CASA C-212-200 REFERENCE

Weight(MTOW) 17637 lbs
Emty Weight 9688 lbs
Max landing weight 16 424 lbs
Power(2)Garret TPE331-10R-513C(900 shp)(671 kW)
Propeller four-bladed Dowty Rotol R334/482-F/13 reversible propellers.



Maximum Speed 200 kt(370 kph)
Maximum cruise speed 191 kt(354 kph)
Cruise speed 145 IAS(162 kt TAS)(300 kph)
Stall speed 78 kt
Range 1446 nm
Service ceiling 26.000 ft
Consum 88 gal/hour
Payload 6217 lbs
Accomodation two (flight deck)maximum of 26 passengers
Dimensions span 66ft 6 1\/2 in (20.28m)\s height 21ft 7 3\/4 in (6.60m)\s length 52ft 11 3\/4 in (16.15m)
Wing span 19m(62 ft 4in)
Wing area 430.6 ft2


Runway requirements:
Take-off STOL: 384 m / 1 260 ft
Landing STOL: 285 m / 935 ft.
Normal TO: 610m / 2000 ft.
Normal Landing: 462 m / 1 516 ft.

Max rate of climb at SL:
Normal: 1 630 fpm
One engine out: 312 fpm.


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.

Cruise

150 IAS(162 TAS) at 5000 ft

145 IAS(162 TAS) at 7000 ft