Saratoga II HP
The New Piper Aircraft, Inc.
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STANDARD EQUIPPED LIST PRICE $529,200 ENGINE Manufacturer Lycoming Model IO-540-K1G5 Horsepower 300 hp Number of Cylinders 6 PROPELLER Manufacturer Hartzell Number of Blades 3 Type Constant Speed WEIGHTS Maximum Take-off Weight 3,600 lbs/1,633 kg Maximum Ramp Weight 3,615 lbs/1,640 kg Standard Equipped Weight 2,411 lbs/1,094 kg Standard Useful Load (a and b) 1,204 lbs/546 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 36.2 ft/11.0 m Length 27.9 ft/8.5 m Height 8.5 ft/2.6 m Cabin Length 124.25 in/315.6 cm 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 34.50 in/87.6 cm WING AREA Wing Area 178.3 ft2/16.56 m2 FUEL AND OIL CAPACITY Usable Fuel 102 gal/386 liters Oil Capacity 12 qts/11.4 liters MAXIMUM SPEED TAS Maximum Cruise Power 175 kts/324 km/h CRUISING SPEEDS TAS High Speed Cruise (@ 4,000 ft 166 kts/307 km/h 50° Rich of Peak EGT Mixture) CRUISING RANGE TAS Cruising range includes 45 minute fuel reserve at long range power plus allowance for fuel used during taxi, take-off, climb at maximum climb power, cruise and descent Long Range Cruise Power 859 nm/1,591 km STALL SPEED Flaps Full Down 40° 63 kias/117 km/h 61 kcas/113 kn/h SERVICE CEILING 100 FTM 15,588 ft/4,752 m BAGGAGE Volume Forward Compartment 7 ft3/0.2 m3 Aft Compartment 17.3 ft3/0.49 m3 Capacity Forward Compartment 100 lbs/45.4 kg Aft Compartment 100 lbs/45.4 kg TAKE-OFF DISTANCE Ground Roll 1,200 ft/366 m Total over 50 ft Obstacle 1,770 ft/539 m LANDING DISTANCE Ground Roll 640 ft/195 m Total over 50 ft Obstacle 1,520 ft/463 m
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