| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
W/S: HELICOPTER, IROQUOIS UH-1 TARAWA CLASS LHA HELICOPTER, CHINOOK, CH-47 SUPPORT EQUIPMENT, B-1 AIRCRAFT MISSILE, AIR-TO-AIR, PHOENIX (AIM-54) ENGINE, AIRCRAFT F110-GE-400 HELICOPTER, ELECTRONIC COUNTERMEASURES, EH-60A HELICOPTER OBSERVATION (AHI |
| AASB |
FASTENER LENGTH |
0.219 INCHES MINIMUM AND 0.281 INCHES MAXIMUM |
| AASL |
HEAD DIAMETER |
0.155 INCHES MINIMUM AND 0.167 INCHES MAXIMUM |
| AASU |
HEAD HEIGHT |
0.053 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
| AASK |
HEAD STYLE |
PAN |
| MATT |
MATERIAL |
STEEL COMP 410 OVERALL |
| ZZZT |
NONDEFINITIVE SPEC/STD DATA |
AB TYPE |
| CTYF |
NONMACHINE NOMINAL THREAD DIAMETER |
0.086 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 |
