CASA C-212 Aviocar
The CASA C-212 Aviocar is a turboprop-powered STOL medium cargo aircraft designed and built by CASA in Spain for civil and military use.
C-212 Aviocar | |
---|---|
A CASA C-212 of the Spanish Air Force | |
Role | Medium STOL military transport aircraft |
Manufacturer | Construcciones Aeronáuticas SA EADS CASA Indonesian Aerospace |
First flight | 26 March 1971 |
Introduction | May 1974 |
Status | In production Indonesia |
Primary users | Indonesia (70) United States (37) Spain (26)[1] |
Produced | 1971–2012 |
Number built | 483[2] + >100 (IPTN) |
Unit cost |
$5.2-8 million (2006)[3] |
Developed into | Indonesian Aerospace N-219 |
Development
During the late 1960s, the Spanish Air Force was still operating a number of outdated piston-engined transports, including the three-engined Junkers Ju 52 and two-engined Douglas C-47. In order to meet the Spanish Air Force's needs to modernise its transport force, CASA proposed the C-212, a twin engined 18 seat transport aircraft that would be capable of fulfilling a variety of military roles, including passenger transport, ambulance aircraft and paratroop carrier, while also being suitable for civil use.[4] The first prototype flew on 26 March 1971. In 1974, the Spanish Air Force decided to acquire the Aviocar to update its fleet.
Airlines took note of the type's success with the military, so CASA developed a commercial version, the first examples of which were delivered in July 1975. In August 2006 a total of 30 CASA C-212 aircraft (all variants) remain in airline service around the world.[5] The -400 was introduced in 1997 with a glass cockpit and more powerful engines.[6]
In 2010, Airbus Military said it could no longer afford to produce the C212 in Europe and after production in Seville slowed to four in two years, the last C-212 produced in Spain was delivered in late December 2012 to the Vietnam Marine Police. Over 42 years, 477 aircraft have been produced for 92 operators.[6]
Indonesian production
IPTN and Nurtanio assembled the type under license at Bandung, Indonesia, during the 1970s and 1980s.[6]
In mid-2011 Airbus agreed to collaborate with their successor PTDI, which holds a license to sell the C212 in Asia.[7] PTDI built the NC-212-200 and the -400 upgrade, with new digital avionics and autopilot, and a cabin for up to 28 passengers.[6] In 2014, PTDI stopped producing the -400 series and moved production to the improved NC-212i model.[8]
Design
The C-212 has a high-mounted wing, a boxy fuselage, and a conventional tail. The tricycle undercarriage is non-retractable. It has space for 21–28 passengers depending on configuration. Since the C-212 does not have a pressurized fuselage, it is limited to relatively low-flight-level airline usage (below 10,000 ft (3,000 m) MSL). It is thus ideal for short legs and regional airline service.
Operational history
The C-212 is used as a transport, for rain-making, surveillance or search and rescue, and in 2013, 290 C-212s were flying in 40 countries with the most in Indonesia with 70.[9] It has seen especially wide employment as a commuter airliner and a military aircraft, with its operators including numerous charter and short-haul aviation companies and several national air forces. The C-212 is also in the service of the United States Army Special Operations Command with the designation C-41A, which utilizes the aircraft for troop infiltration and ex-filtration, supply drops, and airborne operations.[10] Due to the presence of a rear ramp, the C-212 has also gained popularity among skydivers and smokejumpers.[11][12]
Variants
Series 100
- C-212A
- Original military production version. Also known as C-212-5, C-212-5 series 100M, and by the Spanish Air Force as the T-12B and D-3A (for medevac aircraft), 129 built.
- C-212AV
- VIP transport version, T-12C.
- C-212B
- Six pre-production C-212As converted for photo-reconnaissance missions, TR-12A.
- C-212C
- Original civil version
- C-212D
- Two pre-production C-212As converted for use as navigational trainers, TE-12B.
- NC-212-100
- Manufactured under licence in Indonesia since 1976, IPTN producing 28 NC-212-100s before switching to NC-212-200.
Series 200
Stretched version with updated engines (Honeywell TPE331-10R-511C or −512C, rated at 900 shp (671 kW) each), introduced in 1979. The CASA C-212-200 is also a popular skydiving aircraft, known for its large capacity, fast climb, and large tailgate exit ramp.
- C-212 series 200M
- Military version known as T-12D in Spanish service and Tp 89 for the Swedish Air Force. Specialised ASW and maritime patrol aircraft have been built from this version.
- NC-212-200
- C-212-200 built under licence by IPTN.
- NC-212-200 MPA
- C-212-200 built under licence by IPTN, Designed as Maritime Patrol Aircraft
Series 300
Standard production version from 1987 on. Engines were Honeywell TPE331-10R-513C, also rated at 900 shp (670 kW) continuous (925 shp maximum). The propellers were changed from four-bladed Hartzell composite blade propellers to four-bladed Dowty-Rotol all-metal propellers. Winglets and a larger vertical stabilizer area provide improved performance, and the addition of a nose baggage compartment gives the nose a more streamlined look than the Series 200. Various systems have been incrementally upgraded, including the addition of an integrated autopilot system.
- C-212-M series 300 (Series 300M)
- Military version.
- C-212 series 300 airliner
- 26 seat regional airliner.
- C-212 series 300 utility
- 23 seat civil utility version.
- C-212 series 300P
- Civil utility version with Pratt & Whitney Canada PT6A-65 engines
Series 400
Upgraded version with 925 shp (690 kW) TPE331-12JR-701C engines, increased payload and upgraded avionics moved from under the floor to the nose. First flew 4 April 1997, replacing Series 300 in production from 1998.[13] The C-212-400 received Spanish certification in 1998. Between 2004 and 2008, production jigs and fixtures for the NC212-400 were relocated to Bandung from San Pablo, Spain and PTDI became the sole manufacturer of the NC212 family. In 2014, NC212-200 and NC212-400 production ended and production moved to the improved NC212i version.[8]
NC-212i
Improved version of -400 series, using two Honeywell TPE331-12JR-701C turboprop engines, with maximum output of 970 hp (723 kW). The rotor is four-bladed Dowty Rotol R334/4-82-F/13 constant speed propeller with a 2.75 m (110-inch) in diameter.
Operators
Civil operators
- B&H Airlines – former operator[15]
- Air Miami[14]
- Bar Harbor Airlines[14]
- Bighorn Airways[14][17]
- Boston-Maine Airways – operating code share service as Pan Am Express on behalf of Pan Am
- Chaparral Airlines – operating code share service as American Eagle on behalf of American Airlines
- Coastal Airlines[14]
- Evergreen International Airlines[14]
- Executive Airlines – operating code share service as American Eagle in the Caribbean from San Juan, PR (SJU) on behalf of American Airlines[18]
- Fischer Brothers Aviation – operating code share service as Northwest Airlink on behalf of Northwest Airlines and also operating code share service as Allegheny Commuter
- Gulf Air – operating code share service as Air Florida Commuter on behalf of Air Florida
- Inland Empire Airways[14]
- Jet Express – operating code share service as Trans World Express (TWE) on behalf of Trans World Airlines (TWA)
- Mountain Air Cargo[14]
- North American Airlines[14]
- Oceanair
- Presidential Airways – Owned and operated by private military contractor Blackwater during the Iraq War and the War in Afghanistan to provide supply drops to US troops in remote areas during the conflicts. During the conflict, the planes were piloted by former pilots from 160th "Night Stalkers" Special Operations Regiment.[19]
- Prinair
- U.S. Drug Enforcement Administration[14]
- Bering Air
- Ryan Air Cargo
Military operators
|
|
Specifications (Series 400)
Data from Jane's All The World's Aircraft 1989–90[51][52]
General characteristics
- Crew: 2
