Boeing Chinook HC.5, ZH 902, 18 Sqn, RAF
ZH 902 at Norwich Int. Airport (NWI) for refuelling. The helicopter later departed to RAF Odiham (ODH).
Model: Chinook HC.5
Manufacturer: Boeing-Vertol
Year built: 1998
Serial number: M.4481
Registration number: ZH 902
Owner: Royal Air Force
Operator: 18 Squadron
Crew: Pilot, co-pilot, 1 or 2 air loadmasters
Capacity: 55 fully equipped troops
Length with rotors operating: 98 ft. 10.5 in. (30.14 m)
Fuselage length: 50 ft. 9 in. (15.46 m)
Fuselage height: 18 ft. 7.5 in. (5.68 m)
Fuselage width: 12 ft. 5 in. (3.78 m)
Rotor diameter: 60 ft. (18.29 m)
Empty weight: 22,450 lb. (10,183 kg)
MTOW: 50,000 lb. (22,680 kg)
Useful load: 24,000 lb. (10,886 kg)
Sling load capacity: 26,000 lb. (11,793 kg)
Fuel capacity: 861 gal. (3,914 litres)
Engines: 2 x Lycoming T55-GA-714A turboshaft
Engine output: 2 x 4,777 hp (3,562 kW)
Max speed: 159 knots (183 mph - 294 km/h)
Rate of climb: 1,980 ft/min. (10.1 m/s)
Service ceiling: 18,500 ft. (5,639 m)
Mission radius: 200 nm (230 miles - 370 km)
Armament:
2 x M134 7.62 mm miniguns
1 x M60 7.62 mm machine gun
Also registered:
N2064W, Boeing test registration
Boeing Chinook HC.5, ZH 902, 18 Sqn, RAF
ZH 902 at Norwich Int. Airport (NWI) for refuelling. The helicopter later departed to RAF Odiham (ODH).
Model: Chinook HC.5
Manufacturer: Boeing-Vertol
Year built: 1998
Serial number: M.4481
Registration number: ZH 902
Owner: Royal Air Force
Operator: 18 Squadron
Crew: Pilot, co-pilot, 1 or 2 air loadmasters
Capacity: 55 fully equipped troops
Length with rotors operating: 98 ft. 10.5 in. (30.14 m)
Fuselage length: 50 ft. 9 in. (15.46 m)
Fuselage height: 18 ft. 7.5 in. (5.68 m)
Fuselage width: 12 ft. 5 in. (3.78 m)
Rotor diameter: 60 ft. (18.29 m)
Empty weight: 22,450 lb. (10,183 kg)
MTOW: 50,000 lb. (22,680 kg)
Useful load: 24,000 lb. (10,886 kg)
Sling load capacity: 26,000 lb. (11,793 kg)
Fuel capacity: 861 gal. (3,914 litres)
Engines: 2 x Lycoming T55-GA-714A turboshaft
Engine output: 2 x 4,777 hp (3,562 kW)
Max speed: 159 knots (183 mph - 294 km/h)
Rate of climb: 1,980 ft/min. (10.1 m/s)
Service ceiling: 18,500 ft. (5,639 m)
Mission radius: 200 nm (230 miles - 370 km)
Armament:
2 x M134 7.62 mm miniguns
1 x M60 7.62 mm machine gun
Also registered:
N2064W, Boeing test registration