| 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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1029 SHP |
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| Climb Power 500
SHP |
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500 SHP |
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| Take-off Power(Flat Rated) |
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500 SHP |
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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 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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| Prices and
Equipment |
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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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| Scuff Pads, Pilot
and Co-Pilot 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. |
Company
