Casa-takeoff

Specifications

CASA 212 Specifications
Flight Crew
2 pilots
Scientific support personnel Maximum 15 persons/ typical 5 scientists during research missions depending on additional payload and range requirements
Engines
Two flat rated 925 shp Garrett TPE 331-12JR series
Power supply DC (primary)
Power supply AC (primary)
Power available in cabin
2 generators 28V DC 300 Amps continuous.
3 static inverters 26/115 V AC/400Hz/350VA
3 sockets 28V DC/ 10A
Aircraft length
Aircraft height
Wingspan
Cabin length
Cabin width
Cabin height
Cabin capacity
Cargo bay capacity (on ramp)
16 m
6.7 m
20 m
5.9 m
1.8 m
1.8 m
22 cubic metres
5.3 cubic metres
Operating limitations
Standard Restricted Restricted On skis
Max take-off weight
Max landing weight
Empty weight (no pax seats)Max fuel load Max cruising speed
7700kgs
7450kgs
4990kgs
2330kgs
165 kts (305 km/h)
8100kgs
8100kgs
4990kgs
2330kgs
165 kts (305 km/h)
8470kg
8100kgs
5334kgs
2330kgs
155KIAS (287 km/h)

 

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