| STANDARD EQUIPPED LIST PRICE |
$1,896,500 |
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| ENGINE |
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| Manufacturer |
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Pratt & Whitney |
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Canada |
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| Model |
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PT6A-42A |
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| Thermodynamic Power |
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1090 SHP |
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| Climb Power |
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500 SHP |
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| Take-off Power(Flat Rated) |
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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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4 |
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| Type |
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Constant Speed, Reversible |
| Diameter |
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82 in/208 cm |
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| WEIGHTS |
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| Maximum Take-off Weight |
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5,092 lbs/2,310 kg |
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| Maximum Ramp Weight |
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5,134 lbs/2,329 kg |
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| Standard Equipped Weight |
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3,436 lbs/1,562 kg |
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| Standard Useful Load (a and b) |
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1,698 lbs/772 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/13.11 m |
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| Length |
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29.6 ft/9.02 m |
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| Height |
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11.3 ft/3.44 m |
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| Cabin Length |
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12.3 ft/3.75 m |
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| Instrument Panel to Rear Bulkhead |
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| Cabin Width |
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4.1 ft/1.25 m |
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| Cabin Height |
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3.9 ft/1.19 m |
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| WING AREA |
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| Wing Area |
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183 ft2/17.0 m2 |
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| FUEL AND OIL CAPACITY |
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| Useable |
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170 US gal/644 liters |
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| CRUISING SPEEDS TAS |
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| Maximum Cruise Power |
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260 kts |
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| CRUISING RANGE TAS |
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| Range with Full Fuel |
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1,000+ nm/1,885+ km |
| Full power climb to 30,000 ft max cruise power |
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| and descent with 45 minute reserves remaining |
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| (170 gal usable) |
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| ENDURANCE |
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| Endurance with Full Fuel |
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4.2 Hours |
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| Full power climb to 30,000 ft max cruise power |
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| and descent with 45 minutes reserve remaining |
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| RATE OF CLIMB |
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| @ MTOW 1,556 fpm |
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| STALL SPEED |
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| Flaps Extended 36º |
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69 kias/128 km/h |
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61 kcas/113 km/h |
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| SERVICE CEILING |
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| 30,000+ ft/9,144+ m |
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| 30,000 ft is the maximum approved |
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| altitude for the Meridian |
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| TAKE-OFF DISTANCE |
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| Ground Roll |
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1,650 ft/503 m |
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| Total over 50 ft Obstacle |
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2,438 ft/743 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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2,110 ft/643 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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| Pratt & Whitney Canada PT6A-42A Turboprop Engine |
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| Propeller - Hartzell Constant Speed, Reversible and |
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| Full Feathering |
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• Beta Switch with Warning Light |
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• Hydraulic Topping Governor |
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• Polished Propeller Spinner |
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• Woodward Overspeed Governor |
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| Bleed Air Pneumatic and Vacuum System |
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| Compressor Wash Ring |
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| Dust Covers - Engine Air Inlets and Exhaust Ports,with Propeller Locks |
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| Starter Generator, 28 Volt |
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| Engine Condition Trend Monitoring Capability (ECTM) |
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| Free Subscription to ECTM Service for One Year |
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| Fire Detection System |
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| Oil Cooler with Thermostatic Control |
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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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Torque |
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Interstage Turbine Temperature |
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Tachometer – Propeller (Np) |
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Tachometer – Gas Generator (Ng) |
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Oil Temperature |
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Oil Pressure |
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Fuel Totalizer |
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Rudder Trim |
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Vacuum |
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Outside Air Temperature |
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| Magnetic Compass |
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| Self-Dimming Annunciator Panel |
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| Standby Mechanical Flight Instruments |
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| Pilot’s Pitot/Static System |
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| Pilot’s Alternate Static Source |
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| Co-Pilot Pitot/Static System |
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| COCKPIT, FLIGHT AND GROUND CONTROLS |
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| Primary Flight Controls, Dual Hytrel Control Wheels with Electric |
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| Elevator Trim, A/P Disconnect, CWS and Mic Buttons |
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| Engine and Propeller Controls |
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• Single Power Lever |
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• Fuel Condition Lever |
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• Emergency Fuel Control Lever |
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| Flight Trim - Console |
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• Electric Rudder Trim with Digital Display on MFD |
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• Electric and Manual Elevator Trim |
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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'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 |
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| Emergency Extension Capability |
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| Landing Gear Warning Horn with Mute Switch |
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| Wing Flaps, Electrically Operated with Pre-select Feature |
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| Wing Flap Position Indicator |
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| Overhead Switch Panel Containing: |
