Seneca V

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PERFORMANCE SPECIFICATIONS

ENGINE
Manufacturer
Model
Horsepower
Number of Cylinders

Teledyne Continental
TSIO-360-RB and L/TSIO-360-RB
220 hp
6

PROPELLER
Manufacturer
Number of Blades
Type

Hartzell
2
Constant Speed, Full Feathering

WEIGHTS
Maximum Takeoff Weight
Standard Empty Equipped Weight (b and c)
Standard Useful Load (a)

4750 lbs/2155 kg
3413 lbs/1548 kg
1337 lbs/606 kg

DIMENSIONS
Wing Span
Length
Height
Wing Area
Cabin Length
Cabin Width
Cabin Height
HEADROOM (Seat to Ceiling)
Front Seats
Middle Seats
Rear Seats

38.9 ft/11.9 m
28.6 ft/8.7 m
9.9 ft/3.0 m
208.7 ft²/19.39 m²124.25 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

FUEL and OIL CAPACITY
Usable Fuel
Oil Capacity

BAGGAGE
Forward Compartment Volume
Aft Compartment Volume
Forward Compartment Capacity
Aft Compartment Capacity

122 gallons/462 liters
8 quarts/ 7.6 liters

15.3 ft³/0.43 m³17.3 ft³/0.49 m³100 lbs/45.4 kgs
85 lbs/38.6 kgs

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

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

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

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

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.

Seneca V ORDER YOURS TODAY!!
PERFORMANCE SPECIFICATIONS
ENGINE Manufacturer Model Horsepower Number of Cylinders	Teledyne Continental TSIO-360-RB and L/TSIO-360-RB 220 hp 6
PROPELLER Manufacturer Number of Blades Type	Hartzell 2 Constant Speed, Full Feathering
WEIGHTS Maximum Takeoff Weight Standard Empty Equipped Weight (b and c) Standard Useful Load (a)	4750 lbs/2155 kg 3413 lbs/1548 kg 1337 lbs/606 kg
DIMENSIONS Wing Span Length Height Wing Area Cabin Length Cabin Width Cabin Height HEADROOM (Seat to Ceiling) Front Seats Middle Seats Rear Seats	38.9 ft/11.9 m 28.6 ft/8.7 m 9.9 ft/3.0 m 208.7 ft²/19.39 m²124.25 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
FUEL and OIL CAPACITY Usable Fuel Oil Capacity BAGGAGE Forward Compartment Volume Aft Compartment Volume Forward Compartment Capacity Aft Compartment Capacity	122 gallons/462 liters 8 quarts/ 7.6 liters 15.3 ft³/0.43 m³17.3 ft³/0.49 m³100 lbs/45.4 kgs 85 lbs/38.6 kgs
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	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
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	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
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.