Thank you for considering General Electric Company part number 1807M26, an item we carry that is listed with the NSN 2840-01-444-7012 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 1807M26 was specifically produced by General Electric Company under CAGE Code 07482, and with the NSN 2840-01-444-7012, 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 1807M26 today, knowing we will be in touch shortly after reviewing your information.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-444-7012 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 014447012 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1807M26G01 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CZCJ | Stage Number | 2 |
| MRC | Decoded Requirement | Clear Text Reply |
| CRTL | Criticality Code Justification | AGAV |
| ABHP | Overall Length | 4.891 INCHES NOMINAL |
| AGAV | End Item Identification | ACFT ENG TF39 |
| CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
| APGF | Design Type | AXIAL COMPRESSOR |
| MATT | Material | ALUMINUM BLADE |
| BGLW | Blade Attachment Method | FIR TREE |
| ABMK | Overall Width | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM |
| FEAT | Special Features | MATERIAL EXTERNAL PLATINUM ALUMINIDE COATING, THIS IS PART OF THE HT90 MOD FOR THE TF39, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, TRAIL |
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