| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
W/S: AIRCRAFT, THUNDERBOLT II, A-10 AIRCRAFT, (AC-13H, MC-130H, EC-130E, HC-130) AIRCRAFT, ORION P-3 AIRCRAFT, VIKING S-3B HELICOPTER, LAMPS MARK III, SH-60B HELICOPTER, KIOWA OH-58 A&C HELICOPTER, SEAHAWK H-60 AIRCRAFT, GALAXY C-5 AIRCRAFT, HERCU |
| CQFM |
HARDNESS RATING |
42.0 ROCKWELL C MINIMUM AND 47.0 ROCKWELL C MAXIMUM |
| AAUB |
HOLE DIAMETER |
0.166 INCHES MINIMUM AND 0.196 INCHES MAXIMUM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
MIL-S-7947,COND A MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
| ABPX |
MATERIAL THICKNESS |
0.016 INCHES NOMINAL |
| MATT |
MATERIAL |
STEEL COMP 1095 OVERALL |
| ABKV |
OUTSIDE DIAMETER |
0.557 INCHES MINIMUM AND 0.582 INCHES MAXIMUM |
| ABMD |
RECESS DIAMETER |
0.332 INCHES MINIMUM AND 0.342 INCHES MAXIMUM |
| CSTM |
RECESS ANGLE |
99.0 DEGREES MINIMUM AND 103.3 DEGREES MAXIMUM |
| ABKW |
OVERALL HEIGHT |
0.087 INCHES NOMINAL |
| ZZZK |
SPECIFICATION/STANDARD DATA |
80205-NAS1169 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| STYL |
STYLE DESIGNATOR |
FINISHING |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-416,TY 2,CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL AND CHROMATE OVERALL |
