Aircraft Sales and Leasing

CASA 212-100 Aircraft For Sale

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CASA 212-100


The CASA C-212-100 Aviocar is a light Cargo transport that was designed to operate in areas lacking in infrastructure and unpaved runways. It has a high-wing configuration and fixed landing gear, is fitted with twin turboprop engines, and has excellent Short Take Off and Landing (STOL) capability.

The cargo compartment can accommodate 18 passengers and their luggage, or 4,409 pounds (2,100kg) of diversified cargo, including road vehicles. For aero-medical evacuations, 12 litters and seats for two attendants can be mounted. A rear-loading ramp enables different logistic transport tasks to be carried out. It can be opened while on the ground, to load and unload, or in flight for the airdropping of general cargo, food, or survival equipment for example.

The CASA 212-100 features quick and easy rear ramp loading, which is ideal for large, cumbersome cargo. The cargo may be loaded into the 24 ft. cargo area using roller systems. In this case, it is not necessary to break down the freight. The customer can ship the cargo on pallets. LD2 and LD3 containers can also be loaded.

CASA 212-100 Advantages


Specifications

Dimensions, External:

Wing span 19.00 meters (62 ft 4 in)
Wing chord: at root 2.50 meters (8 ft 2½ in)
 At tip 1.50 meters (4 ft 11 in)
Wing aspect ratio 9
Length overall 15.16 meters (44 ft 9 in)
Height overall 6.68 meters (21 ft 11 in)
Tail plane span 7.40 meters (24 ft 3¼ in)
Wheel track 3.10 meters (10 ft 2 in)
Wheelbase 5.55 meters (18 ft 2½ in)
Propeller diameter 2.69 meters (8 ft 10 in)
Distance between propeller centers 5.30 meters (17 ft 4¾ in)
Passenger door (port, aft):  
Max height 1.58 meters (5 ft 2¼ in)
Max width 0.70 meters (2 ft 3½ in)
Crew and servicing door (port, fwd):  
Max height 1.10 meters (3 ft 7¼ in)
Max width 0.60 meters (1 ft 11{5/8} in)
Rear-loading door: Max length 3.66 meters (12 ft 0 in)
Max width 1.70 meters (5 ft 7 in)
Max height 1.80 meters (5 ft 10¾ in)

Dimensions, Internal:

Cabin (between flight deck and rear-loading door):


    Length
6.50 meters (21 ft 4 in)
Max width 2.10 meters (6 ft 10¾ in)
Max height 1.80 meters (5 ft 10¾ in)
Floor area 10.50 m2 (113.0 sq ft)
Volume 22.00 m3 (776.9 cu ft)

Areas


Wings, gross
40.0 m2 (430.56 sq ft)
Ailerons (total) 2.45 m2 (26.37 sq ft)
Trailing-edge flaps (total) 7.38 m2 (79.44 sq ft)
Fin 4.25 m2 (45.75 sq ft)
Rudder, incl. tab 2.02 m2 (31.74 sq ft)
Tail plane 7.36 m2 (79.22 sq ft)
Elevators, incl. tabs 4.36 m2 (46.93 sq ft)

Weights and Loadings

Manufacturer's weight empty 3,700 kg (8,157 lb)
Weight empty, equipped 3,905 kg (8,609 lb)
Max payload 2,100 kg (4,630 lb)
Fuel load 1,600 kg (3,527 lb)
Max T-O weight 6,500 kg (14,330 lb)
Max zero-fuel weight 6,000 kg (13,227 lb)
Max landing weight 6,250 kg (13,780 lb)
Max wing loading 162.5 kg/m2 (33.3 lb/sq ft)
Max power loading 5.81 kg/kW (9.55 lb/shp)

Performance

(At max T-O weight except where indicated)

Never-exceed speed 253 Kts. (471 km/h; 292 mph) EAS
Max level speed at 3,660 meters (12,000 ft)  
  194 Kts. (359 km/h; 223 mph)
Econ cruising speed at 3,660 meters (12,000 ft) 148 Kts. (275 km/h; 171 mph)
Stalling speed: flaps up 74 Kts (137 km/h; 85.5 mph)
Flaps down 61.5 Kt (113 km/h; 70.5 mph)
Max rate of climb at S/L 518 meters (1,700 ft)/min
Max rate of climb at S/L, one engine out 93 meters (305 ft)/min
Service ceiling 8,140 meters (26,700 ft)
Service ceiling, one engine out 4,115 meters (13,500 ft)
T-O run 350 meters (1,148 ft)
T-O run to 15 meters (50 ft) 484 meters (1,588 ft)
Landing run from 15 meters (50 ft) 518 meters (1,700 ft)
Landing run 331 meters (1,085 ft)
Range at 3,050 meters (10,000 ft):  
With max fuel and 1,045 kg (2,303 lb) payload 949 n miles (1,760 km; 1,093 miles)
 With max payload 258 n miles (480 km; 298 miles)
Maximum Fuel 548 gals (20 unusable)

CASA 212-100 tail diagram

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