NSN - 4730-00-555-8203, 4730005558203 of Nut Tube Coupling

Aviation Axis stocks 118-21600-230-4, 137618257, 156 15, 202-21600W4, 2652291W4 - Nut Tube Coupling made by Designed Metal Connections Inc, Dana Inc, Oto Melara Spa, Wellman Group, Triumph Aerostructures Llc with 4730-00-555-8203. Owned and operated by ASAP Semiconductor, we have access to over 2 billion new and after-market parts applicable within the aerospace and defense industries. All our parts are shipped using our premier shipping and supply chain. We offer short lead-times and some of the fastest shipping times in the industry. We are well-equipped to handle any customer situation - including AOG. Submit an RFQ today and expect a response within 15 minutes or less. ASAP - the evolution of purchasing.

Part No Manufacturer Item Name QTY RFQ
118-21600-230-4 designed metal connections inc nut tube coupling Avl RFQ
118-21600-230-4 dana inc nut tube coupling Avl RFQ
137618257 oto melara spa nut tube coupling Avl RFQ
156 15 wellman group nut tube coupling Avl RFQ
202-21600W4 triumph aerostructures llc nut tube coupling Avl RFQ
2652291W4 parker hannifin ltd nut tube coupling Avl RFQ
AS18280 sae international nut tube coupling Avl RFQ
AS18280 society of automotive engineers inc nut tube coupling Avl RFQ
AS21921 society of automotive engineers inc nut tube coupling Avl RFQ
AS21921 sae international nut tube coupling Avl RFQ
AS21921-4D society of automotive engineers inc nut tube coupling Avl RFQ
AS21921-4D sae international nut tube coupling Avl RFQ
CVC4257W4 triumph aerostructures llc nut tube coupling Avl RFQ
MS21921-4D society of automotive engineers inc nut tube coupling Avl RFQ
MS21921-4D sae international nut tube coupling Avl RFQ
VSF1212-4WW alcoa global fasteners inc nut tube coupling Avl RFQ
VSF1212-4WW alcoa fastening systems ltd nut tube coupling Avl RFQ

Technical Characteristics of NSN 4730005558203

MRCCriteriaCharacteristic
AAJDTHREAD CLASS3B
AAJFTHREAD DIRECTIONRIGHT-HAND
AARNFABRICATION METHODANY ACCEPTABLE
ACTANUT STYLETUBE COUPLING
ADEANUT HEIGHT0.710 INCHES MINIMUM AND 0.730 INCHES MAXIMUM
AGAVEND ITEM IDENTIFICATIONAIRCRAFT APPLICATION,IROQUIS UH-1,CHINOOK CH-47 HELICOPTER,DELTA DART F-106,F-111. TOMCAT F-14A,STARLIFTER C-141 AIRCRAFT,E-3A AIRCRAFT WARNING AND CONTROL SYSTEM (AWACS)
ASDBWIDTH ACROSS FLATS0.562 INCHES NOMINAL
BRQLLENGTH TO SHOULDER0.537 INCHES MINIMUM AND 0.557 INCHES MAXIMUM
BSPXSMALLEST INSIDE DIAMETER0.300 INCHES MINIMUM AND 0.305 INCHES MAXIMUM
BZRRTHREAD SERIESUNJF
CMLPTHREAD QUANTITY PER INCH20
CQJXNOMINAL THREAD SIZE0.438 INCHES
CQRJNOMINAL TUBE OUTSIDE DIAMETER0.250 INCHES
CRRBSEAT ANGLE45.00 DEGREES NOMINAL
CRTLCRITICALITY CODE JUSTIFICATIONFEAT
FEATSPECIAL FEATURESGRUMMAN AEROSPACE CORP A10 AIRCRAFT; WEAPON SYSTEM ESSENTIAL
MATTMATERIALALUMINUM ALLOY 2014 OVERALL OR ALUMINUM ALLOY 2024 OVERALL
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-367,T6 FED SPEC SINGLE MATERIAL RESPONSE OVERALL OR QQ-A-225/6,T6,T62 OR T851 FED SPEC SINGLE MATERIAL RESPONSE OVERALL
SFTTSURFACE TREATMENTANODIZE OVERALL
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-A-8625,TYPE 2,CLASS 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
ZZZKSPECIFICATION/STANDARD DATA96906-MS21921 GOVERNMENT STANDARD

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