| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
WS: ENGINE, AIRCRAFT, J-57 ALL MODELS (C-135, EC-135, B-52 AIRCRAFT, PHANTOM F-4 ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) AIRCRAFT, STRATOLIFTER C-135 AIRCRAFT, STRATOFORTRESS B-52 ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P) AIRCRAFT, |
| ABAF |
EXPANSION DEVICE |
SERRATED STEM-TYPE W |
| AASB |
FASTENER LENGTH |
0.177 INCHES MINIMUM AND 0.197 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.031 INCHES MINIMUM AND 0.062 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-A-430 FED SPEC SINGLE MATERIAL RESPONSE SLEEVE |
| MATT |
MATERIAL |
ALUMINUM ALLOY 5056 SLEEVE |
| MATT |
MATERIAL |
STEEL COMP 8740 STEM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 6322 ASSN STD SINGLE MATERIAL RESPONSE STEM |
| AAZE |
SHANK DIAMETER |
0.156 INCHES MINIMUM AND 0.160 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING MECHANICALLY LOCKED 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 |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-C-5541 MIL SPEC SINGLE TREATMENT RESPONSE SLEEVE |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-416,TY 2,CL 2 FED SPEC SINGLE TREATMENT RESPONSE STEM |
| SFTT |
SURFACE TREATMENT |
CADMIUM STEM AND CHROMATE STEM |
| SFTT |
SURFACE TREATMENT |
CHROMATE SLEEVE |
