| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
9W/S:AIRCRAFT, T-38 AIRCRAFT, EAGLE F-15 DEEP SUBMERGENCE SYSTEMS PROGRAMS (DSSP) AIRCRAFT, PHANTOM F-4 AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130) F-22 RAPTOR AIR DOMINANCE FIGHTER AIRCRAFT, GALAXY C-5 AIRCRAFT, F-111 AIRCRAFT, TOMCAT F-14 |
| CRSQ |
COUNTERSINK ANGLE |
98.5 DEGREES MINIMUM AND 101.5 DEGREES MAXIMUM |
| ABAF |
EXPANSION DEVICE |
SERRATED STEM-TYPE W |
| AASB |
FASTENER LENGTH |
0.265 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.126 INCHES MINIMUM AND 0.187 INCHES MAXIMUM |
| AAZG |
HEAD MAJOR DIAMETER |
0.179 INCHES NOMINAL |
| AASK |
HEAD STYLE |
FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-N-281 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| MATT |
MATERIAL |
NICKEL ALLOY 400 OVERALL |
| AAZE |
SHANK DIAMETER |
0.092 INCHES MINIMUM AND 0.097 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
PULL THROUGH HOLLOW SHANK |
| CQSX |
SHEAR STRENGTH |
70 SINGLE POUNDS PER SQUARE INCH |
