Thank you for taking interest in Rockwell Collins Aerospace part number 10-263999-183, which is listed with the NSN 5935-00-947-1037 and a product description of “Dummy Connector Receptacle.” 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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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5935-00-947-1037 Item PartTypeName: DUMMY CONNECTOR,RECEPTACLE | 5935 | 009471037 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | U | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
MS3115-18A | 2 | 2 | 2 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.571 INCHES MAXIMUM |
ABKW | OVERALL HEIGHT | 1.328 INCHES MAXIMUM |
ABMK | OVERALL WIDTH | 1.328 INCHES MAXIMUM |
ADZC | ENVIRONMENTAL PROTECTION | MOISTURE RESISTANT AND VIBRATION RESISTANT AND SALT WATER RESISTANT |
AEBV | UNTHREADED MOUNTING HOLE DIAMETER | 0.120 INCHES NOMINAL |
AEBW | CENTER TO CENTER DISTANCE BETWEEN MOUNTING FACILITIES PARALLEL TO HEIGHT | 1.062 INCHES NOMINAL |
AEHA | DISTANCE BETWEEN CENTERLINES OF MOUNTING FACILITIES PARALLEL TO BODY WIDTH | 1.062 INCHES NOMINAL |
AFQK | DISTANCE FROM MOUNTING SHOULDER TO FRONT FACE | 0.462 INCHES MINIMUM AND 0.493 INCHES MAXIMUM |
AFQW | MATING END QUANTITY | 1 |
AFRN | POLARIZATION METHOD | KEYWAY OR MULTIPLE KEYWAY |
AFRP | INSERT POSITION IN DEG | 0.0 |
AFRT | SHELL TYPE | SOLID |
AFRV | CONNECTOR LOCKING METHOD | BAYONET PIN |
AGAV | END ITEM IDENTIFICATION | AIRCRAFT,STRATOLIFTER C-135; F4S AIRCRAFT; AIRCRAFT,TOMCAT F-14; AIRCRAFT,(AC-130-H,MC-130H,EC-130E,HC-130); HELICOPTER,ADVANCE ATTACK,AH |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CSPT | SHELL MATERIAL | ALUMINUM ALLOY |
CSWM | SHELL SURFACE TREATMENT | CADMIUM |
CTBC | SHELL SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE |
FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
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