CONTROL ASSEMBLY,FUEL AFTER BURNER,ENGINE,J79,TURBOJET AIRCRAFT
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GENERAL CHARACTERISTICS ITEM DESCRIPTION
BRAZE PER HAMILTON STANDARD SPEC NO 198,HEAT TREATMENT PER MIL-H-6875 AND HAMILTON STANDARD SPEC NO 461,0.397 IN. MIN,0.402 IN. MAX O/A LG,0.094 IN. MIN,0.096 IN. MAX DIA 2 HOLES
Relevant Components for NSN - 2915-00-654-2524, 2915006542524
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