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Quote for 421117 by Turbo Power And Marine System Inc (CAGE Code 11449) with NSN 5340-00-808-1002

Mfg Part Number: 421117
CAGE Code : 11449
Item Name : Bracket Angle
NIIN: 008081002

If you have been searching for 421117 of Bracket Angle components with NSN 5340008081002 under FSC 5340 Hardware Commercial, look no further than Limitless Aerospace. 421117 part is listed alongside the other Bracket Angle parts, and it has been manufactured by Turbo Power And Marine System Inc (CAGE Code 11449). With current availability through our website, we invite you to request a quick and competitive quote for 421117 by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.

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NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as Turbo Power And Marine System Inc. Get started on the purchasing process for 421117 today and see how we can serve as your strategic sourcing partner for all of your operational needs.


NSN Information for Part Number 421117 with NSN 5340-00-808-1002, 5340008081002

NSNFSCNIINCLSHazmatDEMILCancelled NSN
5340-00-808-1002

Item Description:

Bracket Angle

53400080810020P
CIICHCCESDPMICCriticalityENAC
U A
Part NumberISCRNVCRNCCHCCMSDSSADC
421117295

Characteristics Data of NSN 5340-00-808-1002, 5340008081002

MRCCriteriaCharacteristic
ADLKFIRST LEG LENGTH0.730 INCHES NOMINAL
ADLLSECOND LEG LENGTH0.970 INCHES NOMINAL
AGAVIII END ITEM IDENTIFICATIONW/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H)
AHLFSECOND LEG WIDTH4.220 INCHES NOMINAL
AHLGSECOND LEG CORNER RADIUS0.219 INCHES NOMINAL
AHLKFIRST LEG HOLE DIAMETER0.339 INCHES MINIMUM AND 0.349 INCHES MAXIMUM
AHPWFIRST LEG THICKNESS0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM
AHPXSECOND LEG THICKNESS0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM
AHQWFIRST LEG DISTANCE BETWEEN LOWER HOLE CENTERS ALONG WIDTH1.919 INCHES NOMINAL
AHQXFIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH0.031 INCHES NOMINAL
AHQYFIRST LEG DISTANCE BETWEEN FIRST AND SECOND HOLE CENTERS ALONG WIDTH0.959 INCHES NOMINAL
AHRBFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.250 INCHES NOMINAL
AKAUFIRST LEG HOLE ARRANGEMENT STYLETHREE HOLES
CSSQFIRST LEG ANGLE90.0 DEGREES NOMINAL
MATTMATERIALSTEEL COMP 4130 OR STEEL COMP 8630
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 6350 ASSN STD 1ST MATERIAL RESPONSE OR AMS 6355 ASSN STD 2ND MATERIAL RESPONSE
SFTTSURFACE TREATMENTCADMIUM
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONAMS 2400 ASSN STD SINGLE TREATMENT RESPONSE
STYLSTYLE DESIGNATORANGLE
AKBUSECOND LEG STYLECORNER RADIUS

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