| MRC |
Requirement Statement |
Characteristics |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| AGAV |
END ITEM IDENTIFICATION |
WSD: AIRCRAFT, GALAXY C-5 AIRCRAFT, EAGLE F-15 HELICOPTER, IROQUOIS HH/UH-1 AIRCRAFT, THUNDERBOLT II, A-10 AIRCRAFT, FREEDOM FIGHTER F-5 AIRCRAFT, HERCULES C-130 AIRCRAFT, STARLIFTER C-141 AIRCRAFT, F-111 AIRCRAFT, AC-130H, MC-130H, EC-130E, HC-13 |
| ABAF |
EXPANSION DEVICE |
SERRATED STEM-TYPE W |
| AASB |
FASTENER LENGTH |
0.299 INCHES MINIMUM AND 0.319 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.126 INCHES MINIMUM AND 0.187 INCHES MAXIMUM |
| AASU |
HEAD HEIGHT |
0.067 INCHES MINIMUM AND 0.077 INCHES MAXIMUM |
| AAZG |
HEAD MAJOR DIAMETER |
0.302 INCHES MINIMUM AND 0.322 INCHES MAXIMUM |
| AASK |
HEAD STYLE |
UNIVERSAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-N-281 FED SPEC SINGLE MATERIAL RESPONSE SLEEVE |
| MATT |
MATERIAL |
NICKEL ALLOY 400 SLEEVE OR NICKEL ALLOY R-405 SLEEVE |
| MATT |
MATERIAL |
STEEL STEM |
| ABAJ |
LUBRICATION |
DRY FILM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5657 ASSN STD SINGLE MATERIAL RESPONSE STEM |
| AAZE |
SHANK DIAMETER |
0.172 INCHES MINIMUM AND 0.176 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING MECHANICALLY LOCKED STEM |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |