Bell Helicopter Bell 212 / Twin Two-Twelve (UH-1N)

Photo ©: Karsten Palt

Bell 212 / Twin Two-Twelve (UH-1N)

Medium Utility Helicopter

Crew	1 / 2
Passengers	13 - 14

Propulsion	1 Turboshaft Engine
Engine Model	Pratt & Whitney Canada PT6T-3 Twin-Pac
Engine Power	962 kW	1290 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	2/2
Main Rotor Diameter	14,69 m	48,2 ft
Tail Rotor Diameter	2,59 m	8,5 ft
Rotor Disc Area	169,5 m²	1824 ft²
Length (Fuselage)	12,92 m	42,4 ft
Length	17,46 m	57,3 ft
Height	4,53 m	14,9 ft

First Flight	April 1969
Production Status	out of production
Total Production	ca. 900
Developed from	Bell 205

ICAO Code	B212
FAA TCDS	H4SW
Data for (Version)	Bell 212

Remarks
The Engine PT6T Twin-Pac is a twinned turboshaft.

Weblinks	Extras
Bell Helicopter Textron	print view

[Photo-ID: 2754] © Karsten Palt 2009-09-23
	Agusta-Bell AB212-AM Italian Air Force Reg.: MM81148 c/n: 5805
NATO Tigermeet 2009 [Kleine Brogel (EBBL)]

[Photo-ID: 2755] © Karsten Palt 2009-09-23
	Agusta-Bell AB212-AM Italian Air Force Reg.: MM81148 c/n: 5805
NATO Tigermeet 2009 [Kleine Brogel (EBBL)]