Saratoga II TC	Others talk about the future; with the Piper Aircraft Saratoga II TC the future is here, now.  Equipped and delivering right now with the "Complete" Avidyne Entegra glass panel or Garmin G1000 including: Air-Data Computer displaying constant wind direction, speed, and fuel computations. As well as, Flight Director & Autopilot system including Altitude Pre-select, Engine Management system, and Mode S transponder (with traffic information) as standard equipment. Couple that to roomy 6 seat comfort, excellent speed, range & generous tax savings from the government...You've got a winner!
PERFORMANCE SPECIFICATIONS
ENGINE Manufacturer Model Horsepower Number of Cylinders	Lycoming TIO-540-AHIA 300 hp to 12,000 ft. 6
PROPELLER Manufacturer Number of Blades Type	Hartzell 3 Constant Speed
WEIGHTS Maximum Takeoff Weight Standard Empty Equipped Weight (b and c) Standard Useful Load (a)	3600 lbs/1633 kg 2465 lbs/1118 kg 1135 lbs/515 kg
DIMENSIONS Wing Span Length Height Wing Area Cabin Length Cabin Width Cabin Height HEADROOM (Seat to Ceiling) Front Seats Middle Seats Rear Seats	35.5 ft/10.8 m 24.0 ft/7.32 m 7.3 ft/2.2 m 178.3 ft2/16.56 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/87.6 cm
FUEL and OIL CAPACITY Usable Fuel Oil Capacity BAGGAGE Forward Compartment Volume Aft Compartment Volume Forward Compartment Capacity Aft Compartment Capacity	102 gallons/386 liters 12 quarts/ 11.4 liters 7 ft3/0.2 m3 17.3 ft3/0.49 m3 100 lbs/45.4 kgs 100 lbs/45.4 kgs
MAXIMUM SPEED TAS at Mid-Cruise Weight CRUISING SPEEDS 8,000 ft 10,000 ft 15,000 ft 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 and descent. Long Range 8,000 ft Cruise Power 10,000 ft Cruise Power 15,000 ft	TAS 187 knots/346 km/h TAS 172 knots/318 km/h 175 knots/324 km/h 185 knots/342 km/h 950 nm/1759 km 948 nm/1755 km 945 nm/1750 km
STALL SPEED Flaps Down Full 40° MAXIMUM OPERATING ALTITUDE Maximum Operating Altitude TAKE-OFF DISTANCE Ground Roll Total over 50 ft Obstacle LANDING DISTANCE Ground Roll Total over 50 ft Obstacle	IAS 63 knots/117 km/h 20,000 ft/6096 m 1110 ft/338 m 1810 ft/552 m 880 ft/268 m 1700 ft/518 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.