Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Plate Engine Aft Fuselage items. You have expressed particular interest in part number 215-49418-2, a Triumph Aerostructures Llc component we offer that is presented with the NSN 1560-00-134-1088 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number 215-49418-2 is manufactured by Triumph Aerostructures Llc under the CAGE Code 80378. Additionally, by using the initial digits of the NSN 1560-00-134-1088, you can discover that this component is associated with the FSC 1560 Airframe Structural Components. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number 215-49418-2 at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-00-134-1088 Item PartTypeName: PLATE,ENGINE AFT FUSELAGE | 1560 | 001341088 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 215-49418-2 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 0.500 IN. THK,6.240 IN. W; 4 HOLES 0.4375 IN. DIA,6.780 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE TOP ALONG L,7.080 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE BOTTOM ALONG L,4.540 IN. DISTANCE BETWEEN HOLES ALONG W; 2.500 |
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