Soong KH-4
Jump to navigation
Jump to search
KH-4 | |
---|---|
![]() | |
Role
|
Utility helicopter |
National origin
|
Monsilva |
Manufacturer
|
Soong Aerospace Company |
First flight
|
August 1962 |
Number built
|
211 |
The Soong KH-4 is a light utility helicopter produced in Monsilva in the 1960s and 70s. A total of 211 KH-4s were built, the vast majority of these were bought by civil operators, although some were purchased by the Monsilvan Air Force.
Specifications
General characteristics
- Crew: 1
- Capacity: 3 passengers
- Length: 13.30 m (43 ft 8 in) (overall length), 9.93 m (32 ft 7 in) (fuselage length)
- Height: 2.84 m (9 ft 4 in)
- Empty weight: 816 kg (1,799 lb)
- Max takeoff weight: 1,293 kg (2,851 lb)
- Main rotor diameter: 11.32 m (37 ft 2 in)
- Main rotor area: 100.6 m2 (1,083 sq ft)
Performance
- Maximum speed: 169 km/h (105 mph, 91 kn)
- Cruise speed: 140 km/h (87 mph, 76 kn)
- Range: 400 km (250 mi, 220 nmi)
- Endurance: 4 hr 6 min
- Service ceiling: 5,640 m (18,500 ft)
- Rate of climb: 4.3 m/s (850 ft/min)