FORCETALLY
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At a glance
Measured figures
Cessna 177B · Length
Single source27 ft 8 in (8.43 m)[source]
Alto TG European ultralight · Length
Configuration
| Specification | Cessna 177 Cardinal | Direct Fly Alto |
|---|---|---|
| Type | Light utility aircraft[source] | Light sport aircraft[source] |
| Manufacturer | Cessna Aircraft Company[source] | Direct Fly s.r.o.[source] |
| Number built | 4,295[source] | 41 (2015)[source] |
| Manufactured | 1968–1978[source] | — |
6.15 m (20 ft 2 in)[source]
Empty; Cessna 177B · Empty weight
Single sourceMaximum take-off; Cessna 177B · Max takeoff weight
Single source1,495 lb (678 kg)[source]
2,500 lb (1,134 kg)[source]
Empty; Alto TG European ultralight · Empty weight
Single sourceGross; Alto TG European ultralight · Gross weight
Single sourceCruise; Cessna 177B · Cruise speed
Single sourceMaximum; Cessna 177B · Maximum speed
Single source136 kn (157 mph, 252 km/h)[source]
124 kn (143 mph, 230 km/h)[source]
Cruise; Alto TG European ultralight · Cruise speed
Single sourceMaximum; Alto TG European ultralight · Maximum speed
Single sourceCessna 177B · Range
Single source604 nmi (695 mi, 1,119 km)[source]
Cessna 177B · 1 × Lycoming O-360 -A1F6D air-cooled flat-4 engine
Single source1 × Lycoming O-360 -A1F6D air-cooled flat-4 engine , 180 hp (130 kW)[source]
Alto TG European ultralight · 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 hp)[source]
Cessna 177B · Service ceiling
Single source14,600 ft (4,500 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Introduction date | 1968[source] | 2008[source] |
|---|
| First flight | July 15, 1966[source] | — |
|---|
| Capacity | 3 passengers[source] | one passenger[source] |
|---|
| National origin | — | Czech Republic[source] |
|---|
| Status | — | In production[source] |
|---|
| Primary user | — | Ukrainian Air Force[source] |
|---|
| Fuel capacity | — | 118 litres (26 imp gal; 31 US gal)[source] |
|---|
| Stall speed | — | 65 km/h (40 mph, 35 kn)[source] |
|---|
| Never exceed speed | — | 270 km/h (170 mph, 150 kn)[source] |
|---|
| g limits | — | +4/-2[source] |
|---|
| Wing loading | — | 46.6 kg/m 2 (9.5 lb/sq ft)[source] |
|---|