| AGAV |
END ITEM IDENTIFICATION |
ENGINE, AIRCRAFT, F110-GE-100/129 (F-16 C/D); ENGINE, F118-GE-100 (B-2 BOMBER); ENGINE, AIRCRAFT, F-108 (CFM-56, KC-135A) |
| AEPR |
FLANGE OUTSIDE DIAMETER |
0.4800 INCHES MINIMUM AND 0.5200 INCHES MAXIMUM |
| MATT |
MATERIAL |
STEEL COMP 630 OUTER LAYER |
| AGFF |
FLANGE WIDTH |
0.0280 INCHES MINIMUM AND 0.0320 INCHES MAXIMUM |
| BZLX |
CORNER SHAPE |
SQUARE INSIDE LEFT CORNER |
| MATT |
MATERIAL |
PLASTIC POLYAMIDE INNER LAYER AND GLASS FIBER INNER LAYER AND RESIN SYNTHETIC INNER LAYER |
| CSYM |
SURFACE FINISH |
63.0 MICROINCHES LEFT END SURFACE OF BODY AND FLANGE |
| ADAS |
BODY INSIDE DIAMETER |
0.2640 INCHES MINIMUM AND 0.2660 INCHES MAXIMUM |
| STYL |
STYLE DESIGNATOR |
SOLID |
| ABHP |
OVERALL LENGTH |
0.2180 INCHES MINIMUM AND 0.2620 INCHES MAXIMUM |
| BZLX |
CORNER SHAPE |
SQUARE LEFT FLANGE BODY CORNER |
| BZLX |
CORNER SHAPE |
CHAMFERED INSIDE RIGHT CORNER |
| BZLX |
CORNER SHAPE |
SQUARE LEFT FLANGE OUTSIDE RIGHT CORNER |
| CSYM |
SURFACE FINISH |
63.0 MICROINCHES RIGHT END SURFACE OF LEFT FLANGE |
| BZLX |
CORNER SHAPE |
SQUARE OUTSIDE LEFT CORNER |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
FABROID X,FSCM 09455 MFR REF SINGLE MATERIAL RESPONSE INNER LAYER |
| BZLX |
CORNER SHAPE |
SQUARE OUTSIDE RIGHT CORNER |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5643 ASSN STD SINGLE MATERIAL RESPONSE OUTER LAYER |
| CSYM |
SURFACE FINISH |
63.0 MICROINCHES INSIDE DIAMETER SURFACE OF BODY |
| CSYM |
SURFACE FINISH |
63.0 MICROINCHES OUTSIDE DIAMETER SURFACE OF BODY |
| ADAR |
BODY OUTSIDE DIAMETER |
0.3720 INCHES MINIMUM AND 0.3730 INCHES MAXIMUM |