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]
Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Grob G 120TP |
|---|---|---|
| Crew | one[source] | two[source] |
| Type | Primary pilot trainer[source] | Trainer[source] |
| National origin | United States[source] | Germany[source] |
| Manufacturer | Cessna[source] | Grob Aircraft[source] |
8.4 m (27 ft 7 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]
1 × Rolls-Royce M250-B17F Turboprop aircraft engine
Single source1 × Rolls-Royce M250-B17F Turboprop aircraft engine , 340 kW (456 hp)[source]
at 10,000 ft and maximum endurance power setting
Single source6 hours at 10,000 ft and maximum endurance power setting[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In production[source] |
|---|
| Primary users | United States Air Force United States Army Indonesian Air Force Turkish Air Force[source] | Indonesian Air Force Mexican Air Force Bangladesh Air Force UK Military Flying Training System Swedish Air Force[source] |
|---|
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | — |
|---|
| Manufactured | 1964–1996[source] | 2010-present[source] |
|---|
| Introduction date | 1964[source] | 2013[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | Grob G 120[source] |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 5-bladed MT Propeller , 2.1 m (6 ft 11 in) diameter[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| First flight | — | 2010[source] |
|---|
| Fuel capacity | — | 360 litres (79 imp gal; 95 US gal)[source] |
|---|
| Stall speed | — | 107 km/h (67 mph, 58 kn) (MSL, landing configuration)[source] |
|---|
| g limits | — | +6/-4G[source] |
|---|