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Measured figures
T-41C · Length
Single source26 ft 11 in (8.20 m)[source]
Configuration
| Specification | Cessna T-41 Mescalero | IRIAF Parastu-14 |
|---|---|---|
| Crew | one[source] | — |
| Type | Primary pilot trainer[source] | Trainer aircraft[source] |
| National origin | United States[source] | Iran[source] |
| Manufacturer | Cessna[source] | HESA[source] |
T-41C · Wingspan
Single source35 ft 10 in (10.92 m)[source]
T-41C · Height
Single source8 ft 10 in (2.69 m)[source]
Maximum; T-41C · Maximum speed
Single source125 kn (144 mph, 232 km/h)[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-41C · Wing area
Single source159 sq ft (14.8 m 2 )[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.
| Status |
|---|
In service[source] |
Active service[source] |
| 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] | September 2013 (Unveiled)[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Beechcraft 33 Bonanza[source] |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | — |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Designer | — | Islamic Republic of Iran Air Force[source] |
|---|
| Primary user | — | Islamic Republic of Iran Air Force[source] |
|---|