Bell UH-1 Iroquois - Specifications (UH-1D)

Specifications (UH-1D)

General characteristics

• Crew: 1-4
• Capacity: 3,880 lb including 14 troops, or 6 stretchers, or equivalent cargo
• Length: 57 ft 1 in (17.40 m) with rotors
• Width: 8 ft 7 in (2.62 m) (Fuselage)
• Height: 14 ft 5 in (4.39 m)
• Empty weight: 5,215 lb (2,365 kg)
• Gross weight: 9,040 lb (4,100 kg)
• Max takeoff weight: 9,500 lb (4,309 kg)
• Powerplant: 1 × Lycoming T53-L-11 turboshaft, 1,100 shp (820 kW)
• Main rotor diameter: 48 ft 0 in (14.63 m)

Performance

• Maximum speed: 135 mph (217 km/h; 117 kn)
• Cruise speed: 125 mph (109 kn; 201 km/h)
• Range: 315 mi (274 nmi; 507 km)
• Service ceiling: 19,390 ft (5,910 m) (Dependent on environmental factors such as weight, outside temp., etc)
• Rate of climb: 1,755 ft/min (8.92 m/s)
• Power/mass: 0.15 hp/lb (0.25 kW/kg)

Armament

Variable, but may include a combination of:

• 2 x 7.62 mm M60 machine gun, or 2 7.62 mm GAU-17/A machine gun
• 2 x 7-round or 19-round 2.75 in (70 mm) rocket pods
• 2 x 7.62 mm Rheinmetall MG3 (German Army and German Luftwaffe)
• 2 x .303 Browning Mk II (Rhodesian, twin machine guns mounted on port side)

For information on US armament systems see: