Aerospace Performance Parts is pleased to offer immediate purchasing options for Turbo Power And Marine System Inc part number 446169, which you have taken interest in. This Bracket Angle item is listed alongside the NSN 5340-00-344-2956 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 446169 or any other FSC 5340 Hardware Commercial components we carry from Turbo Power And Marine System Inc under CAGE Code 11449, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 5340-00-344-2956 part number 446169 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5340-00-344-2956 Item PartTypeName: BRACKET,ANGLE | 5340 | 003442956 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
446169 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | CASE ASSEMBLY,TURBINE; W/S: ENGINE,AIRCRAFT TF33-PW-102 (C-135E,EC-135H/K/P); ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); AIRCRAFT,STRATOFORTRESS B-52; ENGINE,AIRCRAFT TF33-P-3/5/9 (C/EC-135,B-52H) |
AHLF | SECOND LEG WIDTH | 1.509 INCHES NOMINAL |
AHLG | SECOND LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
AHLK | FIRST LEG HOLE DIAMETER | 0.224 INCHES NOMINAL |
AHLN | SECOND LEG HOLE DIAMETER | 0.286 INCHES NOMINAL |
AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.009 INCHES NOMINAL |
AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
AHPW | FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
AHPX | SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
AHQN | FIRST LEG WIDTH | 0.510 INCHES NOMINAL |
AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
AJFP | FIRST LEG END RADIUS | 0.375 INCHES NOMINAL |
AJZU | FIRST LEG STYLE | END RADIUS |
AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
AKBU | SECOND LEG STYLE | CORNER RADIUS |
AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
CSSQ | FIRST LEG ANGLE | 130.0 DEGREES NOMINAL |
CSSZ | SECOND LEG OFFSET ANGLE | 80.9 DEGREES NOMINAL |
FEAT | SPECIAL FEATURES | THIS PART MEETS THE Y REQUIREMENTS DUE TO CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM,DEATH OR SERIOUS INJURY |
MATT | MATERIAL | STEEL COMP 410 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE |
STYL | STYLE DESIGNATOR | OFFSET ANGLE |
ZZZV | FSC APPLICATION DATA | ENGINE,JET,AIRCRAFT |
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