Seneca V
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PERFORMANCE SPECIFICATIONS
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ENGINE
Manufacturer
Model
Horsepower
Number of Cylinders
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Teledyne Continental
TSIO-360-RB and L/TSIO-360-RB
220 hp
6
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PROPELLER
Manufacturer
Number of Blades
Type
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Hartzell
2
Constant Speed, Full Feathering
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WEIGHTS
Maximum Takeoff Weight
Standard Empty Equipped Weight (b and c)
Standard Useful Load (a)
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4750 lbs/2155 kg
3413 lbs/1548 kg
1337 lbs/606 kg
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DIMENSIONS
Wing Span
Length
Height
Wing Area
Cabin Length
Cabin Width
Cabin Height
HEADROOM (Seat to Ceiling)
Front Seats
Middle Seats
Rear Seats
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38.9 ft/11.9 m
28.6 ft/8.7 m
9.9 ft/3.0 m
208.7 ft2/19.39 m2
124.25 in/315.6 cm
48.75 in/123.8 cm
42.0 in/106.7 cm
38 in/96.5 cm
35.75 in/90.8 cm
34.50 in/87.7 cm
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FUEL and OIL CAPACITY
Usable Fuel
Oil Capacity
BAGGAGE
Forward Compartment Volume
Aft Compartment Volume
Forward Compartment Capacity
Aft Compartment Capacity
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122 gallons/462 liters
8 quarts/ 7.6 liters
15.3 ft3/0.43 m3
17.3 ft3/0.49 m3
100 lbs/45.4 kgs
85 lbs/38.6 kgs
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MAXIMUM SPEED
Gross Weight @ 18,500ft
CRUISING SPEEDS
Max Cruise Power @ 10,000ft
Normal Cruise Power @ 10,000ft
CRUISING RANGE
Cruising range includes 45 minute fuel reserve at long range power plus allowance for fuel used during taxi, take-off, climb at MCP, cruise at stated mixture and descent.
Long Range Cruise Power @ 10,000 ft
Long Range Cruise Power @ 15,000 ft
Long Range Cruise Power @ 18,500 ft
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218 knots/404 km/h
182 knots/337 km/h
176 knots/326 km/h
812 nm/1504 km
828 nm/1533 km
819 nm/1517 km
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STALL SPEED
Flaps Down Full 40°
SERVICE CEILING
Two Engines (100fpm)
Single Engine (50fpm)
TAKE-OFF DISTANCE
Ground Roll
Total over 50 ft Obstacle (Flaps 25°)
LANDING DISTANCE
Ground Roll
Total over 50 ft Obstacle
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61 knots/113 km/h
*25,000 ft+/7620 m+
16,500 ft/5029 m
1,143 ft/348 m
1,707 ft/520 m
1,400 ft/427 m
2,180 ft/664 m
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a. Standard useful load is maximum takeoff weight minus standard equipped weight.
b. The standard empty weight and standard equipped weight are the same.
c. Standard equipped aircraft.
*25,000 ft is the maximum approved altitude.
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