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]
Lasta 95N · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Utva Lasta |
|---|---|---|
| Type | Primary pilot trainer[source] | Trainer aircraft[source] |
| National origin | United States[source] | — |
| Manufacturer | Cessna[source] | Utva Aviation Industry[source] |
| Status | In service[source] | In service[source] |
| Primary users |
7.965 m (26 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]
Lasta 95N · 1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine, 232 kW (311 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Air Force United States Army Indonesian Air Force Turkish Air Force[source] |
Serbian Air Force Iraqi Air Force[source] |
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | 37[source] |
|---|
| Manufactured | 1964–1996[source] | — |
|---|
| Introduction date | 1964[source] | 2010[source] |
|---|
| Developed from | Cessna 172 Cessna R172[source] | — |
|---|
| Capacity | three passengers[source] | — |
|---|
| Propellers | 2-bladed variable-pitch propeller[source] | 2-bladed HARTZELL HC-C2YR-4CF/FC 8475-8 constant speed propeller, 1.98 m (6 ft 6 in) diameter[source] |
|---|
| Alternative designation | T-41 Mescalero[source] | — |
|---|
| Designer | — | Military Technical Institute[source] |
|---|
| First flight | — | Lasta 1 prototype: 2 September 1985 Lasta 95: 26 February 2009[source] |
|---|
| Aspect ratio | — | 6.3[source] |
|---|
| Stall speed | — | 95 km/h (59 mph, 51 kn)[source] |
|---|
| Never exceed speed | — | 425 km/h (264 mph, 229 kn)[source] |
|---|
| g limits | — | +6 -3 g[source] |
|---|
| Hardpoints | — | 2 with a capacity of 100 kg (220 lb) bombs, 7.62 mm (0.300 in) or 12.7 mm (0.500 in) calibre machine-gun pods or 57 mm (2.244 in) rocket pods (7 rockets each)[source] |
|---|
| Country of origin | — | Serbia[source] |
|---|
| Reported operators | — |
|
|---|
Maximum take-off; Lasta 95N · unarmed
Single source