| AIRCRAFT LOCATION | INBOARD MOUNT - ENGINE |
| AIRCRAFT MISSION DESIGN SERIES | F/A-18 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | 17-7PH, COND A, 1201NN CREST SHEET PER MIL-S-25043 (AMS 5528) MIL SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.090 INCHES NOMINAL |
| III MATERIAL | STEEL CORROSION RESISTING |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 17.500 INCHES NOMINAL |
| OVERALL WIDTH | 3.100 INCHES NOMINAL |
| SPECIAL FEATURES | NHA: 74A093143. NO HOLES CONFIGURATION |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | HEAT TREAT TO COND TH 1050, PER PS15226 MFR REF 1ST TREATMENT RESPONSE AND APPLY ONE COAT OF GRAY ANI-CHAFE PAINT PER PS13555 AFTER STF FINISH MIL SPEC 2ND TREATMENT RESPONSE |
| SURFACE TREATMENT | PAINT |