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 72-44-20-300-011 HPT Stage 1 Vane - Blend Repair The Airfoil, Repair-011 (VRS3154)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-240 | 2A0561 |
01-240 | 2A2761 |
01-240 | 2A4201 |
01-240 | 2A5591 |
01-240 | 2A4271 |
01-250 | 2A0091CL21 |
01-250 | 2A2591CL21 |
01-251 | 2A0091CL22 |
01-251 | 2A2591CL22 |
01-252 | 2A0091CL23 |
01-252 | 2A2591CL23 |
01-253 | 2A0091CL24 |
01-253 | 2A2591CL24 |
01-254 | 2A0091CL25 |
01-254 | 2A2591CL25 |
01-255 | 2A0091CL26 |
01-255 | 2A2591CL26 |
01-256 | 2A0091CL27 |
01-256 | 2A2591CL27 |
01-257 | 2A0091CL28 |
01-257 | 2A2591CL28 |
01-258 | 2A0091CL29 |
01-258 | 2A2591CL29 |
01-259 | 2A0091CL30 |
01-259 | 2A2591CL30 |
01-260 | 2A0091CL31 |
01-260 | 2A2591CL31 |
01-261 | 2A0091CL32 |
01-261 | 2A2591CL32 |
01-262 | 2A0091CL33 |
01-262 | 2A2591CL33 |
01-263 | 2A0091CL34 |
01-263 | 2A2591CL34 |
01-264 | 2A0091CL35 |
01-264 | 2A2591CL35 |
01-265 | 2A0091CL36 |
01-265 | 2A2591CL36 |
01-266 | 2A0091CL37 |
01-266 | 2A2591CL37 |
01-267 | 2A0091CL38 |
01-267 | 2A2591CL38 |
01-268 | 2A0091CL39 |
01-268 | 2A2591CL39 |
01-269 | 2A0091CL40 |
01-269 | 2A2591CL40 |
01-270 | 2A0091CL41 |
01-270 | 2A2591CL41 |
01-271 | 2A0091CL42 |
01-271 | 2A2591CL42 |
01-272 | 2A0091CL43 |
01-272 | 2A2591CL43 |
01-273 | 2A0091CL44 |
01-273 | 2A2591CL44 |
01-274 | 2A0091CL45 |
01-274 | 2A2591CL45 |
01-275 | 2A0091CL46 |
01-275 | 2A2591CL46 |
01-276 | 2A0091CL47 |
01-276 | 2A2591CL47 |
01-277 | 2A0091CL48 |
01-277 | 2A2591CL48 |
01-278 | 2A0091CL48-5 |
01-279 | 2A0091CL49 |
01-279 | 2A2591CL49 |
01-280 | 2A0091CL49-5 |
01-284 | 2A2591CL50 |
01-286 | 2A2591CL51 |
General
This repair must only be done when the instruction to do so is given in 72-44-20 Inspection.
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
You can blend over any repaired areas on the airfoil if you do not exceed the limits given in the figure.
Price and availability - none
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| File | LOCAL | File | (fine) | |
| Workshop inspection equipment | LOCAL | Workshop inspection equipment |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-106 ABRASIVE STONE | K6835 | CoMat 05-106 | ||
| CoMat 05-110 EMERY POLISHING PAPER | 0AM53 | CoMat 05-110 | ||
| CoMat 05-120 POLISHING CLOTH | 06565 | CoMat 05-120 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
All blends must be smooth, round bottomed and made in the shape of the initial contour.
The maximum blend length to depth is 6 to 1.
The blends must be apart by a minimum of 0.300 in. (7.62 mm).
Make sure all the cooling air holes are clean and open.
Use Comat CoMat 05-110 EMERY POLISHING PAPER and CoMat 05-120 POLISHING CLOTH.
Blend the dents and nicks on the airfoils leading edge.
SUBTASK 72-44-20-350-051 Blend the Dents and Nicks on the Airfoils Leading Edge
Refer to Figure.
All blends must be smooth and round bottomed and made in the shape of the initial contour.
The maximum blend length to depth is 6 to 1.
The blends must be apart by a minimum of 0.300 in. (7.62 mm).
Make sure all the cooling air holes are clean and open.
For larger dents and nicks use a fine file or CoMat 05-106 ABRASIVE STONE.
Finish the blend with the fine abrasive stone.
Blend the dents and nicks on the airfoils and the trailing edge.
SUBTASK 72-44-20-350-052 Blend the Dents and Nicks on the Airfoils and the Trailing Edges
Refer to Figure.
The total maximum blended area is 0.500 sqin. (3.226 sqcm).
Examine the airfoils.
SUBTASK 72-44-20-220-061 Examine the Airfoils
Refer to Repair, VRS3164 TASK 72-44-20-300-015 (REPAIR-015), or Repair VRS3584 TASK 72-44-20-300-028 (REPAIR-028), or Repair VRS3613 TASK 72-44-20-300-033 (REPAIR-033).
Coat the airfoil.
SUBTASK 72-44-20-340-051 Coat the Airfoils
Figure: Repair Details and Dimensions
Repair Details and Dimensions

