Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR SPACER
2840-01-320-0704 A rigid item designed to maintain a predetermined space between two ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may be a complete 360 degrees or a section thereof.
Alternate Parts: 1441M62P01, 2840-01-320-0704, 01-320-0704, 2840013200704, 013200704
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 18, 1990 | 01-320-0704 | 52427 ( SPACER, COMPRESSOR ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-320-0704
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1441M62P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-320-0704
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| 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 |