| FEAT |
SPECIAL FEATURES |
SUBASSEMBLY IS RIB INSTL-RUD STA 131.108 VERT. STAB. FXD TE; REFER TO BOEING I.P.C. BOE2358 55-36-52-02 NO. 40 |
| SFTT |
SURFACE TREATMENT |
PASSIVATE OVERALL OR CADMIUM OVERALL |
| MATT |
MATERIAL |
STEEL CORROSION RESISTING OVERALL |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-35, TY 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL OR QQ-P-416. TY2, CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5525 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| AAVH |
SHOULDER DIAMETER |
0.614 INCHES MINIMUM AND 0.634 INCHES MAXIMUM |
| ABPX |
MATERIAL THICKNESS |
0.064 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| AGAV |
END ITEM IDENTIFICATION |
FIXED WING AIRCRAFT, BOEING MODEL757 |
| AAUB |
HOLE DIAMETER |
0.501 INCHES MINIMUM AND 0.512 INCHES MAXIMUM |
| ABKV |
OUTSIDE DIAMETER |
0.950 INCHES MINIMUM AND 0.970 INCHES MAXIMUM |
| STYL |
STYLE DESIGNATOR |
SHOULDERED AND RECESSED |
| ZZZK |
SPECIFICATION/STANDARD DATA |
81205-BACW10BN MANUFACTURERS STANDARD |