Part No. : 68A332118-2004 | Alternate P/N : 68A3321182004 | Manufacturer : boeing company the |
Item Name: stiffener aircraft | NSN: 1560-01-474-0318 (1560014740318) | CAGE Code: 76301 |
FSC: 1560 Airframe Structural Components |
If you require part number 68A332118-2004 from Boeing Company The which is described as a Stiffener Aircraft component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 68A332118-2004 which is listed under the Federal Supply Class 1560 Airframe Structural Components. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 1560014740318 and was produced under the CAGE Code 76301. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 68A332118-2004 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs. 68A332118-2004
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-474-0318 Item Description: Stiffener Aircraft | 1560 | 014740318 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
68a332118-2004 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 11.000 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 2.380 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.045 INCHES NOMINAL |
CZDJ | AIRCRAFT LOCATION | UPPER INBOARD SKIN,AFT CLOSURE BEAM |
CZEK | AIRCRAFT MISSION DESIGN SERIES | F-15A,B |
FEAT | SPECIAL FEATURES | DIM. ARE STOCK MATERIAL; U/O F-15A,B CUM1-BLK11; NEXT HIGHER ASSY 68A332001 |
MATT | III MATERIAL | TITANIUM ALLOY |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046,TYPE 3,COMP C,ANL MIL SPEC SINGLE MATERIAL RESPONSE |
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