| MRC |
Requirement Statement |
Characteristics |
| ABMX |
CENTER HOLE SHAPE STYLE |
ROUND |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
RECTANGULAR |
| AAUB |
HOLE DIAMETER |
0.338 INCHES MINIMUM AND 0.449 INCHES MAXIMUM |
| AGAV |
III END ITEM IDENTIFICATION |
FIXED WING AIRCRAFT, BOEING MODEL757 |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| MATT |
MATERIAL |
ALUMINUM ALLOY 2024 OVERALL |
| ADAV |
OVERALL DIAMETER |
0.830 INCHES MINIMUM AND 0.850 INCHES MAXIMUM |
| ABMW |
PERIPHERAL SHAPE STYLE |
ROUND |
| FEAT |
SPECIAL FEATURES |
SUBASSEMBLY IS WING, FITTING AND SPLICE INSTL-FRONT SPAR REFER TO BOEING I.P.C. BOE2428 53-41-57-02 NO. 85 |
| ZZZK |
SPECIFICATION/STANDARD DATA |
81205-BACW10BN MANUFACTURERS STANDARD |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625, TY 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| SFTT |
SURFACE TREATMENT |
ANODIZE OVERALL |
| ABNM |
THICKNESS |
0.064 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
