NSN 1560-01-157-8221 of Rib Airfoil - Parts Details
| Alternative NSN: 1560011578221 |
| Item Name: Rib Airfoil |
| FSG: 15 Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC): 1560 Airframe Structural Components |
| NIIN: 011578221 |
| NCB Code: USA (01) |
| Manufacturers: Boeing Company , Dukes Aerospace Inc |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 68A115142-2013, 68A115142-2011 under NSN 1560-01-157-8221 of Rib Airfoil manufactured by Boeing Company, Dukes Aerospace Inc.
Federal Supply Class of NSN 1560-01-157-8221 is FSC 1560 contains part details of Airframe Structural Components. Quote for your desired part numbers.
Part Number's List for NSN 1560-01-157-8221, 1560011578221
-
Part No Manufacturer Item Name QTY RFQ 68A115142-2013 Boeing Company rib airfoil Avl RFQ 68A115142-2013 Dukes Aerospace Inc rib airfoil Avl RFQ 68A115142-2011 Boeing Company rib airfoil Avl RFQ
Characteristics Data of NSN 1560011578221MRC Criteria Characteristic ABHP OVERALL LENGTH 31.000 INCHES NOMINAL ABMK OVERALL WIDTH 5.500 INCHES NOMINAL ABPX MATERIAL THICKNESS 4.000 INCHES NOMINAL BWJF SIDE FOR WHICH DESIGNED LEFT SIDE CZDJ AIRCRAFT LOCATION AFT CZEJ AIRCRAFT STATION NUMBER XW188.255 CZEK AIRCRAFT MISSION DESIGN SERIES F-15 MATT III MATERIAL ALUMINUM ALLOY 7075 MDCL III MATERIAL DOCUMENT AND CLASSIFICATION MMS 159 T7351 MIL SPEC SINGLE MATERIAL RESPONSE
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 31.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 5.500 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 4.000 INCHES NOMINAL |
| BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
| CZDJ | AIRCRAFT LOCATION | AFT |
| CZEJ | AIRCRAFT STATION NUMBER | XW188.255 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-15 |
| MATT | III MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | III MATERIAL DOCUMENT AND CLASSIFICATION | MMS 159 T7351 MIL SPEC SINGLE MATERIAL RESPONSE |