The Blade,compressor,aircraft Gas Tu, cataloged under National Stock Number 2840-00-877-0065, 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 Rolls-Royce Corporation. Government technical data includes 2 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through both NSN and commercial part number lookups. 2 additional reference documents (drawings, advisory and superseded references) are recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 2840-00-877-0065 |
| Primary Part Number | 6809081 |
| Item Name | Blade,compressor,aircraft Gas Tu |
| FSC / FSG | 2840 / 28 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components |
| Manufacturer | Rolls-Royce Corporation |
| Status | ACTIVE |
| Criticality Code Justification | AGAV |
| Material | STEEL CORROSION RESISTING OVERALL |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL Q — CCL Item — Commerce Control List |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | F |
| Part Number | Manufacturer |
|---|---|
| 6809081 PRIMARY | Rolls-Royce Corporation (USA) |
| 6809081 | Pacific Sky Supply, Inc. Dba Pacific Sky Supply Inc (USA) |
| Reference | Meaning |
|---|---|
| 6809081 | 5/9 Secondary reference Allison Transmission Inc Dba Allison Transmission, Inc |
| 6809081 | 5/9 Secondary reference General Motors Corp |
NSN 2840-00-877-0065 is a Blade,compressor,aircraft Gas Tu, manufactured by Rolls-Royce Corporation, classified under FSC 2840, Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. Status: active.
NSN 2840-00-877-0065 has 2 manufacturer part numbers on file: 6809081 (Rolls-Royce Corporation), 6809081 (Pacific Sky Supply, Inc. Dba Pacific Sky Supply Inc).
Key specifications for 6809081: Criticality Code Justification: AGAV; Overall Length: 3.753 INCHES NOMINAL IN; Overall Width: 1.197 INCHES NOMINAL IN; Special Features: CONTOUR OF CONCAVE AND CONVEX SIDES OF AIRFOIL SECTIONS MAY VARY WITHIN A .006 BAND PARALLEL TO BASIC; TOLERANCE BAND APPLIES TO SECTION CONTOURS UP TO TANGENT POINT OF LEADING AND TRAILING EDGE RADII; AIRFOIL SURFACES SHALL BLEND SMOOTHLY BETWEEN DEFINED CONTOUR POINTS AND SECTIONS; THE STACKING AXIS IS A STRAIGHT LINE DEFINING THE BASIC LOCATION OF THE AIRFOIL SECTION STACKING POINTS; AIRFOIL SECTION STACKING POINTS MAY BE DISPLACED A MAXIMUM OF .003" FROM STACKING AXIS; THE ANGULAR RELATION OF THE STACKING AXIS MAY VARY .010" PER INCH IN ANY DIRECTION IN RELATION TO THE GAGE PLANE OF THE BASE; ANGULAR VARIATION OF AIRFOIL SECTIONS ABOUT THE STACKING AXIS SHALL NOT EXCEED 0 DEGREES 15' RELATIVE TO ANGLE DATUM PLAN; FORGING SHALL CONFORM TO E15 502; NO PERMANENT TYPE MARKING PERMITTED ON AIRFOIL SURFACES. 2 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 2840-00-877-0065 has DEMIL Code Q. 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.