| Part Number: 69 6122 2 | Manufacturer: Fmw Inc |
| NSN : 1560-01-530-2176 (1560015302176) | Item Name : stiffener aircraft |
| CAGE Code: 1QJK4 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 6961222 | INC Code: 41029 |
| NIIN : 01-530-2176 (015302176) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 01 |
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| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 15.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 4.800 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | KC-135 ACFT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER-BALANCE PANEL |
| CZDJ | AIRCRAFT LOCATION | OUTBOARD AILERON |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT |
| FEAT | SPECIAL FEATURES | HEAT TREAT T4; OPPOSITE -2 (EXCEPT AS SHOWN); USED ON DWG 5-96130 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-3621 FED SPEC SINGLE MATERIAL RESPONSE |
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