![]() |
![]() |
|
|
|
|
|
|
| . | . |
| Make |
Piper
|
| Model |
PA34 Seneca I
|
| Seats |
6
|
| ID |
N4399E
|
|
|
|
| Engine |
(Right) Lycoming LIO-360-C1E6
200 BHP (Left) Lycoming IO-360-C1E6 200 BHP |
| Equipments |
Retractable landing gears
Constant speed propeller Intercom, Dual NAV, Dual COM Mode C Transponder ADF, Marker Beacons DME, Glide Slope 2 Axis Auto pilot |
| Limitations | |
| Weights |
Basic Empty Weight:
Max. Take off weight: 4200 lbs. (Normal category) Max. Landing weight: 4000 lbs. (Normal category) |
| Fuel |
Aviation grade 100/130 (minimum)
Usable fuel: 95 gallons |
| Airspeed (Indicated) |
Flap operating range: Vso 69- Vfe 125 mph
Normal operating range: Vs1 76- Vno 190 mph Caution range: Vno 190- Vne 217 mph Never exceed speed: Vne 217 mph Best angle of climb speed: Vx 90 mph Vxse 93 mph (single engine) Best rate of climb speed: Vy 105 mph Vyse 105 mph (single engine) Maneuvering speed: Va 146 mph (4200 lbs.) Minimum controllable speed: Vmc 80 mph |
|
|
|