| STANDARD EQUIPPED LIST PRICE |
$573,500 |
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| ENGINE |
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| Manufacturer |
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Lycoming |
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| Model |
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TIO-540-AH1A |
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| Horsepower |
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300 hp |
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| Number of Cylinders |
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6 |
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| PROPELLER |
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| Manufacturer |
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Hartzell |
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| Number of Blades |
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3 |
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| Type |
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Constant Speed |
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| WEIGHTS |
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| Maximum Take-off Weight |
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3,600 lbs/1,633 kg |
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| Maximum Ramp Weight |
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3,615 lbs/1,640 kg |
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| Standard Equipped Weight |
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2,475 lbs/1,122 kg |
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| Standard Useful Load (a & b) |
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1,140 lbs/518 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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36.2 ft/11.0 m |
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| Length |
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27.9 ft/8.5 m |
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| Height |
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8.5 ft/2.6 m |
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| Cabin Length |
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124.25 in/315.6 cm |
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| Cabin Width |
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48.75 in/123.8 cm |
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| Cabin Height |
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42.0 in/106.7 cm |
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| Headroom (Seat to Ceiling) |
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Front Seats |
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38 in/96.5 cm |
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Middle Seats |
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35.75 in/90.8 cm |
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Rear Seats |
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34.50 in/87.6 cm |
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| WING AREA |
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| Wing Area |
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178.3 ft2/16.56 m2 |
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| FUEL AND OIL CAPACITY |
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| Usable Fuel |
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102 gal/386 liters |
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| Oil Capacity |
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12 qts/11.4 liters |
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| MAXIMUM SPEED TAS |
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| Maximum Cruise Power |
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187 kts/346 km/h |
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| CRUISING SPEEDS TAS |
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| High Performance |
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8,000 ft |
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172 kts/318 km/h |
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| Cruise Speed |
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10,000 ft |
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175 kts/324 km/h |
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15,000 ft |
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185 kts/342 km/h |
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| CRUISING RANGE TAS |
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| Cruising range includes 45 minute fuel reserve at |
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| long range power plus allowance for fuel used during |
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| taxi, take-off, climb at maximum climb power, cruise |
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| and descent |
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| Long Range |
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8,000 ft |
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950 nm/1,759 km |
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| Cruise Power |
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10,000 ft |
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948 nm/1,755 km |
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15,000 ft |
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945 nm/1,750 km |
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| STALL SPEED |
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| Flaps Full Down 40° |
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63 kias/117 km/h |
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61 kcas/113 kn/h |
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| MAXIMUM OPERATING ALTITUDE |
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| Maximum Operating Altitude |
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20,000 ft/6,096 m |
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| BAGGAGE |
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| Volume |
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| Forward Compartment |
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7 ft3/0.2 m3 |
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| Aft Compartment |
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17.3 ft3/0.49 m3 |
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| Capacity |
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| Forward Compartment |
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100 lbs/45.4 kg |
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| Aft Compartment |
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100 lbs/45.4 kg |
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| TAKE-OFF DISTANCE |
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| Ground Roll |
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1,110 ft/338 m |
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| Total over 50 ft Obstacle |
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1,810 ft/552 m |
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| LANDING DISTANCE |
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| Ground Roll |
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880 ft/268 m |
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| Total over 50 ft Obstacle |
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1,700 ft/518 m |
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| STANDARD EQUIPPED LIST |
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| Includes all listed standard equipment, FLY-AWAY-FACTORY (F.A.F.) |
| Vero Beach, FL. Dealer delivery and local taxes extra. |
| Piper Aircraft, Inc. reserves the right to make changes in |
| specifications, materials, equipment, or prices at any time without prior |
| notice or to discontinue models as required. |
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| POWERPLANT AND PROPELLER |
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| Engine-Lycoming TIO-540-AH1A 300 HP at 2500 RPM, |
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Turbocharged, Direct Drive, 6 Cylinder, Fuel Injection, |
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Dual Magnetos/Ignition with Shielding |
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| Dynafocal Engine Mounts with Internal Dampers |
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| Light Weight Geared Starter, 28 Volt |
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| Air Filter |
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| Full Flow Oil Coolers (Two) with Thermostatic Control |
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| Muffler and Exhaust System |
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| Alternate Induction Air with Manual Control |
