Part Details | AIRCRAFT PROPELLER
1610-01-540-4740 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: HCD4N2AD9512A, HC-D4N2A/D9512A, 968.29.12.001, 1610-01-540-4740, 01-540-4740, 1610015404740, 015404740
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | MAY 19, 2006 | 01-540-4740 | 30770 ( PROPELLER, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1610-01-540-4740
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HC-D4N2A/D9512A | 24692 | HARTZELL PROPELLER INC. |
| 968.29.12.001 | S4080 | PILATUS AIRCRAFT LTD |
Technical Data | NSN 1610-01-540-4740
| Characteristic | Specifications |
|---|---|
| PROPELLER TYPE | CONTROLLABLE PITCH |
| PITCH CONTROL TYPE | MECHANICAL |
| CONTROL METHOD | AUTOMATIC |
| FEATHERING FEATURE | INCLUDED |
| REVERSIBILITY | NONREVERSIBLE |
| ROTATION DIRECTION | RIGHT-HAND |
| SPAN MAXIMUM DIAMETER | 7.916 FEET |
| BLADE QUANTITY | 4 |
| MATERIAL AND LOCATION | ALUMINUM HUB |