Bell 212 Manuals
Crew 1 / 2 Passengers 13 - 14 Propulsion 2 Turboshaft Engines Engine Model Pratt & Whitney Canada PT6T-3D Twin-Pac Engine Power (each) 1342 kW 1800 shp Speed 230 km/h 124 kts 143 mph Service Ceiling 5.304 m 17.400 ft Range 450 km 243 NM 280 mi. Empty Weight 2.786 kg 6.142 lbs max. Takeoff Weight 5.080 kg 11.200 lbs Rotor Blades (main/tail) 2/2 Main Rotor Diameter 14,69 m 48 ft 2 in Tail Rotor Diameter 2,59 m 8 ft 6 in Rotor Disc Area 169,5 m² 1824 ft² Length (Fuselage) 12,92 m 42 ft 5 in Length 17,46 m 57 ft 3 in Height 4,53 m 14 ft 10 in First Flight April 1969 Production Status out of production Total Production ca. 900 Developed from Bell 205 ICAO Code B212 UH1 FAA TCDS H4SW Data for (Version) Bell 212 Variants Bell UH-1N Iroquois, HH-1N, CH-135 Twin Huey, Agusta-Bell AB212. Photo-ID: 5717 © 2011-07-28 Bell Helicopter 212 Reg.: D-HHPP c/n: 30801 Fly Out special c/s Photo-ID: 6390 © 2013-02-09 Bell Helicopter 212 Reg.: H6K-1/19 c/n: 31692 Photo-ID: 2754 © 2009-09-23 Agusta-Bell AB212-AM Reg.: MM81148 c/n: 5805 Photo-ID: 2755 © 2009-09-23 Agusta-Bell AB212-AM Reg.: MM81148 c/n: 5805 Photo-ID: 5926 © 2012-06-13 Bell Helicopter UH-1N Iroquois Reg.: 159198 c/n: 31674 Photo-ID: 5927 © 2012-06-13 Bell Helicopter UH-1N Iroquois Reg.: 159198 c/n: 31674. Flugzeuginfo.net The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft.
Bell 212 Pictures
Bell 212 Single Engine Conversion
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