| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
9HELICOPTER, COBRA/TOW, AH SERIES AIRCRAFT, AC-130H, MC-130H, EC-130 AIRCRAFT, PHANTOM F-4 AIRCRAFT, F-111 AIRCRAFT, B-1B AIRCRAFT, EAGLE F-15 AIRCRAFT, STRATOFORTRESS B-52 HELICOPTER, UH-60A/UH-60D AIRCRAFT, GALAXY C-5 AIRCTAFT, THUNDERBOLT II, A-10 |
| CRSQ |
COUNTERSINK ANGLE |
100.0 DEGREES NOMINAL |
| ABAF |
EXPANSION DEVICE |
SERRATED STEM-TYPE W |
| AASB |
FASTENER LENGTH |
0.380 INCHES MINIMUM AND 0.400 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.188 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| AAZG |
HEAD MAJOR DIAMETER |
0.357 INCHES MAXIMUM |
| 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 ALL MATERIAL RESPONSES BODY |
| MATT |
MATERIAL |
NICKEL ALLOY 400 BODY OR NICKEL ALLOY R-405 BODY |
| MATT |
MATERIAL |
STEEL COMP 632 STEM |
| ABAJ |
LUBRICATION |
DRY FILM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5657 ASSN STD SINGLE MATERIAL RESPONSE STEM |
| AAZE |
SHANK DIAMETER |
0.201 INCHES MINIMUM AND 0.205 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING MECHANICALLY LOCKED STEM |
| FEAT |
SPECIAL FEATURES |
LUBRICATION ON STEM ONLY |
