NSN 1610-00-277-1146

Part Details | AIRCRAFT PROPELLER

1610-00-277-1146 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: 23E5050564770, 23E50-505-6477-0, P100107, 23E505056477A1, 23E50-505-6477A1, 23E505056477A0, 23E50-505-6477A0, 23E505056477A, 23E50-505-6477A, 1610-00-277-1146, 00-277-1146, 1610002771146, 002771146

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
16JAN 01, 196300-277-114630770 ( PROPELLER, AIRCRAFT )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1610-00-277-1146
Part Number Cage Code Manufacturer
23E50-505-6477-073030HAMILTON SUNDSTRAND CORPORATION
P10010773030HAMILTON SUNDSTRAND CORPORATION
23E50-505-6477A173030HAMILTON SUNDSTRAND CORPORATION
23E50-505-6477A073030HAMILTON SUNDSTRAND CORPORATION
23E50-505-6477A73030HAMILTON SUNDSTRAND CORPORATION
Technical Data | NSN 1610-00-277-1146
Characteristic Specifications
PROPELLER TYPE CONTROLLABLE PITCH
PITCH CONTROL TYPE HYDRAULIC
FEATHERING FEATURE INCLUDED
REVERSIBILITY NONREVERSIBLE
ROTATION DIRECTION RIGHT-HAND
SPAN MAXIMUM DIAMETER11.500 FEET
BLADE QUANTITY3
BLADE ANGLE RANGE IN DEGP10.000/P90.000
DESIGN CONSTANT STATION RADIUS42.0 INCHES
MATERIAL AND LOCATION ALUMINUM ALLOY BLADES