Credit
US Air Force · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
T-41C · Length
Single source26 ft 11 in (8.20 m)[source]
Tucano Replica · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Flying Legend Tucano Replica |
|---|---|---|
| Crew | one[source] | one[source] |
| Type | Primary pilot trainer[source] | Light-sport aircraft[source] |
| National origin | United States[source] | Italy[source] |
| Manufacturer | Cessna[source] | Flying Legend |
7.10 m (23 ft 4 in)[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 Replica · 1 × Rotax 915 iS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 915 iS four cylinder, liquid and air-cooled, four stroke aircraft engine , 104 kW (141 hp)[source]
T-41C · Service ceiling
Single source17,000 ft (5,200 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In production[source] |
|---|
| Primary users | United States Air Force United States Army Indonesian Air Force Turkish Air Force[source] | — |
|---|
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | — |
|---|
| Manufactured | 1964–1996[source] | 2011-present[source] |
|---|
| Introduction date | 1964[source] | 2011[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] | one passenger[source] |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 4-bladed composite[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Fuel capacity | — | 120 litres (26 imp gal; 32 US gal)[source] |
|---|
| Stall speed | — | 75 km/h (47 mph, 40 kn) flaps up[source] |
|---|
| Never exceed speed | — | 330 km/h (210 mph, 178 kn)[source] |
|---|
| g limits | — | +6.0/-3.0[source] |
|---|
| Wing loading | — | 75 kg/m 2 (15 lb/sq ft)[source] |
|---|