Thank you for taking interest in Boeing Company The part number L1700154-034, which is listed with the NSN 1560-01-633-1715 and a product description of “Rib Stiffener 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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Alongside part number L1700154-034, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Rib Stiffener Aircraft part with the NSN 1560-01-633-1715. For example, you can browse other Boeing Company The components that were produced under CAGE Code 43999 or listings that belong to FSC 1560 Airframe Structural Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number L1700154-034 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-633-1715 Item PartTypeName: RIB,STIFFENER,AIRCRAFT | 1560 | 016331715 | 0 | P | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L1700154-034 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| ABPX | Material Thickness | 0.063 INCHES NOMINAL |
| CXCY | Part Name Assigned By Controlling Agency | RIB,AIR LOAD |
| ABMK | Overall Width | 6.210 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| CZDJ | Aircraft Location | FWD AND AFT-SLAT NUMBER 2,WING PANEL |
| AGAV | End Item Identification | B-1 AIRCRAFT |
| ABHP | Overall Length | 7.940 INCHES NOMINAL |
| CZEK | Aircraft Mission Design Series | B-1 |
| MATT | Material | ALUMINUM ALLOY 2219 |
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