Credit
US Air Force · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
T-41C · Length
Single source26 ft 11 in (8.20 m)[source]
G 115E · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Grob G 115 |
|---|---|---|
| Type | Primary pilot trainer[source] | Basic trainer[source] |
| National origin | United States[source] | — |
| Manufacturer | Cessna[source] | Grob Aircraft[source] |
| Status | In service[source] | active[source] |
| Primary users |
7.79 m (25 ft 7 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]
G 115E · 1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Air Force United States Army Indonesian Air Force Turkish Air Force[source]
Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | — |
|---|
| Manufactured | 1964–1996[source] | 1985–present[source] |
|---|
| Introduction date | 1964[source] | 1999[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| First flight | — | November 1985[source] |
|---|
| Fuel capacity | — | 143 L (31 imp gal; 38 US gal) usable[source] |
|---|
| Aspect ratio | — | 8.2:1[source] |
|---|
| Airfoil | — | Eppler 696[source] |
|---|
| Stall speed | — | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| Never exceed speed | — | 341 km/h (212 mph, 184 kn)[source] |
|---|
| g limits | — | + 6.0/ - 3.0[source] |
|---|
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |
|---|