FRAME FRONT
P/N 6030T79G08
NSN 2840 01 004 8115

MFG GENERAL ELECTRIC
CONDITION: SERVICEABLE
SUPPLIER CAGE 03EF7

DEFINITION:  A frame used for and part of the front section of an aircraft gas

             turbine engine. May include struts with or without variable guide

             vanes.

             



CHARACTERISTIC                          VALUE

OVERALL LENGTH                          15.806 INCHES MINIMUM AND 15.814 INCHES MAXIMUM   

END ITEM IDENTIFICATION                 ENGINE,ACFT,MODEL NO. TF34-GE-100                 

CRITICALITY CODE                        MATT AND FEAT AND ABHP AND AGAV                   

JUSTIFICATION                                                                             

SPECIAL FEATURES                        MATL AMS 2473                                     

MATERIAL                                NICKEL ALLOY                                      

DESIGN CONTROL REFERENCE                6030T79G08                                        

THE MANUFACTURERS DATA                  99207                                             

MANUFACTURERS CODE

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