Bell 214

Infobox Aircraft
name=Bell 214


caption= A Bell 214B
type=medium-lift helicopter
manufacturer=Bell Helicopter Textron
designer=
first flight=1970
introduced=1972
retired=
status=
primary user= Islamic Republic of Iran Army
more users=
produced=
number built=
unit cost=
developed from = Bell 204/205
variants with their own articles = Bell 214ST

The Bell 214 is a medium-lift helicopter derived from the ubiquitous UH-1 Huey series. The Bell 214ST shares the same model number, but is a larger, much-modified twin-engined derivative.

Design and development

The original development of the Model 214 was announced by Bell in 1970 under the name "Huey Plus". The first prototype was based on a Bell 205 airframe equipped with a Lycoming TS3 engine of 1900 shp.Apostolo, Giorgio: "The Illustrated Encyclopedia of Helicopters", page 54. Bonanza Books, New York, 1984. ISBN 0-517-439352]

The first 214A demonstration prototype followed and was evaluated in Iran during field exercises with the Iranian Armed Forces. The trial was judged successful and an order for 287 214A helicopters followed. The intention was that these aircraft would be constructed by Bell in their Dallas-Fort Worth facility and that a further 50 214As and 350 Bell 214ST helicopters would then be built in Iran. In the event 296 214A models and 39 214C models were delivered, before the Iranian Revolution ended the plans for Iranian production.

Similar in size and appearance to the Bell 205 and Bell 212, the Bell 214 uses a single much larger, 2930shp (2185kW) engine (Lycoming LTC4B-8) and upgraded rotor system giving it a high lifting capacity and good performance at high temperatures and high altitudes.Frawley, Gerard: "The International Directory of Military Aircraft", page 34. Aerospace Publications Pty Ltd, 2002. ISBN 1-875671-55-2] It can be identified by the single large exhaust duct and wide chord rotor blades without stabilizer bars.

Variants

* Bell 214 Huey Plus - The prototype 214 flew in 1970. Powered by one Lycoming T53-L-702 turboshaft (1900 shp/1415 kW).

* Bell 214A/C Isfahan - The 299 Bell 214As for the Imperial Iranian Army Aviation were built beginning in 1972, followed by 39 Bell 214Cs with a hoist and other search and rescue equipment for the Imperial Iranian Air Force.

* Bell 214B BigLifter - Bell offered the Bell 214B "BigLifter" for civil use. Receiving certification in 1976, it was built until 1981 with total production of 104.

* Bell 214B-1 - This version of the Bell Model 214B is limited to a maximum 12,500-lb (5670-kg) maximum weight. The external load is the same as the 214B. This was done for certification purposes in some countries where the limit for "heavy" aircraft was/is at 5700 kg. The only difference between the 214B and 214B-1 is the dataplate and the flight manual.

Operational history

An estimated 170 Bell 214A/Cs remain in Iranian service. The overhaul facility set up at the time of delivery, the Iran Helicopter Support & Renewal Company, is now able to do major rebuilds that could be considered manufacture of new machines.

Approximately 24 214Bs are still flying in commercial service where the hook lifting capacity of 8000 lb suits them for fire fighting, logging, and similar crane work. User countries are Canada (8), France (1), Korea (8), Norway (2), Singapore (3) United States (?).

Per the Type Certificate Data Sheet, Note 10., "Except for a difference in maximum weight, the Model 214B and 214B-1 are identical to each other.

Operators

Military operators

*BRU
*IRN
*PHI
*YEM

Civil operators

*McDerrmott Aviation, Australia - 3 [ cite web|url = http://www.mcdermottaviation.com.au/helicopters/our_fleet/|title = Helicopters, Our Fleet|accessdate = 2008-02-19|last = McDermott Aviation |authorlink = |year = 2007]
*Helitrans AS, Norway - 2 cite web|url = http://www.helitrans.no/cgi-bin/pg.cgi?id=EEEyVllEyltCilseLQ&tmpl=t_9 |title = Helikoptertyper (in Norwegian language)|accessdate = 2008-08-07|last = Helitrans|authorlink = |year = undated]

pecifications (214A)

aircraft specifications

plane or copter?=copter
jet or prop?=prop

ref=The International Directiory of Civil AircraftFrawley, Gerard: "The International Directory of Civil Aircraft, 2003-2004", page 44. Aerospace Publications Pty Ltd, 2003. ISBN 1-875671-58-7]

crew=2
capacity=3,880 lb including 14 troops, or 6 stretchers, or equivalent cargo
length main=48 ft 0 in
length alt=14.63 m)
span main=50 ft 0 in
span alt=15.24 m
height main=12 ft 10 in
height alt=3.90 m
area main=
area alt=
empty weight main=7,588 lb
empty weight alt=3,442 kg
loaded weight main=13,800 lb
loaded weight alt=6,260kg
max takeoff weight main=15,000 lb with slung load
max takeoff weight alt=6,805 kg

engine (prop)=Lycoming LTC4B-8D
type of prop=turboshaft
number of props=1
power main=2,930 shp
power alt=2,185 kW

max speed main=
max speed alt=
cruise speed main=140 knots
cruise speed alt=260 km/h, 161.5 mph
range main=255 mi
range alt=475 km
ceiling main=16,400 ft Density altitude
ceiling alt=5,000 m
climb rate main=
climb rate alt=
loading main=
loading alt=
power/mass main=
power/mass alt=
armament=

ee also

aircontent
related=
* Bell 214ST
* Bell 204/205
* Bell 212
* UH-1 Iroquois
* UH-1N Twin Huey

similar aircraft=
* AgustaWestland AW139

lists=
see also=

References

External links

* [http://www.aviastar.org/helicopters_eng/bell_214b.php Bell Model 214/214B Big Lifter on aviastar.org]