| STANDARD EQUIPPED LIST PRICE |
$1,141,500 |
|
|
|
| ENGINE |
|
|
| Manufacturer |
|
Lycoming |
|
|
| Model |
|
TI0-540-AE2A |
|
|
| Thermodynamic Power |
|
350 hp |
|
|
| Number of Cylinders |
|
6 |
|
|
|
|
| PROPELLER |
|
|
| Manufacturer |
|
Hartzell |
|
|
| Number of Blades |
|
3 |
|
|
| Type |
|
Composite Constant Speed |
|
|
|
| WEIGHTS |
|
|
| Maximum Take-off Weight |
|
4,340 lbs/1,969 kg |
|
|
| Maximum Ramp Weight |
|
4,358 lbs/1,977 kg |
|
|
| Standard Equipped Weight |
|
3,153 lbs/1,433 kg |
|
|
| Standard Useful Load (a and b) |
|
1,205 lbs/548 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 |
|
43 ft/13.1 m |
|
|
| Length |
|
28.9 ft/8.8 m |
|
|
| Height |
|
11.3 ft/3.4 m |
|
|
| Cabin Length |
|
148 in/375.9 cm |
|
|
| Instrument Panel to Rear Bulkhead |
|
|
| Cabin Width |
|
49.5 in/125.7 cm |
|
|
| Cabin Height |
|
47 in/119.4 cm |
|
|
|
|
| WING AREA |
|
|
| Wing Area |
|
175 ft2/16.25 m2 |
|
|
|
|
| FUEL AND OIL CAPACITY |
|
|
| Usable Fuel |
|
120 gal/454 l |
|
|
| Oil Capacity |
|
12 qts/11.4 l |
|
|
|
|
| MAXIMUM SPEED TAS |
|
|
| Maximum Cruise Power |
|
220 kts/408 km/h |
|
|
|
|
| CRUISING RANGE TAS |
|
|
| Long Range Cruise Power |
|
1,345 nm/2,491 km |
|
|
| Cruising range includes 45 minute fuel reserve at long |
|
|
| range cruise power plus allowance for fuel used |
|
|
| during at optimum altitude and |
|
|
| stated mixture plus descent |
|
|
|
|
| STALL SPEED |
|
IAS |
|
|
| Flaps Extended 36º |
|
59 kias/109 km/h |
|
|
|
60 kcas/111 kn/h |
|
|
|
|
| SERVICE CEILING |
|
|
| 25,000 ft+/7,620+ m |
|
|
| 25,000 feet is the maximum |
|
|
| approved altitude for the Mirage |
|
|
|
|
| MAX DIFFERENTIAL PRESSURE |
|
|
|
5.5 psid |
|
|
|
|
| BAGGAGE |
|
|
| Volume |
|
|
| Forward Compartment |
|
13 ft3/0.37 m3 |
|
|
| Aft Compartment |
|
20 ft3/0.57 m3 |
|
|
|
|
| Capacity |
|
|
| Forward Compartment |
|
100 lbs/45.4 kg |
|
|
| Aft Compartment |
|
100 lbs/45.4 kg |
|
|
|
|
| TAKE-OFF DISTANCE |
|
|
| Ground Roll |
|
1,087 ft/331 m |
|
|
| Total over 50 ft Obstacle |
|
2,090 ft/637 m |
|
|
| Flaps 20º, Gross Weight |
|
|
|
|
| LANDING DISTANCE |
|
|
| Ground Roll |
|
1,020 ft/311 m |
|
|
| Total over 50 ft Obstacle |
|
1,968 ft/600 m |
|
|
|
|
|
|
| STANDARD EQUIPPED LIST |
|
|
| 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. |
|
|
|
|
| POWERPLANT AND PROPELLER |
|
|
| Engine - Lycoming TIO540-AE2A |
|
|
|
Dual Turbocharged, 350 HP at 2500 RPM, Direct Drive, 6 Cylinders, |
|
|
|
Fuel Injected, Dual Ignition with Shielded Ignition Harness |
|
|
| Pressurized Independent Magnetos, Two |
|
|
| Engine Mounts - Dynafocal Type with Internal Dampers |
|
|
| Starter, 24 Volt |
|
|
| Air Filter, Dry Type |
|
|
| Oil Filter, Full Flow |
|
|
| Oil Cooler with Thermostatic Control |
|
|
| Pneumatic Pumps - Dry, Continuous, Independent, Two |
|
|
| Inter-Coolers (Dual) |
|
|
| Alternate Induction Air with Manual Control |
|
|
| Oil Quick Drain |
|
|
| Propeller - Hartzell, 3 Blade |
|
|
|
Composite |
|
|
|
Constant Speed |
|
|
|
Polished Propeller Spinner |
|
|
| FLIGHT INSTRUMENTS AND INDICATORS |
|
|
| Avidyne FlightMax Entegra Flat Panel Display System |
|
|
| Pilot's and Co-Pilot's Electronic Primary Flight Displays (PFDs) |
|
|
| Displays all primary flight instruments on dual 10.4" screens |
|
|
| 10.4" Multi-Function Display |
|
|
| ● Large Screen Moving Map |
|
|
| ● Onboard weather radar |
|
|
|
| ● Trip summary |
|
|
|
| ● Nearest airports |
|
|
| ● Emax Engine Indicating System Displaying: |
|
|
|
Manifold Pressure |
|
|
|
RPM |
|
|
|
Turbine Inlet Temperature |
|
|
|
Fuel Flow |
|
|
|
Oil Temperature and Oil Pressure Indicator |
|
|
|
Cylinder Head Temperatures (6) |
|
|
|
L&R Fuel Quantity |
|
|
|
Fuel Management Including GPS Interface |
|
|
|
Percent Power |
|
|
|
Electrical System Performance |
|
|
|
Exceedence Monitoring and Recording |
|
|
|
|
|
| Magnetic Compass |
|
|
| Standby Mechanical Flight Instruments |
|
|
| Pitot/Static System |
|
|
| Alternate Static Source |
|
|
| Annunciator Panel (with Push to Test): |
|
|
|
• Alternator #1 Inop. |
• Fuel Pressure |
|
|
|
• Cabin Altitude |
• Alternator #2 Inop. |
|
|
|
• Door Ajar |
|
• Starter Engage |
|
|
|
• Oxygen |
|
• Vacuum #2 Inop. |
|
|
|
• Hydraulic Pump |
• Windshield Heat Fail |
|
|
|
• Fuel Imbalance |
• Boost Pump |
|
|
|
• Low Bus Voltage |
• Stall Warn Fail |
|
|
|
• Flaps |
|
• Vacuum #1 Inop. |
|
|
|
• Gear Warn |
• Annunciator Inop. |
|
|
|
• Pitot Heat Off/Inop. |
• Prop De-Ice Fail |
|
|
|
• Oil Pressure |
• Surface De-Ice |
|
|
| Hobbs Meter (Flight Time Recorder) |
|
|
|
|
| COCKPIT, FLIGHT AND GROUND CONTROLS |
|
|
| Primary Flight Controls, Dual Hytrel Control Wheels with Elevator Trim, |
|
|
| A/P Disconnect, CWS and Mic Buttons |
|
|
| Precise Flight Speed Brake System with Yoke Mounted Actuation Switch |
|
| and Panel Mounted Indication Lights. |
|
|
| Galvanized Control Cables |
|
|
| Engine Controls Pedestal |
|
|
|
• Throttle |
|
• Propeller |
|
|
|
• Mixture |
|
• Induction Alternate Air |
|
|
|
• Friction Lock |
|
|
| Flight Trim – Console |
|
|
|
• Elevator Trim with Indicator |
|
|
|
• Rudder Trim with Indicator |
|
|
| Stall Warning Computer and Horn |
|
|
| Steerable Nose Wheel |
|
|
| Brakes |
|
|
|
• Pilot & Co-Pilot’s Toe Brakes |
|
|
|
• Parking Brake |
|
|
| Landing Gear, Retractable Electrohydraulic with |
|
|
|
Emergency Extension Capability |
|
|
| Landing Gear Warning Horn |
|
|
| Wing Flaps, 0 To 36 Degrees - Electrically Operated with Pre-Select Feature |
|
| Wing Flap Position Indicator |
|
|
| Fuel Control Selector with off/left/right |
|
|
| Overhead Switch Panel containing: |
|
|
|
• Bar Guarded Starter |
• Landing Light |
|
|
|
• Taxi Lights/Pulse |
• Fuel Pump |
|
|
|
• Strobe Lights |
• Alternator #1 |
|
|
|
• Alternator #2 |
• Bar-Guarded Magneto |
|
|
|
Switches, Two |
|
|
|
• Battery Master |
• Digital Indicator Reset (Transicoil) |
|
|
|
• Navigation Lights |
• Normal/Dump Cabin Pressure |
|
|
|
• Day/Night Annunciator/Dim |
|
|
| Instrument Switch Panel Configuration including: |
|
|
|
• ADI/HSI Bezel |
|
|
|
• Environmental Control |
Switch Panel |
|
|
|
|
| ELECTRICAL SYSTEM |
|
|
| Dual, 28 Volt, 75 Amp Alternators |
|
|
| 24, Volt, 10 Amp Hour Battery |
|
|
| Master Switch Relay |
|
|
| Alternator Control Units |
|
|
| Resettable-Type Circuit Breakers |
|
|
| Back Lit Rocker Switches |
|
|
| Ground Clearance System |
|
|
| Avionics Master Switch |
|
|
| Truax Static Discharge Wicks |
|
|
| Cabin Overhead Speaker |
|
|
|
|
| FUEL SYSTEM |
|
|
| Integral Fuel Tanks |
|
|
| Capacity - 122 Gals. Total, 120 Gals. Usable |
|
|
| Engine Driven Fuel Pump |
|
|
| Electric Fuel Pumps, Centrifugal Type, Two |
|
|
| Emergency Fuel Pump |
|
|
| Fuel Tank Quick Drains, Two |
|
|
| Fuel Sampling Bottle |
|
|
| Flush Lockable Fuel Caps |
|
|
| Fuel Filter with Quick Drain |
|
|
|
|
| ICE PROTECTION SYSTEM AND PROVISIONS |
|
|
| Pneumatic Wing and Tail De-Icing |
|
|
| Pilot’s Heated Glass Windshield |
|
|
| Propeller De-icing, Electric |
|
|
| Heated Pitot Head |
|
|
| Heated Lift Detector |
|
|
| Ice Inspection Light |
|
|
|
|
| LIGHTING SYSTEMS |
|
|
| External Lighting |
|
|
|
• Nose Gear Landing Light |
|
|
|
• Navigation Lights |
|
|
|
• Wing Tip Strobe Lights |
|
|
|
• Low Profile Red Tail Flashing Light |
|
|
|
• Pulsating Wing Tip Taxi/Recognition Lights |
|
|
| Cockpit Lighting (Solid State Dimming) |
|
|
|
• Instrument Panel |
|
|
|
• Switch |
|
|
|
• Circuit Breaker Panel |
|
|
|
• Cockpit Dome Lights, Two |
|
|
| Cabin Lighting |
|
|
|
• Cabin Overhead/Reading Lights (Seven) |
|
|
|
• Courtesy Lights |
|
|
|
• Nose Baggage Lights |
|
|
|
• Cabin Entrance |
|
|
|
• Interior Baggage Compartments, Two |
|
|
|
|
| CABIN COMFORT SYSTEM |
|
|
| Bleed Air and Heater Muff provides heat to cabin area regulated by |
|
|
|
control on instrument panel with six floor heat outlets |
|
|
| Supplemental Electric Heater |
|
|
| Windshield Defrosters |
|
|
| Air Conditioning- HFC-134a Refrigerant Cycle System, Engine Driven |
|
|
|
Compressor with directional outlets at each seat |
|
|
| Enhanced Cabin Heating |
|
|
|
|
|
|
| EXTERNAL FEATURES AND ACCESSORIES |
|
|
| Polyurethane Exterior Finish |
|
|
| 12" Shadowed or Outlined Registration Numbers |
|
|
| Full Chemical Corrosion Protection |
|
|
| Cabin Entrance Door with Built-In Steps |
|
|
| Cabin Door Locking Pin Enhancement |
|
|
| Nose Baggage Compartment with Molded Door Seal |
|
|
| Exterior Storage Compartments, Two |
|
|
| Stowable Towbar |
|
|
| Stylized Cowling Exhaust Tunnels |
|
|
| Stainless Steel Access Fasteners |
|
|
| External Power Receptacle |
|
|
| Tie Down Rings, Three (Retractable on Wings) |
|
|
| Jack Pads, Two |
|
|
| Locks and Keys with Piper Logo |
|
|
|
|
| PRESSURIZATION SYSTEM |
|
|
| 5.5 psid Pressurization System |
|
|
| Cabin Altitude and Differential Pressure Indicator |
|
|
| Cabin Rate of Climb Indicator |
|
|
| Cabin Door Seal (Molded) |
|
|
| Cabin Outflow Pressure Regulating Valve |
|
|
| Cabin Pressure Safety and Dump Valve |
|
|
| Emergency Exit Pressure Seal (Molded) |
|
|
| Variable Rate Cabin Pressure Controller – Sea Level Controller |
|
|
| Cabin Altitude Warning Light |
|
|
| Emergency Oxygen System |
|
|
| COCKPIT AND CABIN APPOINTMENTS |
|
|
| Forward Refreshment/Entertainment Centers |
|
|
| Choice of Four Interior Colors |
|
|
| Leather Side Panels |
|
|
| Wall to Wall Carpeting |
|
|
| Improved Comfort Pilot/Co-Pilot Seats with increased head and leg-room, |
|
|
|
inflatable lumbar support, adjustable vertically, fore and aft, reclining, |
|
|
safety belts with inertia reel shoulder harness and stowaway armrests |
|
| Pilot/Co-Pilot and Passenger Intercom |
|
|
| Removable Carpet Floor Runner |
|
|
| Relief Tube |
|
|
| Accessory Power Point, 28 Volt |
|
|
| Emergency Exit |
|
|
| Pilot’s Storm Window |
|
|
| Cockpit Entry Hand Hold on Windshield Bow |
|
|
| Scuff Pads, Pilot and Copilot |
|
|
| Sun Visors, Two |
|
|
| Four Rear Passenger Seats, in club arrangement, reclining with |
|
|
|
inertia reel shoulder harness, safety belts and stowaway armrests |
|
|
|
with cabin light switches |
|
|
| Window Shades on passenger windows |
|
|
| Stowaway Executive Writing Table |
|
|
| Super Soundproofing, Quietized Inner Passenger Windows |
|
|
| Luggage Compartments with Security Straps |
|
|
| Halon Fire Extinguisher |
|
|
| Microphone with holder |
|
|
| Headsets for Passengers |
|
|
|
|
| PRODUCT SUPPORT/DOCUMENTS |
|
|
| Manufacturers Full Two Year Limited Warranty |
|
|
| Initial Pilot Training Slot (1) at SimCom International Inc. - VRB |
|
|
| Pilot’s Operating Handbook |
|
|
| Aircraft Log Book |
|
|
| Engine Log Book |
|
|
| Certificate of Airworthiness |
|
|
| Flight Bag |
|
|
| Piper Warranty Form |
|
|
| Inspection Form |
|
|
|
|
| STANDARD AVIONICS SYSTEM |
|
|
| Avidyne FlightMax Entegra Flat Panel Display System |
|
|
| Pilot's and Co-Pilot's 10.4" Primary Flight Displays (PFDs) Portraying Operational |
| and Navigation Flight Parameters |
|
|
| MultiFunction Display |
|
|
| ADAHRS: Dual Avidyne Air Data and Attitude Heading Reference System Integrated in |
|
|
| PFDs |
|
|
| Pilot Selectable for Revisionary Modes |
|
|
| Autopilot 'Pilot Priority' Feature |
|
|
| NAV/COMM/GS/GPS #1 Garmin GNS-430 with broad-band antenna |
|
|
| NAV/COMM/GS/GPS #2 Garmin GNS-430 with broad-band antenna |
|
|
| Audio Selector Panel GMA-340 with market beacon and stereo output for aft-four positions |
|
| Digital Transponder with Traffic Information System and Pilot Control Wheel Ident Button |
|
|
| Autopilot with automatic electric trim S-TEC System 55x |
|
|
| Flight Director bars |
|
|
| Integrated Altitude Pre-Selector (on PFD) |
|
|
| Weather Radar Allied Signal RDR-2000 Vertical Profile |
|
|
| Ground Clearance System |
|
|
| Pilot/Co-Pilot Control Wheel Mic Button |
|
|
| Pilot’s Transponder Ident Button |
|
|
| Mic/Phone Jacks and Overhead Speaker |
|
|
| Pilot’s Microphone |
|
|
| Automatic Emergency Locator Beacon |
|
|
|
|
| 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. |
|
|
Company
