Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
T-35A · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | ENAER T-35 Pillán |
|---|---|---|
| Type | Light aircraft[source] | Trainer[source] |
| Manufacturer | Cirrus Aircraft[source] | ENAER[source] |
| Number built | 2,084 (through 2025)[source] | 154[source] |
| Manufactured | 1999–present[source] | 28 December 1984 – 1991 |
8 m (26 ft 3 in)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
T-35A · 75% power at 2,440 m (8,005 ft) (45 minutes reserve)
Single source1,093 km (679 mi, 590 nmi) 75% power at 2,440 m (8,005 ft) (45 minutes reserve)[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
T-35A · 1 × Avco Lycoming AEIO-540-K1K5 6-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Avco Lycoming AEIO-540-K1K5 6-cylinder air-cooled horizontally-opposed piston engine, 224 kW (300 hp)[source]
T-35A · Wing area
Single source13.69 m 2 (147.4 sq ft)[source]
T-35A · 75% power at sea level
Single source75% power at sea level 4 hours 24 minutes[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | 6 March 1981[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | — |
|---|
| Propellers | 3-bladed[source] | 3-bladed Hartzell HC-C3YR-4BF/FC7663R, 1.93 m (6 ft 4 in) diameter constant-speed propeller[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 125 km/h (78 mph, 67 kn) flaps up[source] |
|---|
| National origin | United States[source] | Chile[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Chilean Air Force Spanish Air and Space Force National Air and Naval Service of Panama Paraguayan Air Force[source] |
|---|
| Developed from | — | Piper PA-32R[source] |
|---|
| Airfoil | — | root: NACA 65 2 -415 ; tip: NACA 65 2 -415 modified[source] |
|---|
| Fuel capacity | — | 291.5 L (77.0 US gal; 64.1 imp gal) in two wing leading edge integral tanks / 210 kg (463 lb) (272.5 L (72.0 US gal; 59.9 imp gal) usable)[source] |
|---|
| Maximum flap extension speed | — | 218 km/h (135 mph; 118 kn)[source] |
|---|
| Maximum undercarriage extension speed | — | 256 km/h (159 mph; 138 kn)[source] |
|---|
| Approach speed over 15 m (49 ft) obstacle | — | 148 km/h (92 mph; 80 kn)[source] |
|---|
| Landing speed | — | 120 km/h (75 mph; 65 kn)[source] |
|---|
| Never exceed speed | — | 446 km/h (277 mph, 241 kn)[source] |
|---|
| Absolute ceiling | — | 6,250 m (20,505 ft)[source] |
|---|
| g limits | — | + 6 - 3[source] |
|---|
| Time to altitude | — | 1,830 m (6,004 ft) in 4 minutes 42 seconds[source] |
|---|
| Wing loading | — | 97.73 kg/m 2 (20.02 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.167 kW/kg (0.102 hp/lb)[source] |
|---|
| Take-off run | — | 287 m (942 ft)[source] |
|---|
| Take-off distance to 15 m (49 ft) | — | 494 m (1,621 ft)[source] |
|---|
| Landing run | — | 238 m (781 ft)[source] |
|---|
| Landing distance from 15 m (49 ft) | — | 509 m (1,670 ft)[source] |
|---|