- Capacity: 26 passengers / 25 paratroops / 2,820 kg (6,217 lb) military payload / 2,700 kg (5,952 lb) cargo payload
- Length: 16.15 m (53 ft 0 in)
- Wingspan: 20.28 m (66 ft 6 in)
- Height: 6.6 m (21 ft 8 in)
- Wing area: 41 m2 (440 sq ft)
- Aspect ratio: 10
- Airfoil: NACA 653-218[53]
- Empty weight: 3,780 kg (8,333 lb)
- Max takeoff weight: 8,000 kg (17,637 lb) military
- 7,700 kg (16,976 lb) standard
- Max Landing weight: 7,450 kg (16,424 lb)
- Fuel capacity: 2,040 l (540 US gal; 450 imp gal) / 1,600 kg (3,527 lb) internal
- and
- 1,000 l (260 US gal; 220 imp gal) auxiliary fuel tanks in the cabin
- or
- 2x 750 l (200 US gal; 160 imp gal) auxiliary fuel tanks in the cabin
- and/or
- 2x 500 l (130 US gal; 110 imp gal) underwing auxiliary fuel tanks
- and
- Powerplant: 2 × Garrett AiResearch TPE331-10R-513C turboprop engines, 671 kW (900 hp) each
- Propellers: 4-bladed Dowty Rotol R-334/4-82-F/13, 2.74 m (9 ft 0 in) diameter constant-speed fully-feathering reversible-pitch propellers
Performance
- Maximum speed: 370 km/h (230 mph, 200 kn) VMO (maximum operating speed) at MTOW
- Cruise speed: 354 km/h (220 mph, 191 kn) (max cruise) at 3,050 m (10,007 ft)
- Economical cruise speed: 300 km/h (190 mph; 160 kn) at 3,050 m (10,007 ft)
- Stall speed: 145 km/h (90 mph, 78 kn) in take-off configuration
- Range: 835 km (519 mi, 451 nmi) with full military payload
- Ferry range: 2,680 km (1,670 mi, 1,450 nmi) with maximum fuel and 1,192 kg (2,628 lb) payload
- Service ceiling: 7,925 m (26,001 ft)
- 3,380 m (11,089 ft) on one engine
- Rate of climb: 8.283 m/s (1,630.5 ft/min)
- Take-off distance to 15 m (49 ft): 610 m (2,001 ft) (MIL-7700C)
- Landing distance from 15 m (49 ft): 462 m (1,516 ft) (MIL-7700C)
- Landing run: 285 m (935 ft) (MIL-7700C)
Armament
- Up to 500 kg (1,102 lb) of weapons on two hardpoints. Typically, machine gun pods or rocket launchers.
Variant | -CB | -CC/CD/CE/CF/DF | -DE |
---|---|---|---|
Approved | 22 Feb 1977 | 16 May 1980-30 Mar 1989 | 1 Oct 1991 |
2× Turboprop | Garrett TPE331-5 | TPE331-10 | P&WC PT6A-65B |
Takeoff power | 559 kW (750 hp) | 671 kW (900 hp) | 746 kW (1,000 hp) |
Propellers | 4-bladed variable pitch | ||
Manufacturer | Hartzell | McCauley | |
Propeller Diameter | 273 cm (107.5 in) | 279 cm (110 in) | 269 cm (106 in) |
Max. operating | 200 kn (370 km/h) IAS | ||
Min. control | 78 kn (144 km/h) IAS | 85 kn (157 km/h) IAS (-CC/CD) 88 kn (163 km/h) IAS (-CE/CF) 76 kn (141 km/h) IAS (-DF) |
76 kn (141 km/h) IAS |
Chord | 86.22 in (219.0 cm) | ||
MTOW | 6,500 kg (14,332 lb) | 7,700 kg (16,976 lb) | |
Flight crew | Two pilots | ||
Max. passengers | 19 | 28 | |
Usable fuel | 2,000 L (528 US gal) | ||
Ceiling | 7,600 m (25,000 ft) |
See also
Aircraft of comparable role, configuration and era
- Antonov An-28
- DHC-6 Twin Otter
- Dornier Do 228
- Evektor EV-55 Outback
- Harbin Y-12
- IAI Arava
- Short Skyvan
Incidents and accidents
As of September 2011, CASA C-212s have been involved in 71 hull-loss incidents with a total of 558 fatalities.[55][56]
- 2 January 1984
- a Royal Jordanian Air Force CASA 212-A3 Aviocar 100 crashed near Al Qatrana/Jordan due to mechanical problems. All 13 people on board the plane were killed.[57]
- 4 March 1987
- Northwest Airlink Flight 2268 crashed while landing at Detroit Metropolitan Wayne County Airport in Romulus, Michigan. Nine of the 19 passengers and crew on board were killed.
- 8 May 1987
- American Eagle Flight 5452 crashed while landing in Puerto Rico, killing two.
- 1 February 1988
- A Panamanian Air Force C-212 crashed into a mountain near the Panamese-Colombian border, killing all 16 people on board.
