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]
G-4M · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Soko G-4 Super Galeb |
|---|---|---|
| Type | Primary pilot trainer[source] | Military trainer aircraft[source] |
| National origin | United States[source] | Yugoslavia[source] |
| Manufacturer | Cessna[source] | SOKO[source] |
| Status | In service[source] | In service |
12.25 m (40 ft 2 in)[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]
G-4M · Combat range
Single sourceG-4M · with cannon pack and four BL755 cluster bombs (combat radius
Single source1,300 km (810 mi, 700 nmi) with cannon pack and four BL755 cluster bombs (combat radius 485 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]
G-4M · 1 × Rolls-Royce Viper 632-46 turbojet thrust
Single source1 × Rolls-Royce Viper 632-46 turbojet , 17.8 kN (4,000 lbf) thrust[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] | Serbian Air Force Myanmar Air Force Montenegrin Air Force (historical) Yugoslav Air Force (historical)[source] |
|---|
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | 85[source] |
|---|
| Manufactured | 1964–1996[source] | 1984–1991[source] |
|---|
| Introduction date | 1964[source] | 1983[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 | — | Aeronautical Technical Institute[source] |
|---|
| First flight | — | 17 July 1978[source] |
|---|
| Aspect ratio | — | 5.01[source] |
|---|
| Fuel capacity | — | 1,882 kg (maximum internal and external fuel)[source] |
|---|
| Stall speed | — | 180 km/h (97 mph, 112 kn) (flaps and undercarriage down)[source] |
|---|
| Never exceed speed | — | 921 km/h (572 mph, 497 kn) 0.9M at 11,000 m[source] |
|---|
| g limits | — | -4.2 to +8[source] |
|---|
| Time to altitude | — | 6 minutes to 8,000m[source] |
|---|
Maximum take-off; G-4M · Max takeoff weight
Single source