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]
Fajr F.3 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Fajr F.3 |
|---|---|---|
| Type | Primary pilot trainer[source] | Training aircraft[source] |
| National origin | United States[source] | Iran[source] |
| Manufacturer | Cessna[source] | Fajr Aviation & Composites Industry[source] |
| Status | In service[source] | Active service |
8.07 m (26 ft 6 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]
Fajr F.3 · 1 × Lycoming AEIO-540-L1B5 6-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-540-L1B5 6-cylinder air-cooled horizontally-opposed piston engine, 201 kW (270 hp)[source]
Fajr F.3 · Endurance
Single source6 hours 15 minutes[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] | 2001—[source] |
|---|
| Introduction date | 1964[source] | Iran[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] | 3 pax[source] |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 3-bladed constant-speed propeller[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Primary user | — | Iranian Air Force[source] |
|---|
| First flight | — | 1995[source] |
|---|
| Airfoil | — | Horstmann-Quast HQ-42E[source] |
|---|
| Fuel capacity | — | 212 L (56 US gal; 47 imp gal)[source] |
|---|
| Cabin Width | — | 1.25 m (4 ft 1 in)[source] |
|---|
| Stall speed | — | 104 km/h (65 mph, 56 kn)[source] |
|---|
| Never exceed speed | — | 370 km/h (230 mph, 200 kn)[source] |
|---|
| Take-off run | — | 310 m (1,017 ft)[source] |
|---|
| Landing run | — | 370 m (1,214 ft)[source] |
|---|