Thank you for considering General Electric Company part number 1807M24G01, an item we carry that is listed with the NSN 2840-01-444-7701 and product description “Blade Turbine Rotor Aircraft Gas.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 1807M24G01 was specifically produced by General Electric Company under CAGE Code 07482, and with the NSN 2840-01-444-7701, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 1807M24G01 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-444-7701 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 014447701 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1807M24 | 6 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM |
ABMK | OVERALL WIDTH | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
BGLW | BLADE ATTACHMENT METHOD | FIR TREE |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
CZCJ | STAGE NUMBER | 2 |
FEAT | SPECIAL FEATURES | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, LEAD |
MATT | III MATERIAL | ALUMINUM BLADE |
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