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 72-32-51-300-029 Rotor Center Shaft - Blend The Thread, Repair-029 (VRS1369)
General
This repair scheme gives the procedure for blending the thread of the shafts.
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Standard Workshop Equipment | LOCAL | Standard Workshop Equipment | ||
| Portablegrinding equipment | LOCAL | Portable grinding equipment |
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 05-064 WATERPROOF SILICON CARBIDE | K6835 | CoMat 05-064 | ||
| CoMat 05-075 WATERPROOF SILICON CARBIDE | IE241 | CoMat 05-075 | ||
| CoMat 05-076 WATERPROOF SILICON CARBIDE | K3895 | CoMat 05-076 |
Spares
NONESafety Requirements
NONEProcedure
Use portable grinding equipment and CoMat 05-021 WATERPROOF SILICON CARBIDE and CoMat 05-020 WATERPROOF SILICON CARBIDE. Dress until all damage is removed.
Dress to remove damage.
Maximum blend depth is 0.02 in. (0.50 mm) and total blend length is 3.54 in. (90.0 mm).
Refer to SPM TASK 70-35-03-300-501.
Polish the repaired area to give a surface finish the same as the adjacent material.
Blend dressed area and polish the blended areas.
SUBTASK 72-32-51-380-001 Dress to Remove the Damage

CAUTION
TITANIUM COMPONENT - YOU MUST USE SILICON CARBIDE TYPE ABRASIVE WHEELS, STONES AND PAPERS TO DRESS, BLEND AND POLISH THIS COMPONENT. IF MECHANICAL CUTTERS ARE USED, ONLY LIGHT CUTS MUST BE MADE TO AVOID OVERHEATING THE MATERIAL.
CAUTION
TITANIUM COMPONENT - AVOID BUILD UP OF HEAT BY APPLYING ONLY GENTLE PRESSURE AND KEEPING THE TOOL SPEED AS LOW AS POSSIBLE. USE TECHNIQUES WHICH ALLOW FOR PROGRESSIVE WEAR OF THE DRESSING MEDIA TO PRESENT A CONTINUALLY FRESH CUTTING SURFACE TO THE WORK PIECE. DO NOT DWELL ON ONE AREA OF THE COMPONENT. DRESS, WHERE POSSIBLE, IN A CIRCULAR MOTION; TAKING LIGHT CUTS TO AVOID OVERHEATING.
CAUTION
TITANIUM COMPONENT - YOU MUST MAKE SURE THAT WHEN YOU REMOVE MATERIAL, BLEND AND POLISH, TO MAKE SMOOTH, THAT NO SPARKS ARE PRODUCED AND THE ADJACENT AREA IS MASKED OFF.
CAUTION
TITANIUM COMPONENT - IF THE MATERIAL SHOWS A CHANGE IN COLOR DURING DRESSING, TO DARKER THAN A LIGHT STRAW COLOR, THE COMPONENT IS TO BE REJECTED.
CAUTION
POWER BLENDING TOOLS MAY BE USED IF DAMAGED TITANIUM PART IS PERIODICALLY CHECKED FOR HEAT BUILD - UP BY TOUCHING OCCASIONALLY WITH UNGLOVED HAND. IF TITANIUM PART BECOMES TOO HOT TO TOUCH, ALLOW MATERIAL TO COOL BEFORE CONTINUING REPAIR.
CAUTION
DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARDS EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.NOTE
Dull tools and worn or loaded abrasive equipment generate heat rapidly and should be checked frequently and replaced when necessary.NOTE
Remove the minimum quantity of material necessary to remove the damage. All blends must be smooth and continuous.NOTE
The surface finish of all the repaired surfaces must have the same or better quality to that of the adjacent, not damaged, areas.NOTE
Keep the material removal to the minimum necessary to remove damage.Refer to SPM TASK 70-11-26-300-503.
Use cleaning equipment.
Clean the repair area.
SUBTASK 72-32-51-110-001 Clean the Shaft
Refer to SPM TASK 70-11-08-300-503, SUBTASK 70-11-08-300-002.
Use chemical etching equipment.
Swab etch the repaired area
SUBTASK 72-32-51-110-002 Do a Swab Etch
Do the penetrant crack test for the repaired area
Refer to SPM TASK 70-23-05-230-501.
Make sure that there are no cracks in the repaired area.
Do the crack test
SUBTASK 72-32-51-230-001 Crack Test
Visually examine repaired area for nicks, dents and/or scores.
Use 10X magnifying glass.
Refer to SPM TASK 72-32-51-200-000.
Do a visual inspection
SUBTASK 72-32-51-220-001 Examine the Shafts
Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.
Use vibro-engraving equipment
Refer to Figure.
Make a mark VRS1369 TASK 72-32-51-300-029 on the castellation surface
SUBTASK 72-32-51-350-001 Identify the Repair
Figure: Rotor center shaft
Rotor center shaft

Figure: Blend Repair - Damaged Thread of the Rotor Center Shaft
Blend Repair - Damaged Thread of the Rotor Center Shaft

