Thank you for your interest in part number 432047, a component manufactured by United Technologies Corporation that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-00-816-8451 and features the description “Bracket Assembly Case Turbine Ex.” To request a quote for part number 432047, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-00-816-8451 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from United Technologies Corporation, which is associated with the CAGECode 77445. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 432047.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-816-8451 Item PartTypeName: BRACKET ASSEMBLY,CASE,TURBINE EX | 2840 | 008168451 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
432047 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | ENGINE MODEL TF33 |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,AMS 5504 BRACKET MATERIAL,ROCKWELL C30-38 HARDNESS,TWO 90 DEG ANGLES,0.310-0.330 IN. CENTER LEG LG,0.790-0.830IN. LONG LEG LG,0.800-0.820 IN. SHORT LEG LG,0.490-0.510 IN. W,1.110-1.130 IN. HOLE CENTER TO HOLE CENTER,CONSISTING OF 1 PAR |
ZZZV | FSC APPLICATION DATA | AIRCRAFT JET ENGINE |
FEAT | SPECIAL FEATURES | FORM,FIT,FUNICITION |
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