| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
C-17A AIRCRAFT |
| BPCJ |
DISTANCE BETWEEN HOLE CENTERS |
1.500 INCHES NOMINAL |
| ASXK |
HOLE QUANTITY |
2 |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| ABPX |
MATERIAL THICKNESS |
0.188 INCHES NOMINAL |
| MATT |
MATERIAL |
ALUMINUM ALLOY 6061 |
| ABTB |
MOUNTING HOLE DIAMETER |
0.193 INCHES NOMINAL |
| ACHY |
MOUNTING HOLE TYPE |
PLAIN |
| ABKW |
OVERALL HEIGHT |
0.820 INCHES NOMINAL |
| ABHP |
OVERALL LENGTH |
2.250 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
0.932 INCHES NOMINAL |
| CXCY |
PART NAME ASSIGNED BY CONTROLLING AGENCY |
FITTING,CLEVIS |
| FEAT |
SPECIAL FEATURES |
THERE IS ALSO ONE HOLE THAT HAS ADIAMETER OF .257 INCHES |
| STYL |
STYLE DESIGNATOR |
QUADRUPLE ANGLE |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625, TYPE III, CLASS I FED SPEC SINGLE TREATMENT RESPONSE |
| SFTT |
SURFACE TREATMENT |
ANODIZE |