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| Oil Quick Drain |
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| Propeller - Hartzell, 3 Blade, Constant Speed |
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| Polished Propeller Spinner |
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| FLIGHT INSTRUMENTS AND INDICATORS |
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| Avidyne Entegra Flat Panel Display System |
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| Primary Flight Display – Displays all required flight |
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| instrumentation and EHSI on 10.4" screen |
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• Solid State ADAHRS |
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• Attitude |
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• Airspeed |
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• Altitude |
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• Rate of Climb |
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• Primary Engine Guages (MAP, RPM, Oil Press and Fuel Flow) |
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• EHSI with Moving Map |
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• Outside Air Temperature |
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• Wind Vector |
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| Multi Function Display |
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• Moving Map |
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• Advanced Terrain Mapping |
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• E-Max Engine Indication System |
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• Trip Summary |
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| Engine Instrument Indicators – Displayed on MFD |
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• Manifold Pressure |
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• RPM |
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• Turbine Inlet Temperature |
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• Fuel Flow |
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• Oil Temperature and Oil Pressure Indicator |
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• Cylinder Head Temperatures (6) |
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• L & R Fuel Quantity |
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• Fuel Management including GPS Interface |
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• Percent Power |
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• Electrical System Performance |
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• Exceedence Monitoring and Recording |
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• Electrical System Performance |
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| AN Heated Pitot Head and Dual Flush Static Ports |
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| Alternate Instrument Static Source |
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| Engine Hour Recorder |
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| Annunciator Panel with Push-to-Test and Day/Night Switch |
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• Starter Engage |
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• Low Bus Voltage |
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• Alternator Inoperative |
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• Oil Pressure Low |
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• Nose Baggage Door Ajar |
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• Gear Warning |
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• Pitot Heat Inoperative/Off |
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• Flaps In Transit |
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• Air Conditioning Door Open (Optional) |
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• Strobe Lights |
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| COCKPIT, FLIGHT AND GROUND CONTROLS |
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| Primary Flight Controls, Dual Hytrel Control Wheels with Mic Buttons, |
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Pilot’s side Elevator Trim, A/P Disconnect and CWS Buttons |
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| Engine Controls-Pedestal with Friction Lock |
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• Throttle |
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• Propeller |
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• Mixture (with Lock) |
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| Alternate Induction Air |
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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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| Electric Elevator Trim Switch – Pilot Control Wheel |
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| Stall Warning Horn |
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| Steerable Nosewheel |
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| Heavy Duty Brake System |
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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 with Emergency |
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Extension Capability |
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| Landing Gear Warning Horn and Position Lights |
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| Main Wheels, 6.00 X 6 Tires and Tubes, 8 Ply |
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| Nose Wheel, 5.00 X 5 Tire and Tube, 6 Ply |
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| Wing Flaps, electrically operated |
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with four pre-selected positions (0, 10, 25 & 40 Degrees) |
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| Fuel Control Selector with off/right/left guarded OFF position |
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| Overhead Switch Panel: |
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• Bar Guarded Push to Start |
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• Battery Master |
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• Alternator |
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• Bar Guarded Electric Fuel Pump |
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• Bar Guarded Magneto Switches |
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• Landing/Recognition Lights |
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• Navigation Lights |
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• Strobe Light |
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| ELECTRICAL SYSTEM |
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| 24 Volt, 10 Amp Hour Battery |
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| 28 Volt, 90 Amp Alternator |
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| External Power Receptacle |
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| Master Switch Relay |
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| Alternator Control Unit |
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| Resettable-Type Circuit Breakers |
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| Back Lighted Rocker Switches, conveniently grouped on pilot's |
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instrument panel and overhead panel |
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| Static Discharge Wicks |
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| FUEL SYSTEM |
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| Two Interconnected Fuel Tanks per Wing with 107 Gallons Total |
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Capacity, 102 Gallons Usable |
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| Flush Lockable Fuel Caps |
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| Engine Driven Fuel Pump |
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| Electric Emergency Fuel Pump |
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| Fuel Quantity Gauge, Inboard Tanks, Two |
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| Fuel Tank Quick Drains, Two |
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| Fuel System Central Drain |
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| Fuel Sampling Bottle |
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| LIGHTING SYSTEMS |
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| External Lighting |
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• Wing Mounted Combination Landing and Recognition Lights |
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• Navigation Lights |
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• Wing Tip Comet Strobe Lights |
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• Low Profile Red Tail Strobe |
