Seneca V

PERFORMANCE SPECIFICATIONS 

ENGINE

Manufacturer

Teledyne Continental

Model

TSI0-360-RB and L/TSI0-360-RB

Horsepower

220

Number of Cylinders

6

PROPELLER

Manufacturer

Hartzell

Number of Blades

2

Type

Constant Speed, Full Feathering

WEIGHTS

Maximum Takeoff Weight

4750 lbs/2155 kg

Standard Empty Equipped Weight (b and c)

3413 lbs/1548 kg

Standard Useful Load (a)

1337 lbs/606 kg

WING AREA

Wing Area

208.7 ft2/19.39 m2

DIMENSIONS

Wing Span

38.9 ft/11.9 m

Length

28.6 ft/8.7 m

Height

9.9 ft/3.0 m

Cabin Length

124.25 in/315.6 cm

(Instrument Panel to Rear Bulkhead)

Cabin Width

48.75 in/123.8 cm

Cabin Height

42.0 in/106.7 cm

Headroom (Seat to Ceiling)

 

Front Seats

38 in/96.5 cm

Middle Seats

35.75 in/90.8 cm

Rear Seats

34.5 in/87.7 cm

FUEL AND OIL CAPACITY

Usable Fuel

122 gal/462 l

Oil Capacity

8 qts/7.6 l

BAGGAGE

Volume

Forward Compartment

15.3 ft3/0.43 m3

Aft Compartment

17.3 ft3/0.49 m3

Capacity

Forward Compartment

100 lbs/45.4 kg

Aft Compartment

85 lbs/38.6 kg

MAXIMUM SPEED

TAS

Gross Weight (@ 18,500 ft)

218 kts/404 km/h

CRUISING SPEEDS

TAS

 

kts/km/h
10,000 ft

kts/km/h
18,500 ft

Max Cruise Power

182/337

197/365

Normal Cruise Power

176/326

190/351

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)

812 nm/1504 km

Long Range Cruise Power (@ 15,000 ft)

828 nm/1533 km

Long Range Cruise Power (@ 18,500 ft)

819 nm/1517 km

STALL SPEED

IAS

Flaps Full Down 40

61 knots/113 km/h

SERVICE CEILING

Two Engines (100 fpm)

*25,000 ft+/7620 m+

Single Engine (50 fpm)

16,500 ft/5029 m

*25,000 ft is max. approved altitude

TAKE-OFF DISTANCE

Ground Roll

1,143 ft/348 m

Total over 50 ft obstacle (Flaps 25)

1,707 ft/520 m

LANDING DISTANCE

Ground Roll

1400 ft/427 m

Total over 50 ft obstacle

2180 ft/664 m

 

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