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]
Tétras B · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Humbert Tétras |
|---|---|---|
| Crew | one[source] | — |
| Type | Primary pilot trainer[source] | Two seat ultralight or kit build[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Humbert Aviation[source] |
6.50 m (21 ft 4 in)[source]
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]
Tétras B · 1 × Rotax 912 UL flat four
Single source1 × Rotax 912 UL flat four , 59.6 kW (79.9 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] | c.150 by 2010[source] |
|---|
| Manufactured | 1964–1996[source] | 1992-present[source] |
|---|
| Introduction date | 1964[source] | 1994[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 2-bladed DUC FC composite, 1.75 m (5 ft 9 in) diameter[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Designer | — | Humbert Aviation[source] |
|---|
| First flight | — | c.1992[source] |
|---|
| Airfoil | — | NACA 23012[source] |
|---|
| Fuel capacity | — | 60 L (15.9 USgal, 13.2 Impgal) standard. Can be increased to 85 L (22.5 USgal, 18.7 Impgal) outside France.[source] |
|---|
| Stall speed | — | 55 km/h (34 mph, 30 kn) flaps down[source] |
|---|
| g limits | — | +4/-2[source] |
|---|
Maximum take-off; Tétras B · where permitted
Single source