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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
M-7-235B · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Maule M-7 |
|---|---|---|
| Type | Business jet[source] | Utility aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Maule Air[source] |
| Status | Out of production, in active service[source] | — |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
| Number built | 512[source] |
23.67 ft (7.21 m)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source862 km/h (536 mph, 465 kn) at 7,620 m (25,000 ft) (max cruise)[source]
750 km/h (470 mph, 400 kn) at 12,200 m (40,000 ft) (econ. cruise)[source]
Cruise; M-7-235B · maximum structural cruising speed
Single source147 mph (237 km/h, 128 kn) maximum structural cruising speed[source]
Falcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[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]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
Falcon 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Falcon 20F · absolute ceiling
Single source12,800 m (42,000 ft) (absolute ceiling)[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
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
ca. 500 by 1995[source] |
| Manufactured | 1965–1991[source] | — |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 1984[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | four passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 40 U.S. gallons (150 L; 33 imp gal) usable (standard)[source] |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | 49 mph (80 km/h, 43 kn) flaps down[source] |
|---|
| National origin | France[source] | United States[source] |
|---|
| Designer | — | Belford Maule[source] |
|---|
| Propellers | — | 2-bladed Hartzell Propeller HC-C2YR-1BF/F8468A-6R constant speed propeller[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