| MRC |
Requirement Statement |
Characteristics |
| ABMX |
CENTER HOLE SHAPE STYLE |
ROUND |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
RECTANGULAR |
| AAUB |
HOLE DIAMETER |
0.4380 INCHES MINIMUM AND 0.4490 INCHES MAXIMUM |
| AGAV |
III END ITEM IDENTIFICATION |
FIXED WING AIRCRAFT, BOEING MODEL757 |
| MATT |
MATERIAL |
STEEL CORROSION RESISTING OVERALL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5525 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ADAV |
OVERALL DIAMETER |
0.830 INCHES MINIMUM AND 0.850 INCHES MAXIMUM |
| ABMW |
PERIPHERAL SHAPE STYLE |
ROUND |
| FEAT |
SPECIAL FEATURES |
SUBASSEMBLY IS FLAP ASSY-TE INBD REFER TO BOEING I.P.C. BOE2427 27-51-02-10A NO. 712 |
| ZZZK |
SPECIFICATION/STANDARD DATA |
81205-BACW10BN MANUFACTURERS SOURCE CONTROL |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-416, TY 2, CL 2 FED SPEC 1ST TREATMENT RESPONSE OVERALL |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL |
| ABNM |
THICKNESS |
0.4380 INCHES MINIMUM AND 0.4490 INCHES MAXIMUM |
