| 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 |