MRC |
Requirement Statement |
Characteristics |
AGAV |
END ITEM IDENTIFICATION |
W/S: MARS CLASS T-AFS-1 USNS HENRY J. KAISER CLASS TAO ENGINE, T700-GE-700 (UH-60 & EH-60A) SUPPORT EQUIPMENT, B-1 AIRCRAFT ENGINE, T700-GE-701 (AH-64) STREAM (STD, TENSIONED REPLENISHMENT AT SEA METHOD) SUPPLY CLASS AOE WASP CLASS LHD HELICOPTER, |
AASB |
FASTENER LENGTH |
0.281 INCHES MINIMUM AND 0.343 INCHES MAXIMUM |
CBBL |
FEATURES PROVIDED |
CASEHARDENED |
AASL |
HEAD DIAMETER |
0.256 INCHES MINIMUM AND 0.270 INCHES MAXIMUM |
AASU |
HEAD HEIGHT |
0.087 INCHES MINIMUM AND 0.097 INCHES MAXIMUM |
AASK |
HEAD STYLE |
PAN |
MATT |
MATERIAL |
STEEL COMP 410 OVERALL |
ZZZT |
NONDEFINITIVE SPEC/STD DATA |
AB TYPE |
CTYF |
NONMACHINE NOMINAL THREAD DIAMETER |
0.138 INCHES |
CRGF |
NONMACHINE THREAD STYLE |
GIMLET POINT (TYPE A, AB OR BA) |
ABQZ |
INTERNAL DRIVE STYLE |
CROSS RECESS TYPE 1 |
MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
66 FED STD SINGLE MATERIAL RESPONSE OVERALL |
STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
SFTT |
SURFACE TREATMENT |
PASSIVATE OVERALL |