Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 9123962-10, a Northrop Grumman Systems Corporation item with the NSN 1560013586993 that is listed alongside the description “Panel Structural Ai.” If you are interested in part number 9123962-10 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 9123962-10 is specifically listed with the NSN 1560-01-358-6993, and this code can be used to determine that it falls under FSC 1560 Airframe Structural Components. Additionally, while tracing back to Northrop Grumman Systems Corporation, this NSN part was specifically produced under CAGE Code 26512. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-358-6993 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 013586993 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9123962-10 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | COMPOSITE |
| ABHP | OVERALL LENGTH | 16.000 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | A-10A |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-R-9300B MIL SPEC SINGLE MATERIAL RESPONSE |
| ABMK | OVERALL WIDTH | 24.000 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | ENGINE NACELLE LOWER INNER PANEL |
| ABNM | THICKNESS | 0.050 INCHES NOMINAL |
| MATT | MATERIAL | GLASS FIBER |
| SFTT | SURFACE TREATMENT | PRIMER EPOXY-POLYAMIDE AND PAINT POLYURETHANE |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |
| CZEJ | AIRCRAFT STATION NUMBER | NS158.245 TO NS171.500 |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-C-83286 MIL SPEC 2ND TREATMENT RESPONSE |
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