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]
UTVA 75A21 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | UTVA 75 |
|---|---|---|
| Type | Primary pilot trainer[source] | Military and civilian trainer aircraft[source] |
| National origin | United States[source] | Yugoslavia[source] |
| Manufacturer | Cessna[source] | UTVA[source] |
| Status | In service[source] | Active |
7.11 m (23 ft 4 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]
UTVA 75A21 · 1 × Lycoming IO-360-B1F 4-cyl. air-cooled horizontally-opposed piston engine
Single source1 × Lycoming IO-360-B1F 4-cyl. air-cooled horizontally-opposed piston engine, 134 kW (180 hp)[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] | — |
|---|
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | — |
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| Manufactured | 1964–1996[source] | — |
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| Introduction date | 1964[source] | 1978[source] |
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| Developed from | Cessna 172 Cessna R172[source] | — |
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| Capacity | three passengers[source] | 210 kg (460 lb) max[source] |
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| Propellers | 2-bladed variable-pitch propeller[source] | 2-bladed Hartzell HC-C2YK-1BF/F7666A variable-pitch metal propeller[source] |
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| Alternative designation | T-41 Mescalero[source] | — |
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| Primary user | — | Serbia Air Force[source] |
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| First flight | — | 19 May 1976[source] |
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| Aspect ratio | — | 6.5[source] |
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| Fuel capacity | — | standard:160 L (42 US gal; 35 imp gal): with drop tanks 360 L (95 US gal; 79 imp gal)[source] |
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| Stall speed | — | 95 km/h (59 mph, 51 kn) flaps up at idle[source] |
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| Never exceed speed | — | 270 km/h (168 mph, 146 kn)[source] |
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| g limits | — | +4.4 -2.2[source] |
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| Takeoff distance to 50 ft (15 m) | — | 501 m grass at Sea Level[source] |
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| Landing distance from 50 ft (15 m) | — | 450 m grass at Sea Level[source] |
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| Hardpoints | — | 2 with a capacity of 150 kg (330 lb) each, with provisions to carry combinations of:[source] |
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| Rockets | — | 2 × RL 128-02 128 mm (HVAR-5), or 2 × 57 millimetres (2.2 in) rocket launchers with 12 rockets[source] |
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| Bombs | — | 2 × 120 kg bombs, or 4 × 50 kg bombs[source] |
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| Other | — | 2 × MAC-AA-52 container with 7.62 mm , or 2 × cargo container 100 kg capacity, or 2 × drop tanks[source] |
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| standard | — | (model 75) KING KR85 ADF and KING KY 195B[source] |
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| optional | — | (model 75A catalog only) KING KR87 ADF, RNAV KING KNS81 VOR/LOC: KING KN 53, KING KY 197 Indicators: HSI KING KI 525A, and RMI KING KI 229, DME:KING KN 62A, Transponder: KING KT 79, Audio panel: KING KMA 24[source] |
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