Credit
US Air Force · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
T-41C · Length
Single source26 ft 11 in (8.20 m)[source]
Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | HESA Yasin |
|---|---|---|
| Type | Primary pilot trainer[source] | Military trainer aircraft / Jet trainer[source] |
| National origin | United States[source] | Iran[source] |
| Manufacturer | Cessna[source] | HESA[source] |
| Status | In service[source] | In production[source] |
12.25 m (40 ft 2 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]
2 × Owj turbojet engines (without afterburner version) thrust each
Single source2 × Owj turbojet engines (without afterburner version), 16 kN (3,600 lbf) thrust each[source]
T-41C · 880 ft/min (
Single source880 ft/min (4.5 m/s)[source]
with additional external fuel tanks
Single sourcewith internal fuel or
Single source90 minutes with internal fuel or 120 minutes with additional external fuel tanks[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] | — |
|---|
| Introduction date | 1964[source] | 11 March 2023[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] | — |
|---|
| Designer | — | Iran Aviation Industries Organization and Islamic Republic of Iran Air Force[source] |
|---|
| Primary user | — | IRIAF[source] |
|---|
| First flight | — | 2019[source] |
|---|
| Stall speed | — | 200 km/h (120 mph, 110 kn)[source] |
|---|
Maximum take-off; Max takeoff weight