| STANDARD EQUIPPED LIST PRICE |
$510,645 |
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| ENGINE |
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| Manufacturer |
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Lycoming |
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| Model |
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L/O-360-A1H6 |
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| Horsepower |
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180 hp each |
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| WEIGHTS |
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| Maximum Take-off Weight |
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3,800 lbs/1,724 kg |
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| Maximum Ramp Weight |
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3,816 lbs/1,731 kg |
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| Standard Equipped Weight |
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2,609 lbs/1,186 kg |
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| Standard Useful Load (a & b) |
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1,207 lbs/547 kg |
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| a. Standard useful load is max ramp weight |
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| minus standard equipped weight. |
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| b. Useful load is indicated for a standard equipped aircraft. |
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| DIMENSIONS |
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| Wing Span |
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38.6 ft/11.8 m |
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| Length |
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27.6 ft/8.4 m |
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| Height |
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8.5 ft/2.6 m |
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| Wing Area |
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183.8 ft2/17.08 m2 |
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| FUEL AND OIL CAPACITY |
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| Usable Fuel |
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108 gal/409 liters |
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| MAXIMUM SPEED TAS |
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| TAS at Gross Weight |
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168 kts/311 km/h |
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| CRUISING SPEEDS TAS |
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| 75% Power |
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162 kts/300 km/h |
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| CRUISING RANGE |
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| 45 min. reserves at 55% Power |
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770 nm/1,426 km |
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| STALL SPEED |
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| Flaps Full Down 40° |
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55 kias/102 km/h |
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59 kcas/109 kn/h |
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| SERVICE CEILING |
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| Twin Engine (100 fpm) |
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15,000 ft/4,572 m |
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| Single Engine (50 fpm) |
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3,800 ft/1,158 m |
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| TAKE-OFF DISTANCE |
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| Total over 50 ft Obstacle |
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2,200 ft/671 m |
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| LANDING DISTANCE |
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| Total over 50 ft Obstacle |
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1,490 ft/454 m |
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| STANDARD EQUIPPED LIST |
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| Includes all listed standard equipment, FLY-AWAY-FACTORY (F.A.F.) |
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| Vero Beach, FL. Dealer delivery and local taxes extra. |
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| Piper Aircraft, Inc. reserves the right to make changes in |
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| specifications, materials, equipment, or prices at any time without prior |
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| notice or to discontinue models as required. |
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| POWERPLANT AND PROPELLER |
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| Engines - 2 Counter Rotating Lycoming 180 HP at 2700 RPM, |
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4 Cylinders, Direct Drive, Dual Ignition with Shielding |
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| Dynafocal Engine Mounts with Integral Dampers, Two |
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| Propellers-2 Hartzell, 2 Blade, Constant Speed, Full Feathering |
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| Unfeathering Accumulators, Two |
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| Propeller Spinners, Two |
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| Geared Starters, 12 Volt, Two |
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| Air Filter, Dry Type, Two |
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| Oil Filter, Full Flow, Two |
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| Oil Coolers with Thermostatic Control, Two |
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| Engine Driven Vacuum Pumps |
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| Oil Quick Drains, Two |
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| Cross-Over Exhaust System with Muffler, Two |
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| Carburetor Heat with Manual Control, Two |
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| Cowl Flaps with Manual Control, Two |
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| Engine Hour Recorder |
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| Flight Hour Recorder |
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| FLIGHT INSTRUMENTS AND INDICATORS |
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| All Metal Instrument Panel |
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| Piper Truespeed Indicator |
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| Magnetic Compass (Illuminated) |
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| Sensitive Altimeter (In. And Mb.) |
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| Artificial Horizon Gyro |
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| Directional Gyro |
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| Turn Coordinator |
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| Vertical Speed Indicator |
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| Heated Pitot Head |
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| Alternate Instrument Static Source and Control |
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| Outside Air Temperature Gauge |
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| Ammeters, Two |
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| Annunciator Panel, with Push to Test |
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• Alternator Inoperative |
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• Oil Pressure Low |
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• Gyro Pressure Low |
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• Voltage Low |
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• Heater Over Temp |
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| Dual Tachometer |
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| Dual Manifold Pressure Gauge |
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| Fuel Quantity Gauges, Two |
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| Fuel Pressure Gauges, Two |
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| Oil Temperature Gauges, Two |
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| Oil Pressure Gauges, Two |
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| Cylinder Head Temperature Gauges, Two |
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| Dual Exhaust Gas Temperature Gauge |
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| Dual Vacuum System with Indicator |
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| Landing Gear Position Lights, Three |
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| Landing Gear-In-Transit/Not Locked Light |
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| ELT Switch and Indicator |
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| Stabilator Trim Position Indicator |
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| Rudder Trim Position Indicator |
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| COCKPIT, FLIGHT AND GROUND CONTROLS |
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| Dual Primary Flight Controls |
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| Dual Hytrel Control Wheels |
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| Engine Controls-Pedestal Mounted with Friction Lock |
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• Throttle, Two |
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• Propellers, Two |
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• Mixture, Two |
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• Cowl Flap, Two |
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• Carburetor Heat, Two |
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| Enhanced Durability Throttle Cover and Placards |
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| Galvanized Control Cables |
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| Flight Trim Controls |
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• Rudder with Indicator |
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• Stabilator with Indicator |
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| Stall Warning Horn |
