INSTANT RFQ

Browse Listing Resources for NSN 5340-00-075-6043

For all the NSN 5340-00-075-6043 parts you are seeking, turn to our vast collection of offerings here on Buy Mil Spares. On this page, part numbers like 3P50004-169, 488073, and others with the NSN 5340-00-075-6043 are featured alongside applicable listing information for your ease of perusal. If any specific item grabs your attention within our NSN 5340-00-075-6043 inventory, you can use the “RFQ” button to its right to access one of our online quote request forms. Once we have an opportunity to receive and assess the details you provided, you can anticipate a tailored response in 15 minutes or less.

To uphold the caliber of our stock, our industry experts carefully assess every supplier, manufacturer, and vendor we source from as needed, while countless components are evaluated by our quality-assurance team or subjected to third-party testing. In addition, we are aware that our customers often encounter rigid schedules and unexpected delivery deadlines, which is why we provide expedited shipping services for various items. Bearing this in mind, get in touch with one of our specialists today to see how we can help you secure all the NSN 5340-00-075-6043 supplies you require.

Item Name Bracket Angle
Federal Supply Group (FSG) Hardware and Abrasives
Federal Supply Class (FSC) 5340 Hardware Commercial
National Item Identification Number (NIIN) 00-075-6043 (000756043)
NCB Code USA (00)
Manufacturer Lockheed Martin Corporation, Turbo Power And Marine System Inc, United Technologies Corporation
Part Number Manufacturer Item Name Cage Code RFQ
3P50004-169 lockheed martin corporation bracket angle 98897 RFQ
488073 turbo power and marine system inc bracket angle 11449 RFQ
488073 united technologies corporation bracket angle 77445 RFQ

Technical Characteristics of NSN 5340000756043

MRCCriteriaCharacteristic
ADLKFIRST LEG LENGTH0.812 INCHES NOMINAL
ADLLSECOND LEG LENGTH2.909 INCHES NOMINAL
AHLFSECOND LEG WIDTH1.593 INCHES NOMINAL
AHLGSECOND LEG CORNER RADIUS0.281 INCHES NOMINAL
AHLKFIRST LEG HOLE DIAMETER0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM
AHLNSECOND LEG HOLE DIAMETER0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM
AHLPSECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH1.031 INCHES NOMINAL
AHLVSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.281 INCHES NOMINAL
AHLWSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.281 INCHES NOMINAL
AHPWFIRST LEG THICKNESS0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM
AHPXSECOND LEG THICKNESS0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM
AHQNFIRST LEG WIDTH1.000 INCHES NOMINAL
AHQPFIRST LEG CORNER RADIUS0.312 INCHES NOMINAL
AHRAFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.500 INCHES NOMINAL
AHRBFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.312 INCHES NOMINAL
AJZUFIRST LEG STYLECORNER RADIUS
AKAUFIRST LEG HOLE ARRANGEMENT STYLEONE HOLE
AKBUSECOND LEG STYLECORNER RADIUS
AKCUSECOND LEG HOLE ARRANGEMENT STYLETWO HOLES
CSSPSECOND LEG RELATIONSHIP TO FIRST LEGNOT IDENTICAL
CSSQFIRST LEG ANGLE88.0 DEGREES NOMINAL
MATTMATERIALSTEEL COMP 410
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 5504 ASSN STD SINGLE MATERIAL RESPONSE
STYLSTYLE DESIGNATORANGLE

Relevant Components for NSN - 5340-00-075-6043, 5340000756043
5340-01-713-6026 (5340017136026) 5305-01-195-7948 (5305011957948) 5325-01-351-7887 (5325013517887) 5310-01-514-1501 (5310015141501)
5365-00-817-9355 (5365008179355) 5310-14-370-1516 (5310143701516) 5340-01-266-6437 (5340012666437) 5355-01-545-3134 (5355015453134)
5330-01-089-1589 (5330010891589) 5305-01-540-4248 (5305015404248) 5340-01-364-2423 (5340013642423) 5340-01-648-4808 (5340016484808)

Submit a Quote and We'll Get Back to You Shortly

Guaranteed quotes back within 15 minutes, 24/7 x 365

Thank You for Visiting.

If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.

Request for Quote

We use cookies to ensure that we give you the best experience on our website. If you continue to use this site we will assume that you are happy with it.

bottom to top