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-1A · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Raytheon T-1 Jayhawk |
|---|---|---|
| Type | Primary pilot trainer[source] | Trainer aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Cessna[source] | Raytheon Hawker Beechcraft[source] |
| Status | In service[source] | Active service[source] |
48 ft 5 in (14.76 m)[source]
Maximum; T-41C · Maximum speed
Single source125 kn (144 mph, 232 km/h)[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-1A · 2 × Pratt & Whitney Canada JT15D -5B turbofan thrust each
Single source2 × Pratt & Whitney Canada JT15D -5B turbofan , 2,900 lbf (13 kN) thrust each[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] |
United States Air Force Japan Air Self-Defense Force[source] |
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | 180[source] |
|---|
| Manufactured | 1964–1996[source] | 1992–1997[source] |
|---|
| Introduction date | 1964[source] | 17 January 1992[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Beechjet/Hawker 400A[source] |
|---|
| Capacity | three passengers[source] | 4 passengers[source] |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | — |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| First flight | — | 5 July 1991[source] |
|---|
| Aspect ratio | — | 7.5:1[source] |
|---|
| Airfoil | — | Mitsubishi MAC510[source] |
|---|
| Stall speed | — | 93 kn (107 mph, 172 km/h) CAS[source] |
|---|
| Country of origin | — | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|