The UH-1D
The UH-1D offers improved performance with the addition of composite main
rotor and tail rotor blades. Along with the Structural Life Extension Program
(SLEP), these aircraft are configured to impress
Highlights of the UH-1D
Structural Life Extension Program (SLEP)
Composite Main & Tail Rotor Blades
T53-L-13B Engine
Cargo Door with Bubble Window
All Major Components with 50% or greater Time Life Remaining
13 Passenger Seating
– Crew: 1-4
– Capacity: 12-15 passengers or 6 stretchers
– Length: 57 ft 1 in (17.4 m)
– Rotor Diameter: 48 ft (14.6 m)
– Height: 14 ft 5 in (4.4 m)
– Empty Weight: 5,215 lbs (2,365 kg)
– Max Takeoff Weight: 9,500 lbs (4,309 kg)
– Engine: Lycoming T53-L-11 turboshaft
– Maximum Speed: 127 mph (204 km/h)
– Range: 293 miles (471 km)
– Service Ceiling: 19,390 ft (5,910 m)
Roles and Missions:
1. Troop Transport
2. Medical Evacuation (MEDEVAC)
3. Cargo Transport
4. Search and Rescue (SAR)
5. Close Air Support (optional)
1. The UH-1D is a versatile utility helicopter with a capacity of 12-15 passengers or 6 stretchers.
2. It features a Lycoming T53-L-11 turboshaft engine, producing 1,100 shp.
3. The helicopter has a maximum speed of 127 mph and a range of 293 miles.
4. The UH-1D was extensively used during the Vietnam War for troop transport, medical evacuation, cargo transport, search and rescue, and close air support.
5. Its service record includes military and civilian operations worldwide.
6. The UH-1D’s design and performance set the standard for utility helicopters.