| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625 TYPE II CLASS I MIL STD SINGLE TREATMENT RESPONSE |
| CXCY |
PART NAME ASSIGNED BY CONTROLLING AGENCY |
FAIRING |
| SPCL |
SPECIAL TEST FEATURES |
SULFURIC ACID ANODIZE AND DICHROMATE SEAL AL COMPONENTS PER MIL-A-8625 TYPE II CLASS I |
| ABPX |
MATERIAL THICKNESS |
0.050 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
3.200 INCHES NOMINAL |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
F-15 EAGLE |
| CZDJ |
AIRCRAFT LOCATION |
FAIRING BRACKET F-15 AILERON RETROFIT DESIGN |
| BWJF |
SIDE FOR WHICH DESIGNED |
LEFT SIDE |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS-QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE OR AMS-QQ-A-250/5 FED SPEC 2ND MATERIAL RESPONSE |
| SFTT |
SURFACE TREATMENT |
ANODIZE AND DICHROMATE |
| FEAT |
SPECIAL FEATURES |
MATL 2024-0 BARE AL SHEET OR 2024-0 CLAD AL SHEET, AMS-QQ-A-250/4 OR AMS-QQ-A-250/5; IDENTIFY PER MIL-STS-130;PENETRANT INSPECT PER AMS 2647;HEAT TREAT 0 COND AL ALY TO T-62 PER AMS 2770 AFTER FORMING |
| AGAV |
END ITEM IDENTIFICATION |
F-15 ACFT |
| MATT |
MATERIAL |
ALUMINUM ALLOY 2024 |
| ABHP |
OVERALL LENGTH |
9.800 INCHES NOMINAL |