Part Details | AIRCRAFT PROPELLER
1610-00-945-1418 A propeller designed to provide thrust for a fixed or tilt wing aircraft. It may be of solid or built-up construction; constant or controllable speed type; adjustable, fixed or variable pitch design with reversing and/or feathering capabilities during aircraft operation. Variable pitch propellers have integral facilities for changing the pitch angle of the blades while aircraft is in flight. Excludes HUB-BLADE ASSEMBLY, PROPELLER, AIRCRAFT. See also TEST CLUB.
Alternate Parts: 23E505057149A0, 23E50-505-7149A0, 1610-00-945-1418, 00-945-1418, 1610009451418, 009451418
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | MAR 04, 1966 | 00-945-1418 | 30770 ( PROPELLER, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1610-00-945-1418
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 23E50-505-7149A0 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
Technical Data | NSN 1610-00-945-1418
| Characteristic | Specifications |
|---|---|
| PROPELLER TYPE | CONTROLLABLE PITCH |
| PITCH CONTROL TYPE | HYDRAULIC |
| CONTROL METHOD | AUTOMATIC |
| FEATHERING FEATURE | NOT INCLUDED |
| REVERSIBILITY | REVERSIBLE |
| ROTATION DIRECTION | RIGHT-HAND |
| SPAN MAXIMUM DIAMETER | 11.500 FEET |
| BLADE QUANTITY | 3 |
| BLADE ANGLE RANGE IN DEG | M16.000/P88.000 |
| DESIGN CONSTANT STATION RADIUS | 42.0 INCHES |
| ICE CONTROL METHOD | ANTI-ICING |
| ICE CONTROL MEDIA | HYDRAULIC FLUID |
| MATERIAL AND LOCATION | ALUMINUM OVERALL |