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 72-45-11-300-001 HPT Stage 1 Hub - Blend Repair, Repair-001 (VRS3184)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-010 | 2A1121 |
01-010 | 2A2021 |
01-010 | 2A2221 |
01-011 | 2A2201 |
01-011 | 2A2801 |
01-011 | 2A5001 |
01-011 | 2A1101 |
01-011 | 2A1801 |
01-011 | 2A1901 |
General
Damage up to 0.001 in. (0.025 mm) is permitted without a repair unless specified differently.
The maximum rotary equipment speed is 18000 RPM.
The practices and processes referred to in the procedure by TASK number are in the SPM.
NOTE
Preliminary Requirements
Pre-Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Make sure that all the cleaning and inspection procedures are done before this repair. |
Support Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-032 CAST STEEL SHOT, S170 | 55807 | CoMat 05-032 | ||
| DELETED | LOCAL | DELETED |
Spares
NONESafety Requirements
CAUTION
Procedure
The Source Demonstration requirements of this repair mean that any facility not authorized to accomplish this repair either utilize the Authorized Repair Vendors listed below or contact IAE Manager Maintenance Operations to determine if a qualification program can be initiated at their facility.
IAE International Aero Engines AG
400 Main Street
M/S 121-10
East Hartford CT 06118
U.S.A.
Attn: Manager Technical Services
Authorized Repair Vendors for the Shot Peen section of Repair VRS3184 are listed below:
Pratt and Whitney Global Service Partners
East Hartford Repair Operations (GSP-EHRO)
400 Main Street, Well No.14 - Mail Stop 117-62
East Hartford, CT 06108
USA
Tel: (860) 557-2646
Fax: (860) 557-2647
Metal Improvements Company Inc. (MIC)
145 Addison Road
P. O. Box 487
Windsor, CT 06095 USA
Tel: (860) 688-6201
Fax: (860) 285-8809
MTU MAINTENANCE HANNOVER GmbH
Flughafen Hannover
Muenchner Strasse 31
D-30855 Langenhagen, Germany
Tel: 49 511 7806 0
Fax: 49 511 7806 111
IHI Corporation
229 Tonogaya,
Mizuho-Machi Nishitama-Gun
Tokyo 190 - 1297
Japan
Tel: 81-42-568-7362
Fax: 81-42-568-7566
ATTN: Program Manager, V2500
Metal Improvements Company Inc. (MIC)
Ascot Drive
Derby DE24 8ST
ENGLAND
ATTN: Program Manager, V2500
Tel: 44-1-332-756-076
Fax: 44-1-332-754-392
Christchurch Engine Centre - CHCEC
115 Orchard Road
Christchurch 8051
New Zealand
The designation by IAE of an authorized repair vendor indicates that the repair vendor has demonstrated the necessary capability to enable it to carry out the listed repair work. However, IAE makes no warranties or representations concerning the qualifications or quality standards of the repair vendors to carry out the repair work, and accepts no responsibility whatsoever for any work that may be carried out by a repair vendor, other than when IAE is listed as the repair vendor. Authorized repair vendors do not act as agents or representatives of IAE.
Repair Facilities
Refer to Figure requirements.
Blend by SPM TASK 70-35-03-300-501.
Remove the rough and unwanted grit until the wheel surface is smooth before you do the blend repair.
The finish marks must follow the lay of the original tool marks.
The minimum blend radius to depth ratio is 30 to 1.
Break all blended area edges 0.003 in. to 0.015 in. (0.08 mm to 0.38 mm) if not specified differently.
Damage resulting in nicks, dents and scratches up to 0.001 in. (0.025 mm) is allowed without blending.
Blend the hub surface damage such as dents, nicks, scratches, wear, fretting, galling distortion and corrosion pits.
A maximum of ten teeth can be blended when the blended area on one repaired tooth is 0.500 in. (12.7 mm) or less in length.
