Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Rib Airfoil items. You have expressed particular interest in part number 215-70200-261, a Triumph Aerostructures Llc component we offer that is presented with the NSN 1560-01-132-7818 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 215-70200-261 is manufactured by Triumph Aerostructures Llc under the CAGE Code 80378. Additionally, by using the initial digits of the NSN 1560-01-132-7818, 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 215-70200-261 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-132-7818 Item PartTypeName: RIB,AIRFOIL | 1560 | 011327818 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
215-70200-261 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 7.500 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 5.800 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
CZDJ | AIRCRAFT LOCATION | INBD LEADING EDGE LANDING FLAP |
CZEK | AIRCRAFT MISSION DESIGN SERIES | A-7 |
FEAT | SPECIAL FEATURES | HEAT TREAT TO COND T42; AGE TO COND T62 |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
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