| MRC |
Requirement Statement |
Characteristics |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-C-5541 MIL SPEC SINGLE TREATMENT RESPONSE BODY QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE STEM |
| AASU |
HEAD HEIGHT |
0.080 INCHES MINIMUM AND 0.090 INCHES MAXIMUM |
| MATT |
MATERIAL |
ALUMINUM ALLOY 5056 BODY STEEL COMP 8740 STEM |
| ANEE |
GRIP LENGTH |
0.313 INCHES MINIMUM AND 0.375 INCHES MAXIMUM |
| FEAT |
SPECIAL FEATURES |
"NS" LETTERS AFTER THE MATERIAL CODE "B" INDICATE NO PREFERENCE TO LOCK TYPE (MAY BE VISIBLE OR INTERNAL). RIVETS WITH NO LETTER CODE (INDICATING VISIBLE LOCK TYPE) AND RIVETS WITH THE LETTER "H" AFTER THE MATERIAL CODE (INDICATING INTERNAL LOCK TYPE) ARE BOTH ACCEPTABLE FOR THIS ITEM OF SUPPLY. |
| ABAF |
EXPANSION DEVICE |
SERRATED STEM-TYPE W |
| AASK |
HEAD STYLE |
UNIVERSAL |
| AASB |
FASTENER LENGTH |
0.505 INCHES MINIMUM AND 0.525 INCHES MAXIMUM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE BODY AMS 6322 ASSN STD SINGLE MATERIAL RESPONSE STEM |
| AAZG |
HEAD MAJOR DIAMETER |
0.356 INCHES MINIMUM AND 0.394 INCHES MAXIMUM |
| AAZE |
SHANK DIAMETER |
0.202 INCHES MINIMUM AND 0.205 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING MECHANICALLY LOCKED STEM |
| AGAV |
III END ITEM IDENTIFICATION |
HELICOPTER, SUPER JOLLY H-53; HELICOPTER, IROQUOIS HH/UH-1; AIRCRAFT, THUNDERBOLT II, A-10; AIRCRAFT, EAGLE F-15; AIRCRAFT, F-111; AIRCRAFT, GALAXY C-5; AIRCRAFT, PHANTOM F-4; AIRCRAFT, HERCULES C-130; AIRCRAFT, AC-130H, MC-130H, EC-130E, HC-130); AIRCRAFT, DELTA DART F-106 |
| SFTT |
SURFACE TREATMENT |
CHROMATE BODY CADMIUM STEM |
