Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1807M26, which you have taken interest in. This Blade Turbine Rotor Aircraft Gas item is listed alongside the NSN 2840-01-444-7012 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 1807M26 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 2840-01-444-7012 part number 1807M26 today, knowing we will support all your operational needs with care.
| 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 |
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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