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MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | CONTROL ASSEMBLY,FUEL AFTER BURNER,ENGINE,J79,TURBOJET AIRCRAFT |
TEXT | 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 |
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