- 2 August 1988
- Operated by Geoterrex of Ottawa, Ontario, Canada, the aircraft crashed on approach to Reykjavik, Iceland with the loss of all 3 people on board. The cause was, "the crew lost control of the aircraft most probably because of large fluctuations in the power output of the right engine caused by the shift of an incorrectly installed speeder spring in the right propeller governor."[58]
- 1 December 1989
- A United States Army C-212-200 crashed into the Patuxent River while trying to land at the Naval Air Test Center, Patuxent River, Maryland, killing all five people on board.[59]
- 16 January 1990
- SANSA Flight 32 crashed into the Cerro Cedral, a mountain in Costa Rica shortly after takeoff from Juan Santamaria International Airport in San Jose. All 20 passengers and 3 crew on board died in the crash.
- 24 January 1990
- A Venezuelan Navy C-212 crashed into a mountain due to poor weather, killing all 24 people on board.
- 27 March 1990
- An Angolan government C-212 was shot down by UNITA rebels near Kuito, killing all 25 people on board.
- 7 June 1992
- American Eagle Flight 5456, a CASA C-212 flying from Fernando Luis Ribas Dominicci Airport in San Juan, Puerto Rico crashed short of the runway in Mayagüez, killing both crew members and all three passengers.[60] The investigation led to the discontinuation of use of the C-212 by American Eagle.
- 8 March 1994
- A Spanish Air Force CASA C-212 was hit in the tail by a Serbian SA-7 missile east of Rijeka when ferrying UNPROFOR personnel from Sarajevo. The aircraft was part of the Ala 37 deployed in Vicenza, Italy. A Croatian MiG-21 had been shot down over nearby Gvozd (then Vrginmost) on 14 September 1993. The tail control surfaces were damaged, the left engine failed and four passengers were injured by splinters. The crew managed to land the aircraft at Rijeka airport. Spanish technicians were able to repair the damage and have the aircraft back in service in 48 hours.[61][62][63][64]
- 17 June 1995
- An Angolan Air Force C-212 carrying members of a local football club crashed while on approach to Catumbela Airport, killing 48 of the 53 people aboard.[65]
- 27 November 2004
- "Blackwater 61" Presidential Airways CASA C-212-200 (registration: N960BW / serial nr: 231) was contracted by the U.S. Department of Defense to supply American forces deployed in remote areas of Afghanistan. The aircraft entered a box canyon and struck the 14,650-foot (4,470 m) level of Baba Mountain, which has a peak elevation of 16,739 feet (5,102 m). The flight was about 25 nm north of the typical route between Bagram and Farah.[66][67][68][69]
- 22 February 2005
- An Indonesian National Police C-212 received engine trouble during landing, causing it to crash into the sea. Of the 18 police officers on board, 15 were killed.
- 26 October 2006
- Swedish Coast Guard CASA C-212-200 (registration: SE-IVF/serial nr: KBV 585) crashed in the Falsterbo Canal during a surveillance mission, killing all four on board.[70][71] Eyewitness accounts suggest that the accident was caused by one of the wings of the aircraft somehow detaching.[72] The preliminary report from the Swedish Accident Investigation Board suggests that the right wing detached due to a fatigue crack which had developed in the load-bearing structure in the wing.[73]
- 15 November 2006
- Mexican Navy CASA 212-200 Maritime Patrol (serial AMP-114) crashed in the sea in Campeche coast over the Mexican Gulf during a surveillance mission, all crew managed to survive, due to a smooth maneuver, reasons of the accident still unknown.[74]
- 26 June 2008
- Indonesian Military CASA C-212 was flying from the capital to Bogor, carrying 12 military personnel and six civilians, and was due to test a digital mapping camera, but it disappeared in the Salak Mountain region, about 90 km (56 mi) south of Jakarta. An air force spokesman said it was assumed it had crashed.[75]
- 9 October 2009
- Uruguayan Air Force CASA C-212 FAU-531,[76] being operated as part of the United Nations Stabilization Mission in Haiti crashed west of Fonds-Verettes killing all 11 on board.[77]
- 19 June 2010
- a Cameroon Aero Service CASA C212 chartered by Sundance Resources crashed in dense jungle after departing Cameroon for Congo, killing all 11 people on board, including Australian mining magnate Ken Talbot and Sundance personnel, Chairman Geoff Wedlock, Chief Executive Officer Don Lewis, company secretary John Carr-Gregg and non-executive directors John Jones and Craig Oliver. At the time of the accident Talbot was a director of Sundance and its largest shareholder.[78][79][80]
