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bagera3005 — Bell 222 pan am
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#bell #helicopter #222 #aircraft
Published: 2019-11-03 04:06:12 +0000 UTC; Views: 1749; Favourites: 29; Downloads: 19
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Description
Model 222 222B 222U 230Announced 1974 1982 1982 1990
First Flight August 13, 1976 1982 1983 August 12, 1991
Certified December 1979 August 1982 April 1983 March 1992
Delivered 1980 1982 1983 November 1992
Seats Front: pilot + one. Main: four–six (depending on seat types)
Maximum ten (pilot and nine passengers)[11]
Height 11 ft 8 in (3.56 m) 12 ft 2 in (3.71 m) 11 ft 8 in (3.56 m)
Fuselage length 42 ft 2 in (12.85 m)[12] 42 ft 11 in (12.78 m) 42 ft 3 in (12.88 m)
Rotor diameter 39 ft 9 in (12.12 m)[13] 42 ft (12.80 m)
Length overall 49 ft 6 in (15.1 m) 50 ft 3 in (15.32 m)
Engine (2x) Lycoming LTS-101-650C-3 Lycoming LTS-101-750C Rolls-Royce 250-C30G/2
Power (2x) 620 shp (462 kW)[13] 684 shp (510 kW)[12] 700 hp (520 kW)
Max speed 133 kn (153 mph; 246 km/h)[13]
(cruise) 135 kt
(155 mph, 250 km/h) 140 kt
(161 mph, 260 km/h)
Climb rate 1,600 ft/min (8.1 m/s)[13] 1,730 ft/min (8.79 m/s) ~1,600 ft/min (8.13 m/s)
Service ceiling 20,000 ft (6,100 m)[13] 15,800 ft (4,816 m) 15,500 ft (4,724 m)
Hover ceiling 4,200 ft (1,300 m)[13] 10,300 ft (3,139 m) 12,400 ft (3,780 m)
Fuel capacity 188+48 US gal (710+182 L) 188+122 US gal (710+460 L) 188+ US gal (710+ L)
Range 282 nmi (325 mi; 522 km)[13] 378 nmi
(434 mi, 700 km) 486 nmi
(559 mi, 900 km) 378 nmi
(434 mi, 700 km)
Empty weight 4,860 lb (2,200 kg)[13] 4,577 lb (2,076 kg) 4,537 lb (2,058 kg) 5,097 lb (2,312 kg)
Maximum takeoff weight 8,100 lb (3,670 kg)[13]
(external load) 8,250 lb (3,742 kg) 8,400 lb (3,810 kg)
