| 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 |
| AAZE |
SHANK DIAMETER |
0.173 INCHES MINIMUM AND 0.176 INCHES MAXIMUM |
| AASK |
HEAD STYLE |
FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
| AASB |
FASTENER LENGTH |
0.236 INCHES MINIMUM AND 0.256 INCHES MAXIMUM |
| MATT |
MATERIAL |
ALUMINUM ALLOY 5056 BODY STEEL COMP 8740 STEM |
| 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 |
| 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 |
0.270 INCHES MINIMUM |
| ANEE |
GRIP LENGTH |
0.063 INCHES MINIMUM AND 0.125 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING MECHANICALLY LOCKED STEM |
| CRSQ |
COUNTERSINK ANGLE |
100.0 DEGREES NOMINAL |
| AGAV |
III END ITEM IDENTIFICATION |
AIRCRAFT, AC-130H, MC-130H, EC-130E, HC-130); HELICOPTER, IROQUOIS UH-1; U-2 SUPPORT EQUIPMENT; AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT, TF39-FE-1 (C-5A); AIRCRAFT, PHANTOM F-4; AIRCRAFT, STRATOLIFTER C-135; T1A AIRCRAFT; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P) |
| SFTT |
SURFACE TREATMENT |
CHROMATE BODY CADMIUM STEM |
