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C-212 Aviocar

Spanish light transport plane, renowned for its versatility, extensively used for surveillance, rescue, and paratrooping missions since the 1970s.

CASA C-212 Aviocar military transport aircraft in flight
Origin country
🇪🇸 Spain
First flight
1971Mar 26
Introduced
1974
Produced
483units
Avg unit price
$7 million
Active worldwide
120+8 on order
CASA C-212 Aviocar military transport aircraft side profile drawing
Side profile · CASA C-212 Aviocar · length 16.2 m
Technical SpecificationsVersion: C-212-300M
Crew2 pilots
Length16.2 m (53.1 ft)
Wingspan20.3 m (66.5 ft)
Height6.3 m (20.7 ft)
Wing area41 m² (441.3 sqft)
Empty weight3,780 kg (8,333 lbs)
Max. takeoff weight7,700 kg (16,976 lbs)
Powerplant2 × turboprops Garrett TPE331-10R-513C 671 kW each
PerformanceVersion: C-212-300M
Maximum speed370 km/h (230 mph)
Operational range835 km (519 mi)
Service ceiling7,925 m (26,001 ft)
Climb rate8.3 m/s (27.2 ft/s)
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C-212 Aviocar vs
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Description

The C-212 was developed during the 1960s by Construcciones Aeronáuticas SA (CASA) in response to the Spanish Air Force's need to replace its aging transport aircraft fleet. The aircraft was designed to perform a variety of military roles, including passenger transport, air medical services, and paratrooper duties, while also being suitable for civil operators. The first prototype of the C-212, a twin-engine 18-seat transport, conducted its maiden flight on 26 March 1971. In 1974, the Spanish Air Force purchased the C-212, which was then named Aviocar, to modernize its fleet. CASA subsequently developed a dedicated commercial version due to interest from several airlines. In 1997, the improved -400 model was introduced, featuring a glass cockpit and more powerful Honeywell TPE331 engines. Production of the type at the Seville facility continued for 40 years, with 485 aircraft produced there.

Design

The CASA C-212 Aviocar is designed as a turboprop-powered STOL-capable cargo aircraft, characterized by its high-mounted wing, box-like fuselage, and conventional tail. It is specifically engineered to operate in austere conditions for extended durations without requiring substantial ground support. Its design incorporates features that provide STOL performance, such as rugged landing gear equipped with low-pressure tires, enabling operation from unpaved fields and in hot and high conditions. To enhance simplicity, the aircraft is fitted with non-retractable tricycle undercarriage. Depending on configuration, the cabin can accommodate between 21 and 28 passengers; in a paratroop configuration, it can accommodate up to 24 paratroopers plus a jumpmaster on foldable sidewall seats, while a mixed configuration allows for up to ten soldiers and a single vehicle. The absence of a pressurized fuselage restricts the C-212 to relatively low-altitude flights below 10,000 feet (3,000 meters), making it suitable for short-range regional airline services.

Armament

The CASA C-212 can be outfitted with up to 500 kg (1,102 lb) of weaponry on two hardpoints. This capacity typically accommodates machine gun pods or rocket launchers, enabling the aircraft to support tactical missions such as close air support or armed reconnaissance.

Operational History

By 2013, 290 C-212s were flying in 40 countries, with Indonesia as the primary operator with 70 aircraft. The C-212 has been widely used both as a commuter airliner and as a military platform, employed by charter and short-haul aviation companies and numerous national air forces, and is commonly used in transport, surveillance, and search and rescue roles. The U.S. Army Special Operations Command has operated the C-212, designated C-41A, for troop infiltration and exfiltration, supply drops, and airborne operations. Additional aircraft were operated by private military contractor Blackwater during the Iraq War and the War in Afghanistan for supply drops to US ground forces in remote areas. Australian airline Skytraders has supported Australia’s scientific research assets across Antarctica and the Southern Ocean with the type.

Variants

Main Variants:

  • C-212A: The original military production version, also known as the C-212-5, C-212-5 series 100M, and designated as T-12B and D-3A (for medevac aircraft) by the Spanish Air Force.

  • C-212C: The initial civil version of the C-212, aimed at commercial operators.

  • C-212 series 200M: This military version, designated T-12D in Spanish service and Tp 89 for the Swedish Air Force, has also been adapted into specialized ASW and maritime patrol aircraft.

  • C-212 series 300 airliner: A 26-seat regional airliner configuration, expanding the C-212's role in civilian transport.

  • C-212-400: An upgraded variant featuring more powerful engines, an increased payload, and enhanced avionics relocated to the nose.

Frequently Asked Questions

What type of aircraft is the C-212 Aviocar?
The CASA C-212 Aviocar is a military transport aircraft aircraft developed by CASA and entered service in 1974.
What is the maximum speed of the C-212 Aviocar?
The CASA C-212 Aviocar has a maximum speed of 370 km/h (229 mph).
What is the range of the C-212 Aviocar?
The CASA C-212 Aviocar has an operational range of 835 km (518 miles). This range can vary based on payload, altitude, and mission profile.
When did the C-212 Aviocar first fly?
The CASA C-212 Aviocar made its first flight on March 26, 1971. It entered operational service in 1974.
How many C-212 Aviocar have been built?
Approximately 483 units of the CASA C-212 Aviocar have been produced since it entered service in 1974.
Which countries operate the C-212 Aviocar?
The CASA C-212 Aviocar is operated by 22 countries with approximately 120 aircraft in active service. The largest operators include Indonesia, Zimbabwe, and Colombia.
How much does a C-212 Aviocar cost?
The CASA C-212 Aviocar has an estimated unit cost of approximately $7.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the C-212 Aviocar?
The CASA C-212 Aviocar has a service ceiling of 7,925 meters (26,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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