You have arrived on the Request for Quote (RFQ) page for part number 68A332089-2001, a Boeing Company The component that is listed with the product description “Frame Access Hole Aircraft” and NSN 1560-01-466-3721 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Boeing Company The part number 68A332089-2001, you can seamlessly search for more items from this manufacturer or CAGECode 76301 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 1560 Airframe Structural Components, which this component falls under having the NSN 1560-01-466-3721. Whether you desire part number 68A332089-2001 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| 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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