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• Engine Switches |
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• Electrical Switches |
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• De-Ice Switches |
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• Lighting Switches |
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| Environmental Switch Panel |
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| ELECTRICAL SYSTEM |
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| Battery – 24 Volt, 38 AMP/Hour |
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| Generator – 28 Volt, 200 AMP |
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| Alternator – 28 Volt, 135 AMP |
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| External Power Supply Receptacle – 28 Volt AN Type |
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| Voltage Regulator |
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| Generator Control Unit (GCU) |
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| Resettable-Type Circuit Breakers |
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| Digital Ammeter/Voltmeter |
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| Static Discharge Wicks |
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| FUEL SYSTEM |
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| Integral Fuel Tanks |
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| Fuel Shutoff Valve |
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| Engine Driven Fuel Pump |
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| Electric Fuel Pumps |
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| Fuel Filter with Bypass |
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| Fuel Tank Drains |
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| Fuel Sampling Bottle |
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| Flush Fuel Caps |
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| Reduced Operational Temperature Fuel System |
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| Fuel Temperature Indicator |
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| ICE PROTECTION SYSTEM AND PROVISIONS |
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| Dual Engine Air Inlets and Inertial Separators |
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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, Pilot and Co-Pilot |
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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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• Pulsating Wing Tip Taxi/Recognition Lights |
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• Navigation Lights |
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• Wing Tip Comet Strobe Lights |
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| Cockpit Lighting (Solid State Dimming) |
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• Avionics |
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• Instrument Panel, Switch and Circuit Breaker Panel |
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• Cockpit Dome Lights |
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| Cabin Lighting |
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• Cabin Overhead Lights |
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• Courtesy Lights |
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• Cabin Entrance Lights |
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• Interior Baggage Compartment Lights |
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| CABIN COMFORT SYSTEM |
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| Bleed Air Heat to Cabin |
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| Windshield Defrosters |
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| Air-Conditioning - HFC-134a Refrigerant Cycle System |
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| Cabin Air Vents for Heating, Ventilation and Cooling |
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| EXTERNAL FEATURES AND ACCESSORIES |
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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 Entrance Door with Built-In Steps |
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| Propeller Gust Lock |
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| Turbine Inlet Plugs |
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| Exterior Storage Compartments, Two |
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| Stainless Steel Access Fasteners |
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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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| 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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| 5.5 psid Pressurization System |
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| Automatic Emergency Pressurization System |
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| Cabin Altitude Warning Light |
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| Emergency Oxygen System |
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| Absolute Pressure Regulator |
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| COCKPIT AND CABIN APPOINTMENTS |
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| All Leather Seats |
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| Highly Durable Simulated 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 |
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leg-room, inflatable lumbar support, adjustable vertically, |
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fore and aft, reclining, safety belts with inertia reel shoulder |
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harness and stowaway armrests |
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| Pilot Relief Tube |
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| Emergency Exit |
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| Pilot's Storm Window |
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| Scuff Pads, Pilot and Co-Pilot |
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| Sunvisors |
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| Four Rear Passenger Seats, in club arrangement, reclining, |
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with inertia reel shoulder harness, safety belts and |
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stowaway armrests |
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| Window Shades on Passenger Windows |
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| Soundproofing, Quietized |
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| Double Pane Windows |
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| Cabin Accessible Luggage Compartment |
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| Halon Fire Extinguisher |
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| Stowaway Executive Writing Table |
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| PRODUCT SUPPORT/DOCUMENTS |
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| Full Two Year Factory 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 and Engine Log Books |
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| Certificate of Airworthiness |
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| Inspection Forms |
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| Flight Bag |
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| STANDARD AVIONICS SYSTEM |
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| Avidyne FlightMax Entegra Flat Panel Display System |
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• Pilot and Co-Pilot Electronic 10.4” Primary Flight Displays |
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Portraying Operational and Navigation Flight Parameters |
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• Multi-Function Display |
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• ADAHRS |
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Dual Avidyne Air Data and Attitude Heading Reference |
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System Integrated in PFDs |
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Pilot Selectable for Reversionary Modes |
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Autopilot ‘Pilot Priority’ feature |
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| NAV/COMM/GS/GPS #1 |
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GNS-430 with Broad Band Antenna |
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| NAV/COMM/GS/GPS #2 |
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GNS-430 with Broad Band Antenna |
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| 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 with Traffic Information System and Pilot Control |
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Wheel ldent Button |
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| Autopilot |
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S-Tec Magic 1500 Automatic Flight Control System with: |
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• Digital Attitude Based |
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• Integrated Altitude Preselector and Alerter |
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• IAS-Indicated Airspeed Mode |
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• Integrated Yaw Damper |
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• Voice Annuciations |
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| Weather Radar |
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Allied Signal RDR-2000 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
