Enstrom F-28
Summary
Category | Training aircraft |
Origin country | πΊπΈ United States |
First flight | 12 November 1960 |
Year of introduction | 1965 |
Number produced | 32 units |
Description
The Enstrom F-28 is a military aircraft primarily designed for training and utility purposes. Developed by Enstrom Helicopter Corporation, it was first introduced in the late 1960s. The F-28 is known for its versatility and reliability, making it suitable for a range of missions including aerial observation, reconnaissance, and transport. It features a compact and lightweight design, equipped with a single engine and a three-bladed main rotor system. The aircraft has been employed by several military forces worldwide, proving its effectiveness in various operational environments. The Enstrom F-28 continues to serve as a dependable platform for military training and support missions.
Technical specifications
Version: F-28F Falcon | |
---|---|
Crew | 1 pilot |
Maximum speed | 180 km/h (112 mph) |
Height | 2.7 m (9.0 ft) |
Length | 8.9 m (29.3 ft) |
Service ceiling | 3658 m (12001 ft) |
Empty weight | 712 kg (1570 lbs) |
Max. takeoff weight | 1179 kg (2599 lbs) |
Climb rate | 7.37 m/s (24.2 ft/s) |
Powerplant | 1 Γ pistons engine Lycoming HIO-360-F1AD delivering 168 kW |
Current operating countries
Country | Units | ||
---|---|---|---|
Pakistan | 19 | ||
Peru | 11 (+4) | ||
Venezuela | 2 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.