DMC:V2500-A0-72-44-3000-00A-530A-BIssue No:001.00Issue Date:2013-11-01
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 72-44-30-040-001 Inner Combustion Chamber Assembly - Disassemble The Inner Combustion Chamber Assembly, Assembly-001
General
Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.
NOTE
To identify the consumable materials refer to the PCI.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-081 PENCIL - METAL MARKING(HARD) | 86874 | CoMat 02-081 |
Spares
NONESafety Requirements
NONEProcedure
Refer to: Figure
SUBTASK 72-44-30-040-051 Remove the Combustion Chamber Liner Segments from the Outer Diameter of the Inner Combustion Chamber Liner
NOTE
Mark the segments with CoMat 02-081 PENCIL - METAL MARKING(HARD) as they are removed so that they can be reassembled in their original positions.If more than 80 lbfin (9.04 Nm) was applied to a stud, fluorescent penetrant inspect the stud threads. Refer to the SPM TASK 70-23-02-230-501. Replace segments if there are cracks in the stud threads. Refer to Repair VRS3173 TASK 72-44-30-300-001.
Figure: Disassemble the inner combustion chamber assembly
Disassemble the inner combustion chamber assembly

