PAC, Pacific Aerospace CT/4 Airtrainer
Photo ©: George Canciani (photos at airliners.net)
CT/4 Airtrainer
Trainer
The Pacific Aerospace CT/4 Airtrainer is a single-engine two-seat aerobatic trainer aircraft produced by the New Zealand manufacturer AESL, Aero Engine Services Ltd, later Pacific Aerospace Corporation Ltd., today Pacific Aerospace Ltd., operated by the Royal Australian Air Force, Royal New Zealand Air Force, Royal Thai Air Force and the Republic of Singapore Air Force.
| Crew | 2 | |
| Propulsion | 1 Piston Engine | |
| Engine Model | Lycoming AEIO-540 L1B5 | |
| Engine Power | 224 kW | 300 hp |
| max. Cruise Speed | 272 km/h | 147 kts 169 mph |
| max. Speed (vne) | 383 km/h | 207 kts 238 mph |
| Service Ceiling | 5.547 m | 18.200 ft |
| Range | 991 km | 535 NM 616 mi. |
| Empty Weight | 807 kg | 1.780 lbs |
| max. Takeoff Weight | 1.180 kg | 2.601 lbs |
| Wing Span | 7,92 m | 26,0 ft |
| Wing Area | 12,0 m² | 129 ft² |
| Length | 7,16 m | 23,5 ft |
| Height | 2,59 m | 8,5 ft |
| First Flight | 23.02.1972 | |
| Production Status | in production | |
| Developed from | Victa Aircruiser | |
| other TCDS | CAA NZ A-10 | |
| Data for (Version) | Pacifc Aerospace CT/4E | |
| Variants | CT/4, CT/4A, CT/4B, CT/4E | |
| Extras | |
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