- 12 February 2011
- Sabang Merauke Raya Air Charter CASA C-212, PK-ZAI, carrying five crew, crashed after takeoff from Batam, Indonesia, during a test flight following engine maintenance. All five crew members were killed.[81]
- 1 April 2011
- FUGRO Aviation Canada Limited CASA C-212, C-FDKM, carrying three crew, crashed while attempting to land at Saskatoon Airport, Saskatoon, Saskatchewan, Canada, after declaring an emergency with an engine failure. The aircraft crashed on Wanuskewin Drive in Saskatoon and hit a concrete barrier, resulting in one person being killed and two injured.[82]
- 2 September 2011
- A Chilean Air Force CASA C-212, carrying 21 people, crashed 500 miles from Chile's Pacific coastline in the Juan Fernández Islands, with no survivors. Felipe Camiroaga, a most popular Chilean TV presenter, was one of those on board the aircraft. Also on board was businessman Felipe Cubillos, who had been working on post-earthquake reconstruction efforts.[83]
- 29 September 2011
- An Indonesian Aerospace CASA C-212, registration PK-TLF, built in 1989, carrying 18 people (14 passengers, three crew and the pilot) on a flight between Medan, North Sumatra and Kutacane, Aceh operated by Nusantara Buana Air crashed into Gunung Kapur, a 1,600-metre-high (5,200 ft) mountain in the Bukit Barisan mountain range, a 10 km walk from the village of Bukit Lawang in Bohorok district Gunung Leuser National Park. There were no survivors. The accident occurred between 07.28 and 08.05 local time about 58 km (36 miles) northwest of Medan, North Sumatra.[84][85][86]
- 16 June 2016
- A CASA C-212-400 operated by Vietnam People's Air Force from Gia Lam Airport en route to the Gulf of Tonkin went missing and was presumed crashed during a search for a downed Su-30MK2 and its pilots a few days before. It was reported that the crash site was located 44 nautical miles south-southwest of Bach Long Vi Island. As of 18 June 2016, some of the debris was found, but there was no sign of the crew. The Vietnam Coast Guard and the Navy claimed that the airframe and the aircraft's black box has been found 15 nautical miles southwest of Bach Long Vi and only 5 nm from the Vietnamese-Chinese border on the gulf. All 9 crew members were lost[87]
- 9 February 2017
- A Botswana Defence Force CASA C-212 crashed in the general area of Thebephatshwa village in the evening, minutes after leaving the Thebephatshwa Air Base. All 3 people on board died in the crash. The aircraft was on its way to the capital, Gaborone, which is 90 km away.[88]
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- Bibliography
- Barrie, Douglas and Jenny Pite. "World's Air Forces". Flight International, Vol. 146, No. 4435, 24– 30 August 1994, pp. 29–64.
- Eastwood, Tony and John Roach. Turbo Prop Airliner Production List. London: The Aviation Hobby Shop, 1990. ISBN 0-907178-32-4.
- Hoyle, Craig. "Directory: World Air Forces". Flight International, Vol. 178, No. 5257, 14– 20 December 2010, pp. 26–53.
- Hoyle, Craig. "World Air Forces Directory". Flight International, Vol. 180, No. 5321, 13– 19 December 2011, pp. 26–52.
- Hoyle, Craig. "World Air Forces Directory". Flight International, Vol. 182, No. 5370, 11– 17 December 2012. pp. 40–64. ISSN 0015-3710.
- Hoyle, Craig. "World Air Forces Directory". Flight International, Vol. 188, No. 5517, 8–14 December 2015. pp. 26–53.
- Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.
- Jackson, Paul. "Royal Jordanian Air Force: Air Power at Three-continent Crossroads". Air International, Vol. 33, No. 5, November 1987, pp. 215–223. ISSN 0306-5634.
- Simpson, Rod. "CASA C-212 Aviocar: A Plane For All Seasons". Air International, Vol. 68, No. 1, January 2005, pp. 32–38. ISSN 0306-5634.
- Taylor, John W. R. Jane's All The World's Aircraft 1988–89. Coulsdon, UK: Jane's Defence Data, 1988. ISBN 0-7106-0867-5.
- "World's Air Forces". Flight International, Vol. 144, No. 4397, November 1993, pp. 41–76. 24–30.
External links
Wikimedia Commons has media related to CASA C-212. |
- Official website
- "Type Certificate Data Sheet No. A43EU, C-212" (PDF). Federal Aviation Administration. 8 January 2015.