Fairchild-Hiller FH-1100
Light Utility Helicopter
The Fairchild-Hiller FH-1100 is a light single-engine four-seat utility helicopter produced by the US-American manufacturer Fairchild-Hiller.
Propulsion | 1 Turboshaft Engine |
Engine Model | Allison 250-C18 |
Engine Power | 204 kW | 274 shp |
Speed | 204 km/h | 110 kts 127 mph |
Service Ceiling | 6.553 m | 21.500 ft |
Range | 693 km | 374 NM 430 mi. |
Empty Weight | 687 kg | 1.515 lbs |
max. Takeoff Weight | 1.247 kg | 2.750 lbs |
Rotor Blades (main/tail) | 2/2 |
Main Rotor Diameter | 10,79 m | 35 ft 5 in |
Tail Rotor Diameter | 1,83 m | 6 ft 0 in |
Rotor Disc Area | 91,4 m² | 984 ft² |
Length (Fuselage) | 9,08 m | 29 ft 9 in |
Length | 11,97 m | 39 ft 3 in |
Height | 2,83 m | 9 ft 3 in |
First Flight | 21.01.1963 |
Production Status | out of production |
Production Range | 1966-1973 |
Total Production | 254 |
ICAO Code | FH11 |
Data for (Version) | Fairchild-Hiller FH-1100 |