Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHAFT
2840-00-981-6997 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: 110062001, 1-100-620-01, 110062001, 1-100-620-01, 2840-00-981-6997, 00-981-6997, 2840009816997, 009816997
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-981-6997 | 50601 ( SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-981-6997
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-100-620-01 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-100-620-01 | D0272 | ROLLS-ROYCE DEUTSCHLAND LTD & CO KGDBA ROLLS-ROYCE DEUTSCHLAND |
Technical Data | NSN 2840-00-981-6997
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 28.030 INCHES NOMINAL |
| SPECIAL FEATURES | TAPERED OD; 3.67 MIN 3.675 MAX IN. LARGEST OD; FIRST END; EXT SPLINES; 19 TEETH; 30 DEG PRESSURE ANGLE; 1.248 MIN 1.25 MAX IN. OD; 1.1675 IN. NOM PITCH DIA; 1.88 MIN 2.44 MAX IN. LG SPLINES; 0.267 MIN 0.272 MAX IN. DISTANCE FROM FIRST END TO SPLINES; SCEOND END; EXT SPLINES; 13 TEETH; 30 DEG PRESSURE ABGLE; 1/162 MIN 1.167 MAX IN. OD; 1.0833 IN. NOM PITCH DIA; 2.12 MIN 2.26 MAX IN. LG SPLINES; 0.96 IN. NOM DISTANCE FROM SECOND END TO SPLINES; FIRST END; INT THD; 0.625 IN.-18 UNF 2B THD; 0.88 MIN 0.92 MAX IN. DP THD; 0.267 MIN 0.272 MAX IN. DISTANCE FROM FIRST END TO THD; SECOND END; INT THD; 0.625 IN.-18 UNF 2B THD; 0.65 MIN 0.69 MAX IN. DP THD COUNTERSUNK 60 DEG TO 0.72 IN. NOM DIA |