| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
AIRCRAFT, T-39 ENGINE, AIRCRAFT,F100-PW-200(F-16A/BC/D) |
| ABAF |
EXPANSION DEVICE |
PLAIN STEM-TYPE T |
| AASB |
FASTENER LENGTH |
0.409 INCHES MINIMUM AND 0.439 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.251 INCHES MINIMUM AND 0.312 INCHES MAXIMUM |
| AASU |
HEAD HEIGHT |
0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM |
| AAZG |
HEAD MAJOR DIAMETER |
0.238 INCHES MINIMUM AND 0.262 INCHES MAXIMUM |
| AASK |
HEAD STYLE |
UNIVERSAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-200/13 FED SPEC SINGLE MATERIAL RESPONSE MANDREL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE BODY |
| MATT |
MATERIAL |
ALUMINUM ALLOY 5052 BODY |
| MATT |
MATERIAL |
ALUMINUM ALLOY 7178 MANDREL |
| AAZE |
SHANK DIAMETER |
0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM |
| AAZF |
SHANK STYLE |
SELF-PLUGGING |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OVERALL OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE OVERALL |
| SFTT |
SURFACE TREATMENT |
ANODIZE OVERALL OR CHROMATE OVERALL |
