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]
Bulldog Series 120 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Scottish Aviation Bulldog |
|---|---|---|
| Crew | one[source] | 2, model 101 has 3[source] |
| Type | Primary pilot trainer[source] | Basic trainer with aerobatic capability[source]Bulldog |
| National origin | United States[source] | United Kingdom[source] |
| Manufacturer | Cessna[source] |
23 ft 3.06 in (7.0881 m)[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]
Bulldog Series 120 · 1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine, 200 hp (150 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Beagle Aircraft / Scottish Aviation[source]Bulldog |
| Status | In service[source] | Active[source]Bulldog |
|---|
| 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] | 328[source]Bulldog |
|---|
| Manufactured | 1964–1996[source] | 1969–1982[source]Bulldog |
|---|
| Introduction date | 1964[source] | 1971[source]Bulldog |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Beagle Pup[source]Bulldog |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 2-bladed Hartzell constant speed propeller[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Primary user | — | Royal Air Force[source]Bulldog |
|---|
| First flight | — | 19 May 1969[source]Bulldog |
|---|
| Aspect ratio | — | 8.4[source] |
|---|
| Airfoil | — | NACA 63 2 615[source] |
|---|
| Stall speed | — | 54 kn (62 mph, 100 km/h)[source] |
|---|
| Never exceed speed | — | 185 kn (213 mph, 343 km/h)[source] |
|---|
| g limits | — | + 6g - 3g, with no longer than 15 seconds sustained inverted flight.[source] |
|---|
| Wing loading | — | 18.2 lb/sq ft (89 kg/m 2 )[source] |
|---|