Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1807M24G01, which you have taken interest in. This Blade Turbine Rotor Aircraft Gas item is listed alongside the NSN 2840-01-444-7701 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 1807M24G01 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, 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 2840-01-444-7701 part number 1807M24G01 today, knowing we will support all your operational needs with care.
| 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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