Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-01-136-0551 An item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals.
Alternate Parts: 23004267, 23004267, 2840-01-136-0551, 01-136-0551, 2840011360551, 011360551
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 03, 1982 | 01-136-0551 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-136-0551
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23004267 | 73342 | ALLISON TRANSMISSION, INC. |
| 23004267 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-136-0551
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 6.417 INCHES NOMINAL |
| SPECIAL FEATURES | 1ST END EXTERNALLY SPLINED; 23 TEETH, 0.4792 IN PITCH DIA FOR 1.520 IN.; FOR BLEED VALVE ACTUATOR; 2ND END BORED 0.6265-0.6295 IN. DIA. FOR 0.720 IN HAS FORKED PROTRUSION W/0.50 IN. DIA. HOLE THROUGH BOTH FORKS |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AMATT$$AMDCL |
| END ITEM IDENTIFICATION | ACFT ENG TF41 |