AIRCRAFT LOCATION | WING |
AIRCRAFT MISSION DESIGN SERIES | C-17 |
HEIGHT | 4.850 INCHES MINIMUM AND 4.910 INCHES MAXIMUM |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/11 FED SPEC SINGLE MATERIAL RESPONSE |
MATERIAL | ALUMINUM ALLOY 6061 |
PROPRIETARY CHARACTERISTICS | PACS |
OVERALL LENGTH | 19.660 INCHES MINIMUM AND 19.720 INCHES MAXIMUM |
OVERALL WIDTH | 4.470 INCHES MINIMUM AND 4.530 INCHES MAXIMUM |
SIDE FOR WHICH DESIGNED | RIGHT SIDE |
SPECIAL FEATURES | CONSISTS OF (1) -5 CAN ASSEMBLY,1 FLANGE AND 1 DRAIN; MANUFACTURER SUGGESTD NAME-HOUSING ASSEMBLY-SLAT TRACK NUMBER 9 |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | DPS 11.01-3 MFR REF 1ST TREATMENT RESPONSE AND DPS 4.50-36 MFR REF 2ND TREATMENT RESPONSE AND DPS 4.50-36 MFR REF 3RD TREATMENT RESPONSE |
SURFACE TREATMENT | ANODIZE AND PRIMER AND PAINT EPOXY |