Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
M-7-235B · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Maule M-7 |
|---|---|---|
| Type | Light aircraft[source] | Utility aircraft[source] |
| Manufacturer | Cirrus Aircraft[source] | Maule Air[source] |
| Number built | 2,084 (through 2025)[source] | ca. 500 by 1995[source] |
| Manufactured | 1999–present[source] | — |
| First flight | 21 March 1995 |
23.67 ft (7.21 m)[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]
M-7-235B · 1 × Lycoming O-540-J1A5D six cylinder, horizontally-opposed , air-cooled aircraft engine
Single source1 × Lycoming O-540-J1A5D six cylinder, horizontally-opposed , air-cooled aircraft engine , 235 hp (175 kW)[source]
SR20-G3 · Service ceiling
Single source17,500 ft (5,300 m)[source]
MX-7 Series / MX-7-180B · Service ceiling
Manufacturer claimMX-7 Series / MX-7-180C · Service ceiling
Manufacturer claimMX-7 Series / MXT-7-180 · Service ceiling
Manufacturer claim15,000 ft (4572 m)[source]MX-7 Series / MX-7-180B
15,000 ft (4572 m)[source]MX-7 Series / MX-7-180C
15,000 ft (4572 m)[source]MX-7 Series / MXT-7-180
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1984[source] |
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | four passengers[source] |
|---|
| Propellers | 3-bladed[source] | 2-bladed Hartzell Propeller HC-C2YR-1BF/F8468A-6R constant speed propeller[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | 49 mph (80 km/h, 43 kn) flaps down[source] |
|---|
| National origin | United States[source] | United States[source] |
|---|
| Designer | — | Belford Maule[source] |
|---|
| Fuel capacity | — | 40 U.S. gallons (150 L; 33 imp gal) usable (standard)[source] |
|---|
| Never exceed speed | — | 182 mph (293 km/h, 158 kn)[source] |
|---|
| g limits | — | +3.8/-1.5 g[source] |
|---|
| Engine | — | Lycoming 0-360-C1F (2000hr. TBO)[source]MX-7 Series / MX-7-180B Lycoming 0-360-C1F (2000hr. TBO)[source]MX-7 Series / MX-7-180C Lycoming 0-360-C1F (2000hr. TBO)[source]MX-7 Series / MXT-7-180 |
|---|
Empty; MX-7 Series / MX-7-180C · Empty weight
Single sourceGross; M-7-235B · Gross weight
Single sourceGross; MX-7 Series / MX-7-180B · Gross weight
Single sourceGross; MX-7 Series / MX-7-180C · Gross weight
Single sourceMX-7 Series / MXT-7-180 · Weight
Single source1,549 lb (703 kg) typical, equipped[source]
2,500 lb (1,134 kg)[source]
2500 lbs. (1136kg)[source]MX-7 Series / MX-7-180B
1470 lbs. (667 kg)[source]MX-7 Series / MX-7-180B
2500 lbs. (1136kg)[source]MX-7 Series / MX-7-180C
1545 lbs. (701 kg)[source]MX-7 Series / MX-7-180C
2500 lbs. (1136kg)[source]MX-7 Series / MXT-7-180
1565 lbs. (667 kg)[source]MX-7 Series / MXT-7-180Source text · numeric interpretation needs review