Vspeeds Flashcards
Vne
190mph
Per wingtip STC (SA914NE)
Vno
170 mph IAS
Vfe 0 - 10°
160 mph IAS
Vfe 10° - 30°
120 mph IAS
Va
138 mph IAS
Vs
70 mph CAS
Vs0
62 mph CAS
Vlo
138 mph IAS
Vle
172 mph IAS
Max Ramp/Dock Weight
3755 lbs
Max Take-off floats
3744 lbs
Max Take-off wheels
3735 lbs
Max landing water
3661 lbs
Max Landing Land
3550 lbs
Max weight in each float locker
100 lbs
Vgl
91 mph IAS
Engine
Continental I0-550
Naturally Aspirated, Fuel injected, Horizontally opposed
Max Horsepower
300 HP continuous @ 2700 RPM @ 25 GPH @ sea level
CHT temp limits
200 - 460°F
Oil Temperature limits
100 - 240°F
Oil Pressure limits
10 - 100 PSI
Oil Pressure Normal range
30 - 60 PSI
Tachometer - Normal range
2200 - 2500 RPM
Tachometer Red Line
2700 RPM
Manifold Pressure - Normal range
15-24 in. Hg
Fuel Capacity (Total)
80 gallons
Fuel Capacity (Useable)
76 Gallons
Unusable Fuel
2 Gallons each wing tank
Type of Propeller
MT Reversing 3-blade propeller
Propeller operating limitations
- Cannot be used in the air
- 30 Second maximum
- Use Caution switching between reverse and forward thrust - aircraft may surge forward
- Use Caution when taxing in reverse on water to avoid damaging rudders/floats
- Only use on ground or water below 50 kts
- Max 20 in. Hg OR 2300 RPM