PAC CT/4 Civil Aircraft Model Details

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General Information of PAC CT/4

Developed From : Victa Aircruiser

First Flight : 26352

Manufacturer : Pacific Aerospace

Primary Users : Royal New Zealand Air Force; Royal Thai Air Force; Royal Australian Air Force; BAE Flight Training Australia

Role : Primary trainer

General characteristics of PAC CT/4

Aspect Ratio : 5.2:1

Crew : 2 : student, instructor

Empty Weight : 807 kg (1,780 lb)

Height : 2.59 m (8 ft 6 in)

Length : 7.16 m (23 ft 2 in)

Max Takeoff Weight : 1,179 kg (2,600 lb)

Powerplant : 1 × Lycoming AEIO-540-L1B5 flat-six piston engine, 224 kw (300 hp)

Wing Area : 11.98 m2 (129 ft2)

Wingspan : 7.92 m (26 ft 0 in)

Performance of PAC CT/4

Cruise Speed : 282 km/h (152 knots, 175 mph) at 2,590 m (8,500 ft) (75% power)

Maximum Speed : 302 km/h (163 knots, 188 mph) at sea level

Never Exceed Speed : 387 km/h (209 knots, 240 mph)

Range : 963 km (520 nmi, 599 mi)(max fuel, 75% power)

Rate Of Climb : 9.3 m/s (1,830 ft/min)

Service Ceiling : 5,550 m (18,200 ft)

Stall Speed : 82 km/h (44 knots, 51 mph) (flaps down)

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