| ADAR |
BODY OUTSIDE DIAMETER |
0.6257 INCHES MINIMUM AND 0.6265 INCHES MAXIMUM |
| FEAT |
SPECIAL FEATURES |
SUBASSEMBLY IS SUPPORT INSTL-WINGINBD TE PNL; REFER TO BOEING I.P.C. B OE2330 57-51-01-07 NO. 111 |
| ADAS |
BODY INSIDE DIAMETER |
0.4840 INCHES MINIMUM AND 0.4851 INCHES MAXIMUM |
| MATT |
MATERIAL |
STEEL COMP 630 OVERALL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 4640 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| AGFF |
FLANGE WIDTH |
0.0550 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM |
| BZLX |
CORNER SHAPE |
SQUARE INSIDE LEFT CORNER |
| ABHP |
OVERALL LENGTH |
0.1900 INCHES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
FIXED WING AIRCRAFT, BOEING MODEL757 |
| STYL |
STYLE DESIGNATOR |
SOLID |
| BZLX |
CORNER SHAPE |
SQUARE INSIDE RIGHT CORNER |
| BZLX |
CORNER SHAPE |
SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER |
| AEPR |
FLANGE OUTSIDE DIAMETER |
0.7500 INCHES NOMINAL |
| BZLX |
CORNER SHAPE |
UNDERCUT LEFT FLANGE BODY CORNER |
| BZLX |
CORNER SHAPE |
SQUARE OUTSIDE LEFT CORNER |
| BZLX |
CORNER SHAPE |
SQUARE OUTSIDE RIGHT CORNER |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-416, TY 2, CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL |