| STANDARD EQUIPPED LIST PRICE |
$1,141,500 |
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| ENGINE |
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| Manufacturer |
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Lycoming |
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| Model |
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TI0-540-AE2A |
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| Horsepower |
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350 hp |
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| Number of Cylinders |
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6 |
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| PROPELLER |
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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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Composite Constant Speed |
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| WEIGHTS |
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| Maximum Take-off Weight |
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4,340 lbs/1,969 kg |
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| Maximum Ramp Weight |
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4,358 lbs/1,977 kg |
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| Standard Equipped Weight |
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3,153 lbs/1,1433 kg |
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| Standard Useful Load (a and b) |
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1,205 lbs/548 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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43 ft/13.1 m |
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| Length |
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28.9 ft/8.8 m |
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| Height |
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11.3 ft/3.4 m |
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| Cabin Length |
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148 in/375.9 cm |
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| Instrument Panel to Rear Bulkhead |
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| Cabin Width |
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49.5 in/125.7 cm |
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| Cabin Height |
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47 in/119.4 cm |
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| Headroom (Seat to Ceiling) |
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Front Seat |
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38in/96.5 cm |
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Middle Seats |
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38in/96.5 cm |
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Rear Seats |
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37in/94.0cm |
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| WING AREA |
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| Wing Area |
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175 ft2/16.25 m2 |
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| FUEL AND OIL CAPACITY |
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| Usable Fuel |
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120 gal/454 l |
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| Oil Capacity |
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12 qts/11.4 l |
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| MAXIMUM SPEED TAS |
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| TAS at Mid Cruise weight |
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220 kts/408 km/h |
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| CRUISING SPEEDS TAS |
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| High-speed cruise power |
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213 kts 394km/h |
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Mid-Cruise weight, optimum altitude |
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| CRUISING RANGE TAS |
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| Long Range Cruise Power |
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1,345 nm/2,491 km |
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| Cruising range includes 45 minute fuel reserve at long |
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| range cruise power plus allowance for fuel used |
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| during taxi, take-off, climb at maximum climb power, |
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| cruise at optimum altitude and stated mixture plus descent |
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| STALL SPEED |
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IAS |
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| Flaps Extended 36º |
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59 kias/109 km/h |
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60 kcas/111 kn/h |
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| SERVICE CEILING |
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| 25,000 ft+/7,620+ m |
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| 25,000 feet is the maximum |
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| approved altitude for the Mirage |
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| MAX DIFFERENTIAL PRESSURE |
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5.5 psid |
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| BAGGAGE |
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| Volume |
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| Forward Compartment |
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13 ft3/0.37 m3 |
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| Aft Compartment |
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20 ft3/0.57 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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1,087 ft/331 m |
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| Total over 50 ft Obstacle |
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2,090 ft/637 m |
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| Flaps 20º, Gross Weight |
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| LANDING DISTANCE |
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| Ground Roll |
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1,020 ft/311 m |
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| Total over 50 ft Obstacle |
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1,968 ft/600 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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| Engine - Lycoming TIO540-AE2A |
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Dual Turbocharged, 350 HP at 2500 RPM, Direct Drive, 6 Cylinders, |
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Fuel Injected, Dual Ignition with Shielded Ignition Harness |
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| Pressurized Independent Magnetos, Two |
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| Engine Mounts - Dynafocal Type with Internal Dampers |
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| Starter, 24 Volt |
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| Air Filter, Dry Type |
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| Oil Filter, Full Flow |
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| Oil Cooler with Thermostatic Control |
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| Pneumatic Pumps - Dry, Continuous, Independent, Two |
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| Inter-Coolers (Dual) |
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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 |
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Composite |
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Constant Speed |
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Polished Propeller Spinner |
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| FLIGHT INSTRUMENTS AND INDICATORS |
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| Avidyne FlightMax Entegra Flat Panel Display System |
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| Pilot's and Co-Pilot's Electronic Primary Flight Displays (PFDs) |
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Displays all primary flight instruments on dual 10.4" screens |
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10.4" Multi-Function Display |
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• Large screen moving map |
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• Onboard weather radar |
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• Trip summary |
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• Nearest airports |
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• EMax Engine Indicating System Displaying: |
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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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| Magnetic Compass |
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| Standby Mechnical Flight Instruments |
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| Pitot/Static System |
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| Alternate Static Source |
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| Annunciator Panel: |
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• Alternator #1 Inop. |
• Fuel Pressure |
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• Cabin Altitude |
• Alternator #2 Inop. |
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• Door Ajar |
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• Starter Engage |
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• Oxygen |
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• Vacuum #2 Inop. |
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• Hydraulic Pump |
• Windshield Heat Fail |
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• Fuel Imbalance |
• Boost Pump |
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• Low Bus Voltage |
• Stall Warn Fail |
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• Flaps |
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• Vacuum #1 Inop. |
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• Gear Warn |
• Annunciator Inop. |
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• Pitot Heat Off |
• Prop De-Ice Fail |
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- Left Pitot Heat |
- Right Pitot Heat |
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• Oil Pressure |
• Surface De-Ice |
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| Hobbs Meter (Flight Time Recorder) |
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| COCKPIT, FLIGHT AND GROUND CONTROLS |
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| Primary Flight Controls, Dual Hytrel Control Wheels with Elevator Trim, |
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| A/P Disconnect, CWS and Mic Buttons |
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| Precise Flight Speed Brake System with Yoke Mounted Actuation Switch |
| and Panel Mounted Indication Lights. |
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| Galvanized Control Cables |
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| Engine Controls Pedestal |
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• Throttle |
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• Propeller |
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• Mixture |
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• Induction Alternate Air |
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• Friction Lock |
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| Flight Trim – Console |
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• Elevator Trim with Indicator |
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• Rudder Trim with Indicator |
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| Stall Warning Computer and Horn |
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| Steerable Nose Wheel |
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| Brakes |
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Pilot & Co-Pilot's Toe Brakes |
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Parking Brake |
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| Landing Gear, Retractable Electrohydraulic with |
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Emergency Extension Capability |
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| Landing Gear Warning Horn |
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| Wing Flaps, 0 To 36 Degrees - Electrically Operated with Pre-Select Feature |
| Wing Flap Position Indicator |
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| Fuel Control Selector with off/left/right |
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| Overhead Switch Panel containing: |
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• Bar Guarded Starter |
• Landing Light |
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• Taxi Lights/Pulse |
• Fuel Pump |
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• Strobe Lights |
• Alternator #1 |
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• Alternator #2 |
• Bar-Guarded Magneto |
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Switches, Two |
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• Battery Master |
• Digital Indicator Reset (Transicoil) |
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• Navigation Lights |
• Normal/Dump Cabin Pressure |
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• Day/Night Annunciator/Dim |
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| Instrument Switch Panel Configuration including: |
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• ADI/HSI Bezel |
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• Environmental Control |
Switch Panel |
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| ELECTRICAL SYSTEM |
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| Dual, 28 Volt, 75 Amp Alternators |
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| 24, Volt, 10 Amp Hour Battery |
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| Master Switch Relay |
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| Alternator Control Units |
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| Resettable-Type Circuit Breakers |
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| Back Lit Rocker Switches |
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| Ground Clearance System |
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| Avionics Master Switch |
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| Truax Static Discharge Wicks |
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| Cabin Overhead Speaker |
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| FUEL SYSTEM |
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| Integral Fuel Tanks |
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| Capacity - 122 Gals. Total, 120 Gals. Usable |
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| Engine Driven Fuel Pump |
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| Electric Fuel Pumps, Centrifugal Type, Two |
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| Emergency Fuel Pump |
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| Fuel Tank Quick Drains, Two |
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| Fuel Sampling Bottle |
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| Flush Lockable Fuel Caps |
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| Fuel Filter with Quick Drain |
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| ICE PROTECTION SYSTEM AND PROVISIONS |
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| Pneumatic Wing and Tail De-Icing |
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| Pilot’s Heated Glass Windshield |
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| Propeller De-icing, Electric |
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| Heated Pitot Head |
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| Heated Lift Detector |
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| Ice Inspection Light |
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| LIGHTING SYSTEMS |
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| External Lighting |
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• Nose Gear Landing Light |
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• Navigation Lights |
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• Wing Tip Strobe Lights |
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• Low Profile Red Tail Flashing Light |
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• Pulsating Wing Tip Taxi/Recognition Lights |
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| Cockpit Lighting (Solid State Dimming) |
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• Instrument Panel |
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• Switch |
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• Circuit Breaker Panel |
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• Cockpit Dome Lights, Two |
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| Cabin Lighting |
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• Cabin Overhead/Reading Lights (Seven) |
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• Courtesy Lights |
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• Nose Baggage Lights |
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• Cabin Entrance |
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• Interior Baggage Compartments, Two |
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| CABIN COMFORT SYSTEM |
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| Bleed Air and Heater Muff provides heat to cabin area regulated by |
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control on instrument panel with six floor heat outlets |
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| Supplemental Electric Heater |
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| Windshield Defrosters |
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| Air Conditioning- HFC-134a Refrigerant Cycle System, Engine Driven |
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Compressor with directional outlets at each seat |
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| Enhanced Cabin Heating |
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| EXTERNAL FEATURES AND ACCESSORIES |
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| Polyurethane Exterior Finish |
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| 12" Shadowed or Outlined Registration Numbers |
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| Full Chemical Corrosion Protection |
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| Cabin Entrance Door with Built-In Steps |
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| Cabin Door Locking Pin Enhancement |
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| Nose Baggage Compartment with Molded Door Seal |
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| Exterior Storage Compartments, Two |
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| Stowable Towbar |
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| Stylized Cowling Exhaust Tunnels |
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| Stainless Steel Access Fasteners |
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| External Power Receptacle |
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| Tie Down Rings, Three (Retractable on Wings) |
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| Jack Pads, Two |
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| Locks and Keys with Piper Logo |
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| PRESSURIZATION SYSTEM |
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| 5.5 psid Pressurization System |
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| Cabin Altitude and Differential Pressure Indicator |
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| Cabin Rate of Climb Indicator |
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| Cabin Door Seal (Molded) |
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| Cabin Outflow Pressure Regulating Valve |
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| Cabin Pressure Safety and Dump Valve |
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| Emergency Exit Pressure Seal (Molded) |
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| Variable Rate Cabin Pressure Controller – Sea Level Controller |
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| Cabin Altitude Warning Light |
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| Emergency Oxygen System |
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| COCKPIT AND CABIN APPOINTMENTS |
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| Forward Refreshment/Entertainment Centers |
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| Choice of Four Interior Colors |
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| Leather Side Panels |
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| Wall to Wall Carpeting |
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| Improved Comfort Pilot/Co-Pilot Seats with increased head and leg-room, |
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inflatable lumbar support, adjustable vertically, fore and aft, reclining, |
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safety belts with inertia reel shoulder harness and stowaway armrests |
| Pilot/Co-Pilot and Passenger Intercom |
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| CD Player with Remote Control |
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| Removable Carpet Floor Runner |
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| Relief Tube |
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| Accessory Power Point, 28 Volt |
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| Emergency Exit |
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| Pilot’s Storm Window |
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| Cockpit Entry Hand Hold on Windshield Bow |
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| Scuff Pads, Pilot and Copilot |
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| Sun Visors, Two |
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| Four Rear Passenger Seats, in club arrangement, reclining with |
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inertia reel shoulder harness, safety belts and stowaway armrests |
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with cabin light switches |
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| Window Shades on passenger windows |
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| Stowaway Executive Writing Table |
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| Super Soundproofing, Quietized Inner Passenger Windows |
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| Luggage Compartments with Security Straps |
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| Halon Fire Extinguisher |
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| Microphone with holder |
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| Headsets for Passengers |
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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 Form |
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| Inspection Form |
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| STANDARD AVIONICS SYSTEM |
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| Avidyne FlightMax Entegra Flat Panel Display System |
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| Pilot's and Co-Pilot's 10.4" Primary Flight Displays (PFDs) Portraying Operational and Navigation Flight Parameters |
| MultiFunction Display |
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| ADAHRS: Dual Avidyne Air Data and Attitude Heading Reference System Integrated in PFDs |
| Pilot Selectable for Revisionary Modes |
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| Autopilot 'Pilot Priority' feature |
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| NAV/COMM/GS/GPS #1 |
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Garmin GNS-430 with Broad-Band antenna |
| NAV/COMM/GS/GPS #2 |
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Garmin GNS-430 with Broad-Band antenna |
| Audio Selector Panel |
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GMA-340 with Marker Beacon and Stereo Output for aft- four positions |
| Digital Transponder |
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GTX-330 |
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with Traffic Information System and Pilot |
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Control Wheel Ident Button |
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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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| Weather Radar |
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Allied Signal RDR-200 Vertical Profile |
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| Ground Clearance System |
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| Pilot/Co-Pilot Control Wheel Mic Button |
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| Pilot’s Transponder Ident Button |
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| Mic/Phone Jacks and Overhead Speaker |
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| Pilot’s Microphone |
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| Automatic Emergency Locator Beacon |
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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
