Part Details | AIRCRAFT PROPELLER
1610-00-721-7106 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: 43D50301, 43D50-301, 1610-00-721-7106, 00-721-7106, 1610007217106, 007217106
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 01, 1963 | 00-721-7106 | 30770 ( PROPELLER, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1610-00-721-7106
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 43D50-301 | 73030 | HAMILTON SUNDSTRAND CORPORATION |
Technical Data | NSN 1610-00-721-7106
| Characteristic | Specifications |
|---|---|
| PROPELLER TYPE | CONTROLLABLE PITCH |
| PITCH CONTROL TYPE | HYDRAULIC |
| CONTROL METHOD | AUTOMATIC |
| FEATHERING FEATURE | INCLUDED |
| REVERSIBILITY | NONREVERSIBLE |
| ROTATION DIRECTION | RIGHT-HAND |
| SPAN MAXIMUM DIAMETER | 11.000 FEET |
| BLADE QUANTITY | 3 |
| BLADE ANGLE RANGE IN DEG | M27.000/P89.000 |
| DESIGN CONSTANT STATION RADIUS | 42.0 INCHES |
| MATERIAL AND LOCATION | ALUMINUM ALLOY BLADES |