Part Number 1270M42G01 with NSN 5340012150149 by Aerospace Industries Inc - Request for Quote Now!

Part Number: 1270M42G01
Manufacturer: Aerospace Industries Inc
NIIN: 012150149
Item Name : Bracket Angle
CAGE Code: 0AMR1
FSG: 53 Hardware and Abrasives
Country: USA
NCB Code: 01

Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number 1270M42G01, a Aerospace Industries Inc item that is listed alongside the description “Bracket Angle” and the NSN 5340012150149. To guarantee a swift procurement process for NSN part number 1270M42G01, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.

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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number 1270M42G01 is manufactured by Aerospace Industries Inc, it is specifically done so under CAGE Code 0AMR1, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 5340-01-215-0149, one can also determine that this part falls under FSC 5340 Hardware Commercial. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.

NSN Information for Part Number 1270M42G01 with NSN 5340-01-215-0149, 5340012150149

NSNFSCNIINCLSHazmatDEMILCancelled NSN
5340-01-215-0149

Item PartTypeName:

BRACKET,ANGLE

53400121501490P
CIICHCCESDPMICCriticalityENAC
UA0
Part NumberISCRNVCRNCCHCCMSDSSADC
1270M42G01525

Characteristics Data of NSN 5340-01-215-0149, 5340012150149

MRCCriteriaCharacteristic
ACHYMOUNTING HOLE TYPEPLAIN
AGAVEND ITEM IDENTIFICATIONW/S: MISSILE,AIR LAUNCH CRUISE (ALCM) AGM-86B; ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); U-2 ENGINE (F-118-GE-101); ENGINE,F118-GE-100 (B-2 BOMBER); ENGINE,AIRCRAFT,F110-GE-100/129 (F-16 C/D); ENGINE,AIRCRAFT,F-108 (CFM-56,KC-135A); EN
AHLKFIRST LEG HOLE DIAMETER0.337 INCHES MINIMUM AND 0.351 INCHES MAXIMUM
AHLNSECOND LEG HOLE DIAMETER0.274 INCHES MINIMUM AND 0.288 INCHES MAXIMUM
AHLSSECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH1.150 NOMINAL INCHES
AHPWFIRST LEG THICKNESS0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM
AHPXSECOND LEG THICKNESS0.060 INCHES MINIMUM AND 0.066 INCHES MAXIMUM
AHQUFIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH1.088 INCHES NOMINAL
AJZUFIRST LEG STYLECORNER RADIUS
AKAUFIRST LEG HOLE ARRANGEMENT STYLETWO HOLES
AKCUSECOND LEG HOLE ARRANGEMENT STYLETWO HOLES
CBBLFEATURES PROVIDEDNUT
CSSPSECOND LEG RELATIONSHIP TO FIRST LEGNOT IDENTICAL
CSSQFIRST LEG ANGLE90.0 DEGREES NOMINAL
FEATSPECIAL FEATURESFURNISHED WITH 2 NUTPLATES (ITEM 2); EACH NUTPLATE HAS FLOATING NUT AND 2 RIVET HOLES,0.098 IN. MIN,0.102 IN. MAX DIA,AND 4 RIVETS (ITEM 3),2 FOR EACH NUTPLATE
MATTMATERIALNICKEL ALLOY 625
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 5599 ASSN STD SINGLE MATERIAL RESPONSE
STYLSTYLE DESIGNATORANGLE

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