* * * FOR ALL
TASK 72-53-40-300-802
1 . Corrosion Pitting Shotpeen Repair.
A.Procedure RD 150-1538-P3 or higher gives instructions to repair the high pressure turbine rotor (HPTR) stage 1 disk for corrosion pitting by using a standard practice shotpeen procedure.
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)
 
2352M61G02  
2352M61G03  
2383M83G03  
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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:
 
E-mail GE Technology Licensing: License.Requests@ge.com
 
OR
 
GE Aviation
 
1 Neumann Way, Mail Drop: RM100
 
Cincinnati, Ohio 45215-6301, U.S.A.
 
Attn: Manager, Technology Licensing
C.The Repair Document and the Repair Source Substantiation requirements may be obtained from:
 
E-mail Repair Administration: GEAviation.PCN_RSS@ge.com
 
OR
 
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 GE Repair Sources Directory for a list of approved repair sources.