DMC:V2500-A0-72-00-6001-00A-649A-CIssue No:002.00Issue Date:2016-08-01
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 72-00-60-300-001 External Gearbox Module - Brackets - Blend Repair, Repair-001 (VRS1125)
Material of component
DESCRIPTION | RR SYMBOL | MATERIAL |
|---|---|---|
Bracket | Titanium alloy | |
Bushing | Corrosion resistant steel |
General
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Portablegrinding equipment | LOCAL | Portable grinding equipment |
Consumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure

CAUTION
TITANIUM COMPONENTS.SILICON CARBIDE TYPE WHEELS, STONES AND ABRASIVE PAPERS ARE TO BE USED FOR THIS REPAIR.ALUMINUM OXIDE TYPES MUST NOT BE USED.THE MATERIAL WILL OXIDIZE AND CRACK IF MECHANICAL CUTTERS ARE USED HEAVILY. THIS HAS OCCURRED IF THE COMPONENT SHOWS DARK STRAW TO BLUE DISCOLORATION. IF AT ANY TIME THIS COLORATION OCCURS THE BRACKET MUST BE REJECTED.Dress to remove damage.
Refer to the SPM TASK 70-35-03-300-501.
Maximum blend limit is 0.005 in. (0.12 mm) in depth.
Blend dressed area and polish out scores.
SUBTASK 72-00-60-350-051 Dress to Remove Damage
Make sure there are no cracks in the repaired area.
Refer to the SPM TASK 70-23-01-230-501.
Fluorescent penetrant examine the repaired area.
SUBTASK 72-00-60-230-054 Examine the Bracket for Cracks
