Thank you for taking interest in Boeing Company The part number 68A332089-2001, which is listed with the NSN 1560-01-466-3721 and a product description of “Frame Access Hole Aircraft.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-466-3721 Item PartTypeName: FRAME,ACCESS HOLE,AIRCRAFT | 1560 | 014663721 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
68A332089-2001 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABPX | Material Thickness | 0.088 INCHES NOMINAL |
ABMK | Overall Width | 9.064 INCHES NOMINAL |
MATT | Material | TITANIUM ALLOY |
CZEJ | Aircraft Station Number | FS761.000 TO FS772.500 |
ABHP | Overall Length | 10.010 INCHES NOMINAL |
FEAT | Special Features | NEXT HIGHER ASSEMBLY PART NUMBER 68A332078;U/OF-15C CUM 354 AND UP,F-15C CUM 354 AND UP,F-15D CUM 59 AND UP,F-15E CUM 2 AND UP;TITANIUM ALLOY PER 6AL-6V-2SN |
CZEK | Aircraft Mission Design Series | F-15C,D,E |
CZDJ | Aircraft Location | HORIZONTAL STABILIZER |
BWJF | Side For Which Designed | RIGHT SIDE |
MRC | Decoded Requirement | Clear Text Reply |
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