair identification symbol.
  3. If this is the third application of the repair scheme.
    Strike through the /1 and vibro-engrave /2 adjacent to the repair identification symbol, i.e; 2/2.
4. 1. Use CoMat 05-140 ABRASIVE STONE SILICON CARBIDE.

HP Compressor Stage 3 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 4 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 5 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 6 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 7 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 8 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 9 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 10 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 11 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 12 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 6 To 8 Rotor Blades - Marking Locations

HP Compressor Stage 9 To 12 Rotor Blades - Repair Marking Zones

Legend

HP Compressor Stage 9 To 12 Rotor Blades - Repair Marking Zones

1. Dovetail Side Surface Marking Area. Both Sides Of Dovetail.

2. Platform Underside Surfaces Marking Areas. Do Not Mark On Outer Edges.

3. Dovetail Bottom Surfaces Marking Areas.

4. 0.0315 Inch (0.800 mm) Minimum.

5. Corner Radius Minimum. Both Sides Of Dovetail.

6. Fillet Radius Minimum.

7. Corner Radius Minimum.

8. Distance From Dovetail Fillet Radius To The Projected Dovetail Bottom Surface. Do Not Extend Marking Into The Fillet Radius.

Requirements After Job Completion

Follow-On Conditions

NONE

Manufacturer Code:	IE460
Enterprise Name:	DELETED. REFER TO VENDOR CODE V460V.
BU Name:	DELETED. REFER TO VENDOR CODE V460V.

Manufacturer Code:	LOCAL
Enterprise Name:	LOCALLY SUPPLIED

Manufacturer Code:	LOCAL
Tool Number:	Abrasive Blast Equipment
Tool Name:	Abrasive Blast Equipment

TASK 72-41-15-300-040 HPC Rotor Blades - (Stages 3 To 12) Restore The Airfoil Surface Condition By Glass/Ceramic Bead Peening, Repair-040 (VRS6150)

Export Control

Copyright

Applicability

Common Information

TASK 72-41-15-300-040 HPC Rotor Blades - (Stages 3 To 12) Restore The Airfoil Surface Condition By Glass/Ceramic Bead Peening, Repair-040 (VRS6150)

Effectivity

Material of component

General

NOTE

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-41-15-220-237 Examine for Previous Applications of the Repair

SUBTASK 72-41-15-110-112 Degrease the Component

SUBTASK 72-41-15-380-092 Glass Bead Peen the Airfoil Surfaces

NOTE

SUBTASK 72-41-15-380-094 Ceramic Bead Peen the Airfoil Surfaces

NOTE

SUBTASK 72-41-15-380-093 Restore the Airfoil Surface Condition of the Stage 7, 8, 9, 10, 11 and 12 Rotor Blades

SUBTASK 72-41-15-380-095 Vibro-Polish the Rotor Blade Airfoil

SUBTASK 72-41-15-350-125 Identify the Repair

CAUTION

NOTE

Figure: HP Compressor Stage 3 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 3 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 4 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 4 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 5 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 5 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 6 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 6 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 7 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 7 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 8 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 8 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 9 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 9 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 10 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 10 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 11 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 11 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 12 Rotor Blade - Repair Details and Dimensions

HP Compressor Stage 12 Rotor Blade - Repair Details and Dimensions

Figure: HP Compressor Stage 6 To 8 Rotor Blades - Marking Locations

HP Compressor Stage 6 To 8 Rotor Blades - Marking Locations

Figure: HP Compressor Stage 9 To 12 Rotor Blades - Repair Marking Zones

HP Compressor Stage 9 To 12 Rotor Blades - Repair Marking Zones

Requirements After Job Completion

Follow-On Conditions