Seneca V

The New Piper Aircraft, Inc.

фотография с сайта www.newpiper.com

STANDARD EQUIPPED LIST PRICE $735,000
 
ENGINE 
Manufacturer Teledyne Continental
Model TSI0-360-RB and
 L/TSI0-360-RB
Horsepower 220 hp
Number of Cylinders 6
 
PROPELLER 
Manufacturer Hartzell
Number of Blades 2
Type Constant Speed
 Full-Feathering
 
WEIGHTS 
Maximum Take-off Weight 4,750 lbs/2,155 kg
Maximum Ramp Weight 4,773 lbs/2,165 kg
Standard Equipped Weight 3,406 lbs/1,545 kg
Standard Useful Load (a and b) 1,367 lbs/620 kg
a. Standard useful load is max ramp weight 
minus standard equipped weight. 
b. Useful load is indicated for a standard equipped aircraft. 
 
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) 
 38 in/96.5 cm
 35.75 in/90.8 cm
 34.5 in/87.7 cm
 
WING AREA 
Wing Area 208.7 ft2/19.39 m2
 
FUEL AND OIL CAPACITY 
Usable Fuel 122 gal/462 liters
Oil Capacity 8 qts/7.6 liters
 
MAXIMUM SPEED TAS 
Gross Weight (@ 18,500 ft) 218 kts/404 km/h
 
CRUISING SPEEDS TAS 
 
 kts/km/h
 10,000 ft
Max Cruise Power 182/337
Normal Cruise Power 176/326
 
CRUISING RANGE TAS 
Cruising range includes 45 minute fuel reserve at 
long range cruise power plus allowance for fuel used 
during taxi, take-off, climb at maximum climb power 
and cruise at stated mixture and descent 
 
 
 
 
 
 
 
STALL SPEED IAS 
Flaps Full Down 40° 64 kias/119 km/h
 65 kcas/120 kn/h
 
SERVICE CEILING 
 
Two Engines (100fpm) 
Single Engine (50fpm) 
*25,000 ft is max. approved altitude 
 
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
 
TAKE-OFF DISTANCE 
Ground Roll 1,143 ft/348 m
Total over 50 ft Obstacle 1,707 ft/520 m
Flaps 25º 
 
LANDING DISTANCE 
Ground Roll 1,400 ft/427 m
Total over 50 ft Obstacle 2,180 ft/664 m

Сайт разработчика: www.newpiper.com