Using the Request for Quote (RFQ) form provided on this page, you can request competitive procurement options on part number AAC4311-121012 with rapid responses always offered by our staff. To ensure that you locate and procure exactly what you need with ease, we list parts with as much information as we can. For example, part number AAC4311-121012 It is listed as Tee Tube. component manufactured by Allan Aircraft Supply Co Llc, specifically under CAGE Code 06581. It is also accompanied by the NSN 4730013915867 for ease of organization, the first digits of the NSN indicating that the part belongs to FSC 4730 Hose Pipe Tube Lubrication and Railing Fittings.
NSN Information for Part Number AAC4311-121012 with NSN 4730-01-391-5867, 4730013915867
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
4730-01-391-5867 Item Description: Tee Tube | 4730 | 013915867 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Aac4311-121012 | 5 | 2 | 5 |
Characteristics Data of NSN 4730-01-391-5867, 4730013915867
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | AIRCRAFT; B-2 BOMBER |
AEHZ | MAXIMUM OPERATING TEMP | -65.0 DEG FAHRENHEIT 1ST RESPONSE |
CWFD | NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.625 INCHES 2ND END |
CQGM | MAXIMUM OPERATING PRESSURE | 4000.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
MATT | MATERIAL | TITANIUM ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4965 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
AHSJ | LEG LENGTH | 1.719 INCHES NOMINAL 1ST END 1.620 INCHES NOMINAL 2ND END 1.719 INCHES NOMINAL 3RD END |
CWFK | TUBING WALL NOMINAL THICKNESS FOR WHICH DESIGNED | 0.115 INCHES 1ST END 0.097 INCHES 2ND END 0.115 INCHES 3RD END |
FEAT | SPECIAL FEATURES | CRYOFIT END CONNECTIONS |
AHNC | CONNECTION STYLE | PLAIN (TUBE) ALL ENDS |
AWLS | CONNECTION TYPE | UNTHREADED EXTERNAL TUBE ALL ENDS |
MEDA | MEDIA FOR WHICH DESIGNED | AERONAUTICAL FLUID SINGLE RESPONSE |