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]
Yak-130 · Length
Single sourceConfiguration
| Specification | Cessna T-41 Mescalero | Yakovlev Yak-130 |
|---|---|---|
| Type | Primary pilot trainer[source] | Lead-in fighter trainer / Light combat aircraft[source] |
| National origin | United States[source] | Russia[source] |
| Manufacturer | Cessna[source] | Yakovlev, Sokol, Yakovlev Corporation[source] |
| Status | In service[source] | Active |
11.49 m (37 ft 8 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]
Yak-130 · 2 × Ivchenko-Progress AI-222-25 turbofan engines thrust each
Single source2 × Ivchenko-Progress AI-222-25 turbofan engines, 24.52 kN (5,510 lbf) thrust each[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] | Russian Aerospace Forces Bangladesh Air Force Algerian Air Force Myanmar Air Force Islamic Republic of Iran Air Force[source] |
|---|
| Number built | T-41A : 230 T-41B : 255 T-41C : 52 T-41D : 299[source] | 219[source] |
|---|
| Manufactured | 1964–1996[source] | — |
|---|
| Introduction date | 1964[source] | 19 February 2010[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] | Yak-130[source] |
|---|
| Designer | — | Yakovlev[source] |
|---|
| Built by | — | Irkut Corporation Sokol Aircraft Plant[source] |
|---|
| First flight | — | 25 April 1996 ( 1996-04-25 ) (Yak/AEM-130) 30 April 2004 ( 2004-04-30 ) (Yak-130)[source] |
|---|
| Variant | — | Alenia Aermacchi M-346 Master[source] |
|---|
| Guns | — | SNPU-130 gun pod[source] |
|---|
| Hardpoints | — | 8 (1 on each wingtip, usable only for flares/chaff, 3 under each wing) with a capacity of up to 3,000 kg (6,614 lb), with provisions to carry combinations of: Rockets: 80 mm S-8 rocket, S-25 rocket Missiles: R-73 infrared-homing short-range air-to-air missiles Bombs: FAB-M62, ZB-500, KAB-500Kr[source] |
|---|
| Stall speed | — | 165 km/h (103 mph, 89 kn)[source] |
|---|
| g limits | — | + 8.0 − 3.0[source] |
|---|
| Wing loading | — | 276.4 kg/m 2 (56.6 lb/sq ft)[source] |
|---|
| Thrust/weight | — | 0.70[source] |
|---|
| Rockets | — | 80 mm S-8 rocket, S-25 rocket[source] |
|---|
| Missiles | — | R-73 infrared-homing short-range air-to-air missiles[source] |
|---|
| Bombs | — | FAB-M62, ZB-500, KAB-500Kr[source] |
|---|
Maximum take-off; Yak-130 · Max takeoff weight
Single source