| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
W/S: AIRCRAFT, PROWLER EA-6B AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130) ENGINE, T700-GE-701C (AH-64) ENGINE, T700-GE-701 (UH-60 & EH-60A) TRAINER, B-1B AIRCRAFT AIRCRAFT, C-2A (REPROCURED) TACTICAL AIR OPNS MODULE (AN/TYQ-23) ENGINE, AIRCRAFT, F |
| ABAF |
EXPANSION DEVICE |
PLAIN STEM-TYPE T |
| AASB |
FASTENER LENGTH |
0.373 INCHES MINIMUM AND 0.403 INCHES MAXIMUM |
| ANEE |
GRIP LENGTH |
0.188 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| AASU |
HEAD HEIGHT |
0.026 INCHES MINIMUM AND 0.046 INCHES MAXIMUM |
| AAZG |
HEAD MAJOR DIAMETER |
0.224 INCHES MINIMUM AND 0.248 INCHES MAXIMUM |
| AASK |
HEAD STYLE |
UNIVERSAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE BODY |
| MATT |
MATERIAL |
ALUMINUM ALLOY 5056 BODY |
| MATT |
MATERIAL |
STEEL 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 BODY AND MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE BODY |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-Z-325 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE MANDREL |
| SFTT |
SURFACE TREATMENT |
ZINC MANDREL AND CHROMATE MANDREL |
