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At a glance
Measured figures
Maximum; T-41C · Maximum speed
Single source125 kn (144 mph, 232 km/h)[source]
T-41C · 1 × Continental IO-360-D Six-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Continental IO-360-D Six-cylinder air-cooled horizontally-opposed piston engine, 210 hp (160 kW)[source]
Tucano · 1 × Garrett TPE331 -12B turboprop 1,151 shp
Single source1 × Garrett TPE331 -12B turboprop , 858 kW (1,151 shp)[source]
Tucano · Endurance
Single source5 h 12 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Cessna T-41 Mescalero | Short Tucano |
|---|---|---|
| Type | Primary pilot trainer[source] | Trainer aircraft[source]Tucano |
| National origin | United States[source] | United Kingdom[source]Tucano |
| Manufacturer | Cessna[source] | Short Brothers[source]Tucano |
| Status | In service[source] | In limited service[source]Tucano |
| Primary users | United States Air Force United States Army Indonesian Air Force Turkish Air Force[source] | Royal Air Force (Retired) Kenya Air Force Kuwait Air Force[source]Tucano |
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | 160[source]Tucano |
| Manufactured | 1964–1996[source] | 1986–1995[source]Tucano |
| Introduction date | 1964[source] | 1989[source]Tucano |
| Developed from | Cessna 172 Cessna R172[source] | Embraer EMB 312 Tucano[source]Tucano |
| Capacity | three passengers[source] | — |
| Propellers | 2-bladed variable-pitch propeller[source] | 4-bladed Hartzell constant speed , fully feathering, aluminium , reversible-pitch propeller, 2.39 m (7 ft 10 in) diameter[source] |
| Alternative designation | T-41 Mescalero[source] | — |
| First flight | — | 14 February 1986[source]Tucano |
| Retired | — | 2019 (Royal Air Force)[source]Tucano |
| Airfoil | — | NACA 63 2 A-415 (root), 63A-212 (tip)[source] |
| Fuel capacity | — | 724 L (159 imp gal; 191 US gal)[source] |
| Stall speed | — | 80 km/h (50 mph, 43 kn) (flaps and gear down) (EAS)[source] |
| Never exceed speed | — | 518 km/h (322 mph, 280 kn) ( EAS )[source] |
| g limits | — | +7/-3.6[source] |
| Takeoff run to 15 m (50 ft) | — | 524 m (1,719 ft)[source] |
| Landing run from 15 m (50 ft) | — | 573 m (1,880 ft)[source] |
| Hardpoints | — | Provision for 1,000 lb (454 kg) of stores on four underwing hardpoints, but not on RAF Tucanos[source] |