Part Details | AIRCRAFT PROPELLER
1610-00-640-8321 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: 278102, 278-102, 1610-00-640-8321, 00-640-8321, 1610006408321, 006408321
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 01, 1963 | 00-640-8321 | 30770 ( PROPELLER, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1610-00-640-8321
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 278-102 | 70898 | BEECHCRAFT CORPORATIONDBA TEXTRON AVIATION |
Technical Data | NSN 1610-00-640-8321
| 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 | 7.000 FEET |
| BLADE QUANTITY | 2 |
| BLADE ANGLE RANGE IN DEG | M12.500/P33.000 |
| DESIGN CONSTANT STATION RADIUS | 33.0 INCHES |
| MATERIAL AND LOCATION | ALUMINUM ALLOY BLADES |