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MRC | Criteria | Characteristic |
---|---|---|
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416, TY 2, CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
ADAS | BODY INSIDE DIAMETER | 0.4840 INCHES MINIMUM AND 0.4851 INCHES MAXIMUM |
MATT | MATERIAL | STEEL COMP 630 OVERALL |
FEAT | SPECIAL FEATURES | SUBASSEMBLY IS SUPPORT INSTL-WINGINBD TE PNL; REFER TO BOEING I.P.C. B OE2330 57-51-01-07 NO. 111 |
AGFF | FLANGE WIDTH | 0.0550 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM |
ADAR | BODY OUTSIDE DIAMETER | 0.6257 INCHES MINIMUM AND 0.6265 INCHES MAXIMUM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4640 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
AEPR | FLANGE OUTSIDE DIAMETER | 0.7500 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 0.1900 INCHES NOMINAL |
STYL | STYLE DESIGNATOR | SOLID |
BZLX | CORNER SHAPE | SQUARE OUTSIDE LEFT CORNER SQUARE OUTSIDE RIGHT CORNER SQUARE INSIDE RIGHT CORNER SQUARE INSIDE LEFT CORNER SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER UNDERCUT LEFT FLANGE BODY CORNER |
AGAV | III END ITEM IDENTIFICATION | FIXED WING AIRCRAFT, BOEING MODEL757 |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
BAC-23 | BAC 1520-1063 | BAC-21 | BAC 1520-1200 |
BAC-100-25RCSS | BAC-200-25 | BAC-21B | BAC-211 |
BAC-160-25RC-FF | BAC-22 | BAC-100-25RCFF | BAC-23 |
BAC-100-25RCFF | BAC-29 | BAC 3106-10 | BAC-28 |
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