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| Cockpit Lighting |
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• Instrument Panel Lighting |
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• Avionics Dimming |
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• Overhead Map Lights |
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• Cockpit Entry Light |
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| Cabin Lighting |
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• Cabin Reading Lights, Four |
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• Forward Baggage Compartment Light |
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• Cabin Entry Light |
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| CABIN COMFORT SYSTEM |
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| Heater Muff, provides heat to cabin area, regulated by |
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control on panel with six floor heat outlets |
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| Windshield Defrosters and Control |
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| Cabin Air Exhaust Vents, Two |
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| Cabin Fresh Air Vents, six individually-controlled, overhead and |
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four individually-controlled, floor mounted |
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| Ventilation Fan with two speed settings |
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| EXTERNAL FEATURES |
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| Polyurethane Exterior Finish |
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| 12” Shadowed Registration Numbers |
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| Full Chemical Corrosion Protection |
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| Cabin Doors, Two-Cockpit (Right Forward) and Cabin (Left Rear) |
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| Tie Down Rings, Three (Retractable On Wings) |
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| Jack Pads |
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| Locks and Keys with Piper Logo |
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| Fore and Aft Cabin and Nose Baggage Doors, Lockable |
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| Utility Door for Rear Baggage Access and Cargo Loading |
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| Stowable Towbar |
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| Cockpit Entrance Step |
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| COCKPIT AND CABIN APPOINTMENTS |
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| Forward Cabin Door Single-Lever Locking System |
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| Choice of four 2005 Interior Colors which includes: leather seats, |
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designer side panels, wall to wall carpeting and headliner |
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| Pilot/Co-Pilot vertically adjustable seats with inflatable lumbar |
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support, magazine storage pockets on back of each seat with |
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headrests, fore/aft and tilting adjustment with inertial reels, |
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shoulder and safety belts |
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| Accessory Power Point, 28 Volt |
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| Pilot and Co-Pilot Stowable Armrests |
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| Map Pockets, Two |
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| Pilot's Storm Window |
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| Sunvisors, Two |
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| POH Holder |
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| Color Coordinated Throttle Quadrant and Center Console |
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| Scuff Pads, Pilot and Co-Pilot |
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| Tinted Windshield and Windows |
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| Window Shades on passenger windows |
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| Door Closing Strap, Aft Cabin |
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| Deluxe Six (6) Seats Lounge Interior Group with improved comfort |
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seats, headrests for all seats, club seating arrangements with |
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shoulder harness and seat belts, rear seats incorporate quick |
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release feature for easy removal, refreshment console with cup |
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holders, fold-down armrests on crew and rear seats and builtin |
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executive writing table |
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| Soundproofing, Quietized |
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| Luggage Compartments with Security Straps |
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| Rear Cabin and Hat Shelf Area, 17.3 Cu. Ft.- 100 Lbs. Capacity |
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| Fuselage Nose, 7.0 Cu. Ft. 100 Lbs. Capacity |
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| Compass Correction Card with 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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| Initial Pilot Training Slot (1) at SimCom International Inc. - VRB |
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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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| Flight Bag |
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| Piper Warranty/Inspection Form |
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| AVIDYNE STANDARD AVIONICS PACKAGE |
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| Primary Flight Display Avidyne |
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EXP5000 |
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| Multi Function Display Avidyne |
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EX5000 |
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| COMM/Nav/GS/GPS/#1 |
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Garmin-430 |
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| COMM/Nav/GS/GPS/#2 |
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Garmin-430 |
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| Autopilot with automatic electric trim |
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S-TEC System 55x |
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| Flight Director Bars |
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| Integrated Altitude Pre-Selector (on PFD) |
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| E-Max Engine Indicating System |
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| Stand-by Mechanical Flight Instruments |
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| Vacuum Pumps Removed – All electric airplane |
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| Audio Panel with Marker Beacon |
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Garmin GMA-340 |
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and Intercom |
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| Digital Transponder with Traffic |
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Garmin GTX-330 |
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Information System |
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| Altitude Encoder |
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| Control Wheel Mic Button |
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| Avionics Master Switch |
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| Microphone |
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Telex 100T |
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| Headset |
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Telex Airman |
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| Speaker with Mic/Phone Jacks |
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| Static Discharge Wicks |
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| PS Engineering Headsets (4) |
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| Automatic Emergency Locator Transmitter (ELT) |
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| Piper Aircraft, Inc. reserves the right to make changes in specifications, |
| materials, equipment, or prices at any time without prior notice or to discontinue |
| models as required. |
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Company
