The Spacer,compressor Rotor,aircraft, cataloged under National Stock Number 2840-01-320-0704, 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 1 specification, cited from the U.S. Government catalog. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 2840-01-320-0704 |
| Primary Part Number | 1441M62P01 |
| Item Name | Spacer,compressor Rotor,aircraft |
| FSC / FSG | 2840 / 28 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components |
| Manufacturer | General Electric Company |
| Status | ACTIVE |
| Material | TITANIUM ALLOY |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL Q — CCL Item — Commerce Control List |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Part Number | Manufacturer |
|---|---|
| 1441M62P01 PRIMARY | General Electric Company (USA) |
NSN 2840-01-320-0704 is a Spacer,compressor Rotor,aircraft, manufactured by General Electric Company, classified under FSC 2840, Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. Status: active.
NSN 2840-01-320-0704 has 1 manufacturer part number on file: 1441M62P01 (General Electric Company).
Key specifications for 1441M62P01: Special Features: 1.3680-1.3620 IN. OF LENGTH IS TAPERED TO AN OUTSIDE DIA OF 6.4100-6.4120 IN. AND AN INSIDE DIA OF 6.2450-6.2550 IN.; TAPERED EDGE HAS 6 EQUALLY SPACED PRONGS PROJECTING INTERNALLY W/BOLT HOLES CENTRALLY LOCATED ON EACH PRONG W/DIA OF 0.2620-0.2690 IN.,PRONGS ARE 0.5900-0.6100 IN. WIDE AND 0.6435-0.6475 IN. LONG; AT BEGINNING OF TAPER 6 EQUALLY SPACED NOTCHES ARE LOCATED 0.2400-0.2600 IN. WIDE AND 0.4450-0.4550 IN. LONG PROJECTING INTERNALLY; OPPOSITE OF TAPERED END ARE 6 EQUALLY SPACED PRONGS PROJECTING INTERNALLY W/BOLT HOLES CENTRALLY LOCATED ON EACH PRONG W/DIA OF 0.2620-0.2690 IN. AND CHAMFERED 0.0250-0.0350 IN.,45 DEG; ALL BOLT HOLES HAVE 63.0 MICROINCH FINISH IN; Material: TITANIUM ALLOY. 1 specification is 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 2840-01-320-0704 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.