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| Steerable Nose Wheel, Cushioned |
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| Brakes |
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• Pilot's Toe Brakes |
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• Co-Pilot's Toe Brakes |
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• Parking Brake |
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| Landing Gear, Retractable Electrohydraulic |
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| Landing Gear Selector Switch |
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| Landing Gear Warning Horn |
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| Landing Gear Emergency Extension-Gravity Free Fall |
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| Main Wheels, 6.00 X 6 with Michelin H.D. Tires and Tubes, 8 Ply |
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| Nose Wheel, 5.00 X 5 with Michelin H.D. Tire and Tube, 6 Ply |
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| Wing Flaps Control, Manual, Four Positions (0, 10, 25 & 40 Degrees) |
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| Fuel Control Selectors with on/off/crossfeed |
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| ELECTRICAL SYSTEM |
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| 12 Volt, 35 Amp Hour Battery |
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| 14 Volt, Alternators-70 Amp, Two |
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| Master Switch Relay |
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| Alternator Control Units, Two |
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| Resettable Circuit Breakers |
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| Rocker Switches, Internally Lighted |
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| External Power Supply Receptacle |
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| Circuit Breaker Panel |
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| Static Discharge Wicks |
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| FUEL SYSTEM |
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| Two Fuel Tanks with 110 Gallons Total Capacity, |
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108 Gallons Usable |
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| Engine Driven Fuel Pumps, Two |
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| Auxiliary Fuel Pumps, Electric, Two |
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| Engine Primers, Electric, Two |
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| Fuel Tank Quick Drains, Two |
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| Fuel Sampling Bottle |
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| LIGHTING SYSTEMS |
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| External Lighting |
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• Landing/Taxi Lights, Two |
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• Wing Tip Recognition Lights, Two |
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• Navigation Lights |
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• Wing Tip Strobe Lights |
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• Tail Strobe Light, Low Profile |
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| Interior Lighting |
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• Instrument Panel Post Lighting |
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• Internally Lighted Switches |
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• Panel/Switch Dimming |
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• Overhead Blue Dome Light |
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• Overhead White Dome light |
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• Day/Night Dimming Switch |
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| CABIN COMFORT SYSTEM |
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| Janitrol 45,000 BTU Combustion Heater thermostatically |
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regulated by control on Co-Pilot instrument panel with |
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four floor air/heat outlets |
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| Heater Hour Recorder |
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| Heat Regulating Levers Front/Rear, Two |
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| Windshield Defrosters and Control |
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| Cabin Air Exhaust Vent |
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| Overhead Cabin Fresh Air Distribution Vents, four, single control |
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with individual deflectors, with fan system |
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| EXTERNAL FEATURES |
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| Exterior Paint - DuPont Imron in a wide choice |
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of color combinations |
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| Stainless Steel Cowl Fasteners |
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| Full Chemical Corrosion Protection |
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| Stowable Towbar |
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| Entrance Step |
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| Tie Down Rings, Three |
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| Jack Pads |
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| Nose Gear Safety Mirror |
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| Cowl Access Doors |
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| 12" Registration Numbers |
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| Cabin and Baggage Door Locks with Piper Logo Key |
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| COCKPIT AND CABIN APPOINTMENTS |
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| Overhead Cockpit Speaker |
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| Four Position Intercom System |
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| Pilot/Co-Pilot Seats - simulated leather, fore/aft and |
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vertically adjustable, with magazine storage pockets on |
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back of each seat |
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| Wall to Wall Carpeting and Headliner |
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| Crew Assist Hand Grips |
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| Armrests - Crew Area, Two |
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| Map Pocket |
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| Pilot’s Storm Window |
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| Scuff Pads, Pilot and Co-Pilot |
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| Tinted Windshield and Windows |
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| Sunvisors, Two |
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| Door Closing Strap |
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| Two Rear Passengers Seats |
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* Simulated Leather with Reclining Feature |
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| Seat Belts with Inertial Reel Harnesses, Four |
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| Soundproofing, Quietized |
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| Emergency Exit Window |
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| Luggage Compartments with Two Security Straps |
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| Rear Cabin Area (24 Cu. Ft., 200 Lbs.) plus a Hat Shelf |
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| Compass Card and Holder |
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| Halon Fire Extinguisher |
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| PRODUCT SUPPORT/DOCUMENTS |
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| Manufacturers Full Two Year Limited Warranty |
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| Pilot's Operating Handbook |
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| Aircraft Log Book |
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| Engine Log Book |
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| Certificate of Airworthiness |
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| Piper Warranty Form |
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| Inspection Forms |
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| Piper Key Chain |
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| Piper Flight Bag |
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| STANDARD GARMIN/S-TEC AVIONICS PACKAGE |
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| COMM/NAV/GS/GPS Multifunction Display |
GNS 430 |
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| VOR/LOC/GS/GPS Indicator |
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GI-106A |
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| Transponder with Traffic Information Sytem |
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GTX-330 |
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| Audio Panel with Marker Beacon and Intercom |
GMA 340 |
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| Altitude Encoder |
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| Avionics Master Switch |
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Piper |
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| Microphone |
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Telex 100T |
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| Headset |
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Airman 760 |
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| Speaker with Mic/Phone Jacks |
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| Automatic Emergency Locator Transmitter (ELT) |
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| Piper Aircraft, Inc. reserves the right to make changes in specifications, |
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| materials, equipment, or prices at any time without prior notice or to discontinue |
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| models as required. |
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Company
