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At a glance
Measured figures
T-41C · Length
Single source26 ft 11 in (8.20 m)[source]
T-4 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Kawasaki T-4 |
|---|---|---|
| Type | Primary pilot trainer[source] | Intermediate trainer aircraft[source] |
| National origin | United States[source] | Japan[source] |
| Manufacturer | Cessna[source] | Kawasaki[source] |
| Status | In service[source] | Active[source] |
13.00 m (42 ft 8 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-4 · 2 × Ishikawajima-Harima F3 -IHI-30 turbofans thrust each
Single source2 × Ishikawajima-Harima F3 -IHI-30 turbofans , 16.32 kN (3,670 lbf) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| 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] | 208+[source] |
|---|
| Introduction date | 1964[source] | 1988[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | — |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| First flight | — | 29 July 1985[source] |
|---|
| Fuel capacity | — | 2,241 L (493 imp gal; 592 US gal) internal fuel[source] |
|---|
| Hardpoints | — | 5 (4 underwing and 1 under fuselage) for drop tanks, practice bombs and target towing equipment[source] |
|---|
| Aspect ratio | — | 4.7:1[source] |
|---|
| Stall speed | — | 167 km/h (104 mph, 90 kn)[source] |
|---|