The Rotor,turbine,aircraft Gas Turbi, cataloged under National Stock Number 2840-01-447-2504, is classified within Federal Supply Class 2840 (Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components) of the Engines, Turbines, and Components group. The manufacturer of record is General Electric Company. Government technical data includes 3 specifications, cited from the U.S. Government catalog. The record lists 2 manufacturer part numbers for this item, enabling identification through both NSN and commercial part number lookups. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. 1 item shares a part number with this NSN in the catalog (possible match — not a government interchangeability claim). Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 2840-01-447-2504 |
| Primary Part Number | 9547M19G08 |
| Item Name | Rotor,turbine,aircraft Gas Turbi |
| FSC / FSG | 2840 / 28 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components |
| Manufacturer | General Electric Company |
| Status | ACTIVE |
| Design Type | AXIAL COMPRESSOR |
| Criticality Code Justification | FEAT AND CZBJ |
| Engine Section Location | LOW PRESSURE TURBINE |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL D — Destroy Item |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | F |
| Part Number | Manufacturer |
|---|---|
| 9547M19G07 | General Electric Company (USA) |
| 9547M19G08 PRIMARY | General Electric Company (USA) |
| Reference | Meaning |
|---|---|
| 9547M19 | D/9 Drawing number reference only General Electric Company |
NSN 2840-01-447-2504 is a Rotor,turbine,aircraft Gas Turbi, manufactured by General Electric Company, classified under FSC 2840, Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. Status: active.
NSN 2840-01-447-2504 has 2 manufacturer part numbers on file: 9547M19G07 (General Electric Company), 9547M19G08 (General Electric Company).
1 possible match (shared part number, not a government interchangeability claim): 2840-01-450-8982. Verify interchangeability with system specifications before substitution.
Key specifications for 9547M19G08: Design Type: AXIAL COMPRESSOR; Criticality Code Justification: FEAT AND CZBJ; Engine Section Location: LOW PRESSURE TURBINE; Special Features: MATERIAL IS A CRYSTAL RENE N6, A PRECIPITATION STRENGTHENED ALLOY; ROTOR HAS A NEW REDESIGNED STG 1 BLADE WITH THE NEW MATERIAL; INCREASED LIFE OF BLADE; BLADES ARE STILL DOVETAIL AND ARE IDENTICAL TO THE OLD CONFIGURATION P/N 1475M47P01; NEW BLADES ARE INTERCHANGEABLE IN COMPLETE SETS ONLY; INTERMIXING OF BLADES, OLD AND NEW, WILL NOTBE ALLOWED; SINCE DOVETAILS ARE IDENTICAL AND WILL FIT IN THE SAME DISK, NO CHANGES TO DISK. 3 specifications are documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.
NSN 2840-01-447-2504 has DEMIL Code D. Demilitarization may be required before disposal or transfer to non-military entities.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.