A maximum of five teeth can be blended when the blended area on one repaired tooth is more than 0.500 in. (12.7 mm) in length.
NOTE
For PNs 2A5001 and 2A2801, make sure fit 1517 at location 10 is maintained. The Stage 1 HPT Hubs that incorporated SB 72-0451 have metering plugs. Post SB 72-0511 Stage 1 HPT Hubs do not have metering plugs.
The maximum blend depth is 0.005 in. (0.13 mm).
Blend the area at location 11 to remove the surface damage.
The maximum blended area is one third of the circumference of the hole.
The blend must be smooth and continuous into the original contour in all directions.
If the damage or blend goes through the edge of the hole blend the hole radius by the procedures given in the SPM TASK 70-35-19-350-501.
Break the edges of the hole to between 0.010 in. and 0.030 in. (0.25 mm and 0.76 mm) radius (flats not included) when no part of the edge has a radius of the curvature that is less than 0.010 in. (0.25 mm) radius.
The maximum blend depth is 0.010 in. (0.25 mm).
Blend all the areas at location 10 to remove the surface damage.
SUBTASK 72-45-11-350-051-001 Blend the Hub (Rotary Method)
Blend by SPM TASK 70-35-03-300-501.
The finish marks must follow the lay of the original tool marks.
The minimum blend radius to depth ratio is 30 to 1.
Break all blended area edges 0.003 in. to 0.015 in. (0.08 mm to 0.38 mm) if not specified differently.
Damage resulting in nicks, dents and scratches, up to 0.001 in. (0.025 mm) is allowed without blending.
Refer to Figure requirements.
Blend the hub surface damage such as dents, nicks, scratches, wear, fretting, galling distortion and corrosion pits.
A maximum of ten teeth can be blended when the blended area on one repaired tooth is 0.500 in. (12.7 mm) or less in length.
A maximum of five teeth can be blended when the blended area on one repaired tooth is more than 0.500 in. (12.7 mm) in length.
NOTE
For PNs 2A5001 and 2A2801, make sure fit 1517 at location 10 is maintained. The Stage 1 HPT Hubs that incorporated SB 72-0451 have metering plugs. Post SB 72-0511 Stage 1 HPT Hubs do not have metering plugs.
The maximum blend depth is 0.005 in. (0.13 mm).
Blend the area at location 11 to remove the surface damage.
The maximum blended area is one third of the circumference of the hole.
The blend must be smooth and continuous into the original contour in all directions.
If the damage or blend goes through the edge of the hole blend the hole radius by the procedures given in SPM TASK 70-35-19-350-501.
Break the edges of the hole to between 0.010 in. and 0.030 in. (0.25 mm and 0.76 mm) radius (flats not included) when no part of the edge has a radius of the curvature that is less than 0.010 in. (0.25 mm) radius.
The maximum blend depth is 0.010 in. (0.25 mm).
Blend all the areas at location 10 to remove the surface damage.
SUBTASK 72-45-11-350-051-002 Blend the Hub (Manual Method)
Refer to Figure.
Do the procedure given in the TASK 72-45-11-200-000 and applicable part number.
No cracks permitted.
Fluorescent penetrant inspect all of the repaired surfaces for cracks.
SUBTASK 72-45-11-230-054 Fluorescent Penetrant the Repair Areas
Do the procedure given in SPM TASK 70-38-13-380-501.
Shot peen all of the repaired surfaces at locations 1 and 2. The minimum intensity 6A or equivalent is not required. You must shot peen the complete repaired area.
SUBTASK 72-45-11-380-057 Shotpeen the Hub Repaired Areas (Local Application)
Make a permanent mark by the procedure given in the SPM TASK 70-09-00-400-501.
Use the vibration peen method.
Mark VRS3184 adjacent to the part number.
SUBTASK 72-45-11-350-068 Identify the Repair
Figure: Repair Details and Dimensions
Sheet 1

Figure: Repair Details and Dimensions
Sheet 2

