CT/4E Airtrainer

Pacific Aerospace Corporation

Приборная доска:

фотографии с сайта www.aerospace.co.nz

Fuel

Usable fuel = 44 Imp Gal (199 litres),
Range = 520 nm (836 km),
Fuel Consumption (cruise) = 14 gph (65 litres/hr) ,
Fuel feed system comprises two integral wing tanks and associated valves and filters,
Fuel is gravity fed from each tank into a common collector tank.
Performance

Assume: ISA, Nil Wind, 2 Pilots

Take off ground roll (SL) = 600 ft (182 m),
Landing run = 553 ft (250 m),
Rate of climb = 1830 ft/min,
Stall speed (full flap) = 45 kts (83 km/hr).
The manoeuvre flight load factor limits are:

Flaps UP:
Aerobatic Flight = +6.0 G - 3.0 G,
Flaps DOWN:
Normal Flight = +2.0 G - 0.0 G,
Wing Loading = 20.2 lbs./ft sq,
Power Loading = 8.7 lbs/hp (at maximum all up weight).
Leading Particulars

Propeller Ground Clearance = 8" - 28" (200-710 mm),
Weight (empty typical) = 1780 lbs (807 kg),
Maximum Gross Weight = 2600 lbs (1180 kg),
Maximum Landing Gross Weight = 2600 lbs (1180 kg),
Wing span = 26.0 ft (7.92 m),
Length = 23.48 ft (7.16 m),
Height = 8.50 ft (2.59 m),
Tailplane span = 11.83 ft (3.6 m),
Wheel base = 5.45 ft (1.66 m),
Wheel track = 9.75 ft (2.97 m).
Airspeed

Stalling Speed Flaps Up = 60 kts (111 km/hr),
Stalling Speed Full Flap = 45 kts (83 km/hr),
Stalling Speed Half Flap = 52 kts (96 km/hr),
Manoeuvring Speed Flaps Up = 144 kts (267 km/hr),
Manoeuvring Speed Full Flap = 63 kts (117 km/hr),
Manoeuvring Speed Half Flap = 74 kts (137 km/hr),
Cruising Speed = 150 kts (278 km/hr),
Maximum = 209 kts (388 km/hr).
Weights

Two Crew - Full Fuel:

Empty Aircraft = 1750 lbs (793 kg),
Maximum Fuel = 322 lbs (150 kg),
Crew (2) = 340 lbs (154 kg),
TOTAL = 2447 lbs (1109 kg).

Сайт разработчика: www.aerospace.co.nz