* * * FOR ALL
TASK 72-51-01-300-814
1 . Laser Cladding Weld Repair Of The Outer Flange Cracks.
A.Procedure RD 172-420-P1 or higher gives instructions to repair the high pressure turbine stage 1 nozzle support (nozzle support) by laser cladding welding cracks on the outer flange.
B.The subsequent table gives a list of the part numbers that are applicable to this procedure. All part numbers are applicable to all paragraphs unless specified differently.
 
Part Number(s)
 
2407M46G02  
2407M46G04  
2407M46G06  
2407M46G08  
2 . Proprietary/Complex Process Statement.
A.This repair or portions of this repair require a Technical License Agreement and Repair Source Substantiation prior to use. It is necessary that the repair source be approved by the FAA, obtain a Technical License Agreement from GE Aviation, and receive Repair Source Substantiation before performing this repair.
B.Information concerning a Technical License Agreement is available from:
 
GE Aviation
 
1 Neumann Way, Mail Drop: RM100
 
Cincinnati, Ohio 45215-6301, U.S.A.
 
Attn: Manager, Technology Licensing
C.After the repair source has a Technical License Agreement, this repair is available from GE Aviation. Revisions to the Repair Document will be provided to approved repair sources. The Repair Document and the Repair Source Substantiation requirements may be obtained from:
 
GE Aviation
 
1 Neumann Way, Mail Drop: S171
 
Cincinnati, Ohio 45215-6301, U.S.A.
 
Attn: Repair Substantiation
3 . Approved Repair Sources.
A.Refer to the GEnx Repair Sources Directory for a list of approved repair sources.