We appreciate your interest in Lockheed Martin Corporation part number 205-061-631-11, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 205-061-631-11 is listed with the NSN 1560-00-789-4964 and description “Crossover Fuel Standard.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Lockheed Martin Corporation under the CAGE Code 80070 or that similarly fall under the FSC 1560 Airframe Structural Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 1560-00-789-4964 parts and Crossover Fuel Standard items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-00-789-4964 Item PartTypeName: CROSSOVER,FUEL,STANDARD | 1560 | 007894964 | P | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | ||||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
91236-21 | 6 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | AIRCRAFT MODEL UH-1D |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | INTERNAL PROOF PRESSURE TEST 5 PSIG,BURST PRESSURE TEST 10 PSIG,FLEXIBLE SECTION RESISTANT TO HYDRAULIC FLUID TO 160.0 DEG F,1 END FLANGED CONNECTION,2ND END FLARED W/NUT AND SLEEVE,9.200 IN. LG,7.220 IN. CONNECTING SPAN,0.750 IN. OD END TU |
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