Part Details | AIRCRAFT GAS TURBINE ENGINE FAN VANE
2840-01-242-2134 A component of a VANE ASSEMBLY, FAN, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding fan blades and deliver it to the succeeding row of fan blades or compressor at correct pressure, velocity and direction.
Alternate Parts: 1284M93P05, 2840-01-242-2134, 01-242-2134, 2840012422134, 012422134
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 08, 1986 | 01-242-2134 | 50613 ( VANE, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-242-2134
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1284M93P05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-242-2134
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 6.840 INCHES NOMINAL |
| DIAMETER | 2.598 INCHES NOMINAL |
| SPECIAL FEATURES | THREADED 2ND END,0.250-28 UNJF-3A MOD,MAJ DIA. 0.2435-0.2480,MIL-S-8879 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110 ACFT ENGINE |