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-7 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Fuji T-7 |
|---|---|---|
| Type | Primary pilot trainer[source] | Primary/Basic Trainer[source] |
| National origin | United States[source] | Japan[source] |
| Manufacturer | Cessna[source] | Fuji Heavy Industries[source] |
| Status | In service[source] | Active[source] |
8.59 m (28 ft 2 in)[source]
T-41C · Range
Single source626 nmi (720 mi, 1,159 km)[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-7 · 1 × Rolls-Royce 250-B17F turboprop engine
Single source1 × Rolls-Royce 250-B17F turboprop engine, 336 kW (451 hp)[source]
T-41C · Service ceiling
Single source17,000 ft (5,200 m)[source]
T-41C · 880 ft/min (
Single source880 ft/min (4.5 m/s)[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] | 49[source] |
|---|
| Manufactured | 1964–1996[source] | 2002-present[source] |
|---|
| Introduction date | 1964[source] | — |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Fuji T-3[source] |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 3-bladed constant-speed propeller, 2.12 m (6 ft 11 in) diameter[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Airfoil | — | root: NACA 23016.5 ; tip: NACA 23012[source] |
|---|
| Stall speed | — | 104 km/h (65 mph, 56 kn) flaps and gear down[source] |
|---|
| Wing loading | — | 96.1 kg/m 2 (19.7 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.2114 kW/kg (0.1286 hp/lb)[source] |
|---|
| Take-off distance to 15 m (49 ft) | — | 608 m (1,995 ft)[source] |
|---|
| Landing distance from 15 m (49 ft) | — | 566 m (1,857 ft)[source] |
|---|