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]
T-5 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Fuji T-5 |
|---|---|---|
| Type | Primary pilot trainer[source] | Basic trainer[source] |
| National origin | United States[source] | Japan[source] |
| Manufacturer | Cessna[source] | Fuji Heavy Industries[source] |
| Status | In service[source] | — |
| Primary users |
8.4 m (27 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]
T-5 · 1 × Allison Model 250-B17D turboprop
Single source1 × Allison Model 250-B17D turboprop , 261 kW (350 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] |
| — |
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | — |
|---|
| Manufactured | 1964–1996[source] | — |
|---|
| Introduction date | 1964[source] | 1988[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Fuji KM-2[source] |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 3-bladed constant-speed propeller[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
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| Primary user | — | Japan Maritime Self-Defense Force[source] |
|---|
| First flight | — | 28 June 1984[source] |
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| Airfoil | — | root: NACA 23016.5 ; tip: NACA 23012[source] |
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| Stall speed | — | 104 km/h (65 mph, 56 kn)[source] |
|---|
| Never exceed speed | — | 413 km/h (257 mph, 223 kn)[source] |
|---|