Thank you for considering General Electric Company part number 1796M20G01, an item we carry that is listed with the NSN 2840-01-444-7013 and product description “Seal Air Aircraft Gas Turbine En.” 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 1796M20G01 was specifically produced by General Electric Company under CAGE Code 07482, and with the NSN 2840-01-444-7013, 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 1796M20G01 today, knowing we will be in touch shortly after reviewing your information.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-444-7013 Item PartTypeName: SEAL,AIR,AIRCRAFT GAS TURBINE EN | 2840 | 014447013 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1796M20G01 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | DIAMETER | 28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| FEAT | SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 62, IND 31; ECP 369; DCN 97-37; HONEYCOMBED; INTERSSTAGE; REPL P/N 9083M60G05 BUT NOT TO BE GRPD PER ECP/DCN; WHOLE NEW CONFIGURATION; AS THE OLD CONFIG IS REPL BY TCTO KITS WITH THE NEW ITEMS, THE OLD CONFIG IS THROWN A |
| MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
| ABHP | OVERALL LENGTH | 2.370 INCHES MINIMUM AND 2.450 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND FEAT |
| CZCJ | STAGE NUMBER | 2 |
| MATT | MATERIAL | TITANIUM ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | B50TF25 CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL |
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