CASA C-212-CB Aviocar (Series 100)

CASA

ICAOC212IATACS2
CASA C-212-CB Aviocar (Series 100) aircraft
CASACASA C-212 Aviocar

Photograph of the CASA C-212 Aviocar family. No photograph on Wikimedia Commons identifies this variant specifically.

Photo: AlbertoDV · CC0 · Modified

About

The first Aviocar, at 6,500 kg on TPE331-5 engines and limited to 19 seats by its emergency exits. Every later model on the certificate is 1,200 kg heavier and seats 28. The cruise speed, range, ceiling, climb rate, wingspan, length, height and take-off distance are EUROCONTROL's figures for the C212 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A318

MTOW (Maximum Takeoff Weight)

6,500kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

6,250kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

6,000kg
0
25k
53k

Capacitycompared to Airbus A318

Passenger Capacity

19passengers
0
100
132

14% of A318 maximum capacity

Crew

Total
2
Cockpit
2

Dimensions

Length

16.2m

Wingspan

20.3m

Height

6.6m

Engine Specifications

Engine Count

2×

Engine Model

Garrett TPE331-5-251C turboprop

Production & History

Production Status

Out of production

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