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 72-41-11-300-003 HPC Stage 3 - 8 Drum Disk - Blend Repair, Repair-003 (VRS6047)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-200 | 6A3508 |
01-200 | 6A3648 |
01-200 | 6A3934 |
01-200 | 6A3936 |
01-200 | 6A4189 |
01-200 | 6A4900 |
01-200 | 6A5467 |
01-200 | 6A5592 |
01-200 | 6A5594 |
01-200 | 6A5659 |
01-200 | 6A6473 |
01-200 | 6A7379 |
01-200 | 6A7380 |
01-200 | 6A7382 |
01-200 | 6A7383 |
01-200 | 6A7384 |
01-200 | 6A7385 |
01-200 | 6A7401 |
01-200 | 6A7705 |
01-200 | 6A8236 |
01-200 | 6A8316 |
01-200 | 6A8318 |
01-200 | 6A8350 |
01-200 | 6B1379 |
01-200 | 6B1380 |
01-200 | 6B1381 |
01-200 | 6B1382 |
01-200 | 6B1383 |
01-200 | 6B1384 |
01-200 | 6B1385 |
01-200 | 6B1386 |
01-200 | 6B1387 |
01-200 | 6B1391 |
01-200 | 6B1392 |
01-200 | 6B1393 |
01-200 | 6B1401 |
01-200 | 6B1402 |
01-200 | 6B1403 |
01-200 | 6B1404 |
01-200 | 6B1405 |
01-200 | 6B1406 |
General
This repair must only be done when the instruction to do so is given in inspection procedures (identified by the applicable part number) located in section 72-41-11.
The practices and processes referred to in the procedure by the TASK/SUBTASK numbers are in the Standard Practices Manual (SPM).
If the damage is nicks, dents or scores the maximum depth of damage before material removal is 0.002 in. (0.051 mm) and you must remove damage to 2X depth to a maximum depth of 0.005 in. (0.127 mm).
If the damage is frettage the maximum depth of damage before material removal is 0.005 in. (0.127 mm) and you must remove damage to depth to a maximum depth of 0.005 in. (0.127 mm).
Price and availability.
Refer to International Aero Engines (IAE).
Related repairs.
None.
NOTE
Equipment and materials necessary to do this repair are in the SPM TASKS given below:
NOTE
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Standard workshop equipment | LOCAL | Standard workshop equipment | ||
| Chemical cleaning equipment | LOCAL | Chemical cleaning equipment | ||
| Workshop inspection equipment | LOCAL | Workshop inspection equipment | ||
| Penetrant Crack Test Equipment | LOCAL | Penetrant crack test equipment | ||
| Binoculars 10X | LOCAL | Binoculars 10X | ||
| Vibrating marking pencil | LOCAL | Vibrating marking pencil |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 | ||
| CoMat 05-021 WATERPROOF SILICON CARBIDE | 44197 | CoMat 05-021 | ||
| CoMat 05-106 ABRASIVE STONE | K6835 | CoMat 05-106 | ||
| CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY) | LOCAL | CoMat 06-022 |
Spares
NONESafety Requirements
NONEProcedure
Refer to SPM TASK 70-23-05-230-501.
Cracks are not permitted.
Do a local penetrant crack test on the area to be repaired.
SUBTASK 72-41-11-230-055 Do a Crack Test

CAUTION
TITANIUM COMPONENT - YOU MUST USE SILICON CARBIDE TYPE ABRASIVE WHEELS, STONES AND PAPERS TO DRESS, BLEND AND POLISH THIS COMPONENT.
CAUTION
TITANIUM COMPONENT - DO NOT USE FORCE WITH MECHANICAL CUTTERS OR THE MATERIAL WILL BECOME TOO HOT.
CAUTION
TITANIUM COMPONENT - MAXIMUM SPEED FOR MECHANICAL TOOLS MUST NOT EXCEED 1000 REVOLUTIONS PER MINUTE.
CAUTION
TITANIUM COMPONENT - YOU MUST MAKE SURE THAT WHEN YOU REMOVE MATERIAL, BLEND AND POLISH, TO MAKE SMOOTH, THAT NO SPARKS ARE PRODUCED.
CAUTION
TITANIUM COMPONENT - IF THE MATERIAL SHOWS A CHANGE IN COLOR, TO DARKER THAN A LIGHT STRAW COLOR, THE COMPONENT IS TO BE REJECTED.Refer to Figure.
Refer to SPM TASK 70-35-03-300-501.
The maximum depth to remove the damage must not be more than 0.005 in. (0.13 mm).
The repaired area(s) diameter is to be 50 times the depth.
Remove small area(s) of damage as necessary.
Refer to SPM TASK 70-35-03-300-501.
Remove sharp corners.
Blend the area of repair.
Refer to SPM TASK 70-35-03-300-501.
Polish the repaired area to give a surface finish the same as the adjacent material.
Polish the area of repair.
SUBTASK 72-41-11-325-054 Remove the Damage
Refer to SPM TASK 70-11-08-300-503, SUBTASK 70-11-08-300-001.
Chemically clean.
Refer to SPM TASK 70-11-08-300-503, SUBTASK 70-11-08-300-002.
Swab etch the repair area.
SUBTASK 72-41-11-110-100 Do a Swab Etch
Use Binoculars 10X.
Indications of surface defects are not permitted.
Make sure that there is no raised metal remaining.
Binocular examine the repaired area.
SUBTASK 72-41-11-220-247 Binocular Examine
Refer to SPM TASK 70-23-05-230-501.
Cracks are not permitted.
Do a local penetrant crack test of the repaired area.
SUBTASK 72-41-11-230-102 Do a Crack Test
Refer to SPM TASK 70-11-26-300-503.
Chemically clean the repaired area to remove fluorescent penetrant.
SUBTASK 72-41-11-110-101 Chemically Clean
Refer to Figure.
SUBTASK 72-41-11-220-071 Examine the Repair
Refer to Figure.
Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.
Vibro-engrave VRS6047 adjacent to the part number.
SUBTASK 72-41-11-350-054 Identify the Repair
Figure: Repair details and dimensions
Repair details and dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

