Piper 1997 PA-34-220T Seneca V

Tuesday, January 01, 2008 at 12:00 AM ET

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Key Takeaways:

The article details the specifications for the Piper 1997 PA-34-220T Seneca V, a 6-seater aircraft powered by twin 200 HP Continental L/TSIO-360-RB engines.
Key operational statistics include a gross weight of 4750 lbs, a useful load of 1396 lbs, and a fuel capacity of 122 gallons.
Performance figures highlight a cruise speed of up to 198 knots, a maximum range of 715 nautical miles (at 65% power with reserve), a service ceiling of 25,000 ft, and a best rate of climb of 1480 fpm.

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Piper 1997 PA-34-220T Seneca V

Engine make/model:

Cont. L/TSIO-360-RB

Horsepower:

200

TBO hrs.:

1800

Propeller:

Const. spd.

Landing gear type:

Tri/Retr.

Gross weight (lbs.):

4750

Empty weight, std. (lbs.):

3377

Useful load, std. (lbs.):

1396

Fuel (gals.):

122

Wingspan:

38 ft. 9 in.

Overall length:

28 ft. 7 in.

Height:

9 ft. 10 in.

Wing area (sq. ft.):

208.7

Seating capacity:

6

Cabin width (in.):

48

Cabin height (in.):

48

Baggage capacity (lbs.):

185

PERFORMANCE

Cruise speed (kts.):

75% power:

198

65% power:

190

Max range (w/ reserve) (nm):

75% power:

660

65% power:

715

Fuel consumption (gph):

75% power:

26

65% power:

24

Estimated endurance (65% power with 1-hr. reserve):

4 hrs. 18 mins.

Stall speed (gear, flaps down) (knots):

61

Best rate of climb (fpm):

1480

Service ceiling (ft.):

25,000

Takeoff ground roll (ft.):

1525

Landing ground roll (ft.):

1400