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The 'CASA C-212 Aviocar' is a turboprop-powered STOL medium transport aircraft designed and built in Spain for civil and military use. C-212s have also been produced under licence in Indonesia by IPTN.

Contents

Design and development

Description

Incidents and Accidents

Variants

Series 100

Series 200

Series 300

Series 400

Operators

Specifications (Series 300M)

References

Related content

Design and development

During the late 1960s, the Spanish Air Force was still operating the already outdated Junkers Ju 52 and Douglas C-47. CASA developed the C-212 as a more modern alternative, with the first prototype flying on March 26 1971. In 1974, the Spanish Air Force decided to acquire the Aviocar to update its fleet.
When airlines took note of the type's success with the military, CASA developed a commercial version, the first examples of which were delivered in July 1975. In August 2006 a total of 30 CASA 212 aircraft (all variants) remain in airline service around the world.^[1]

Description

The Aviocar has a high-mounted wing, a boxy fuselage, and a conventional tail. The tricycle undercarriage is fixed.

Incidents and Accidents

The CASA 212 has been involved in 71 hull-loss incidents with a total of 499 fatalities.^{[2] [3]} This is a high occurrence, however the aircraft is generally not considered accident-prone as the cause of most crashes have been attributed to it being used in high-risk operations at low altitudes.
;October 26, 2006: Swedish Coast Guard CASA 212-200 (registration: SE-IVF/serial nr: KBV 585) crashed in the Falsterbo Canal during a surveillance mission, killing all four onboard.^{[4] [5]} Eye-witness accounts suggest that the accident was caused by one of the wings of the aircraft somehow detaching from the plane.^[6] 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 ^[7]. The investigation is ongoing.
;November 15, 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.^[8]

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 uprated engines 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 build under licence by IPTN.

Series 300

Standard production version from 1987 on. Winglets for improved performance.
;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

Slightly enlarged version first flying in 1997. US military designation is C-41.

Operators

★ (Abu Dhabi)

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★ (Myanmar)

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Specifications (Series 300M)

{{aircraft specifications
|plane or copter?= plane
|jet or prop?= prop
|ref={name of first source}
|crew= Two (pilot and co-pilot)
|capacity=Up to 20 troops, 12 litters, or 2,820 kg (6,217 lb) of cargo
|length main= 16.15 m
|length alt= 53 ft 0 in
|span main= 20.28 m
|span alt= 66 ft 7 in
|height main= 6.60 m
|height alt= 21 ft 8 in
|area main= 41 m²
|area alt= 441 ft²
|airfoil=
|empty weight main= 4,400 kg
|empty weight alt= 9,680 lb
|loaded weight main=
|loaded weight alt=
|useful load main=
|useful load alt=
|max takeoff weight main= 8,000 kg
|max takeoff weight alt= 17,600 lb
|more general=
|engine (prop)=Garrett AiResearch TPE-331-10R-513C
|type of prop= turboprop engines
|number of props=2
|power main= 690 kW
|power alt= 925 shp
|power original=
|max speed main= 370 km/h
|max speed alt= 200 kts, 230 mph
|cruise speed main=
|cruise speed alt=
|never exceed speed main=
|never exceed speed alt=
|stall speed main=
|stall speed alt=
|range main= 1,433 km
|range alt= 774 nm, 895 miles
|ceiling main= 7,925 m
|ceiling alt= 26,000 ft
|climb rate main= 497 m/min
|climb rate alt= 1,630 ft/min
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=

★ Up to 500 kg (1,100 lb) of weapons on two hardpoints. Typically, machine gun pods or rocket launchers.
|avionics=
}}

References

1. Flight International, 3-9 October 2006
2. Accident statistics for CASA 212 from the Aviation Safety Network
3. List of incidents in the Aviation Safety Network Database
4. Press release from the Swedish Coast Guard
5. Accident description, October 26, 2006 in the Aviation Safety Network Database
6. Four dead after coastguard plane crash, The Local, October 26, 2006.
7. Statens Haverikommission, (Swedish Accident Investigation Board)
8. SEMAR aircraft crashed in Mexican Gulf from the SEMAR

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