The Aircraft is depicted in the colours of the Indonesian Navy, Squadron 600.
The CASA C-212-100 Aviocar is a light military 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 TakeOff and Landing (STOL) capability.
The first prototype flew in 1971
The cargo compartment can accommodate 18 passengers and their luggage, or 16 fully-equipped paratroopers, or 4,409 pounds (2,000kg) of diversified cargo, including road vehicles. For aeromedical 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 cargo, survival equipment or paratroops.
This aircraft is based on a previous model of Johan Crous
Specifications (Military configuration):
Powerplant:Two Garret single shaft 671kW/900shp TPE-331-10R Turboprops
with four-bladed Dowty Rotol R334/482-F/13 reversible propellers.
Capable of delivering 925 shp in case of one engine take-off.
Length: 16015m / 52ft 11¾ inc
WingSpan:20.28m / 66ft 6½ inc
MTOW:8000 kg / 17 637 lb.
Max landing weight: 7 450 kg / 16 424 lb.
Max Speed: 200kt / 370km/h / 230 mph
Max cruising speed: 191 kt / 354 km/h / 220 mph.
Economical cruising Speed: 162 kt / 300 km/h / 186 mph.
Stall speed at MTOW: 78 kt
Max Payload: 2 820 kg / 6 217 lb.
Range:
Max fuel & 2 120 kg (4 674 lb) payload : 907 nm / 1 682 km / 1 045 miles.
Max payload: 450 nm / 835 km / 519 miles.
With additional Fuel & 1 192 kg (2 628 lb) payload:1 446 nm /
2 680 km / 1 665 miles.
[All three with 45 min reserve].
Additional fuel in pylon underwing tanks: 1 000 kg / 1 764 lb.
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.
Service Ceiling: 7 925m / 26 000 ft. (unpressurized).
Max rate of climb at SL:
Normal: 1 630 fpm
One engine out: 312 fpm.
DISCLAIMER AND USE
The aircraft, panel and the xml gauges are freeware and you may use them only in freeware panels and aircraft. You may not unbundle the cab file without my permission. If you want to do any changes to any of the gauges, you must get my permission to do so. Please just keep any improvements freeware.
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