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Wright Aviation Services LLCPresents
Aircraft Introduction
Piper PA46-500TPMeridian
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PA46 Initial Training
Aircraft General Aircraft Systems Performance Limitations Normal Procedures Emergency Procedures Weight and Balance Piper Operating Tips
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PA46 Aircraft General
Meridian – PA46-500TP
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PA46 Aircraft General
Meridian – PA46-500TPHigh Performance
PW PT6A-42A Turboprop
500 shp/continuousComplex Aircraft
fowler flaps4 blade constant
speed propretractable landing
gear Pressurized cabinService Ceiling* – 30,000 feetNormal Cruise – 265 KTASFuel – JetA / 170 gal usable5 to 6 placeNormal categorySingle engine landApproved for
Day/Night VFRDay/Night IFRKnown Icing
Conditions
*Note: Service Ceiling is 30,000 feet, however, it is not RVSM so the operating ceiling becomes FL280
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PA46 Aircraft GeneralMeridian – PA46-500TP
Airframe Structure• Low wing, semi-
monocoque • Primarily all metal
structure– Fiberglass & composite
in specific areas• Flush riveting & adhesive
bonds – Reduce drag– Increase strength– Reduce corrosion
exposure
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PA46 Aircraft GeneralMeridian – PA46-500TP
Dimensions Height – 11.3 ft/3.44mLength – 29.6ft/9.02m
Wingspan – 43.0ft/13.11mDihedral – 4.5 degrees
Horizontal Stab – 17ft/5.18m
Wheel stance – 12.33ft/3.76mGround stance – 2.25ft/0.68mTail Clearance – 5.25ft/1.6m
Prop Diameter – 6.9ft/2.1m
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PA46 Aircraft GeneralMeridian – PA46-500TP
• Fuselage– Nose & Aft sections
unpressurized– Center Section – Pressurized
• Nose Section– NLG assembly & Engine
Compartment
• Aft Section– Empennage– Equipment bay – ELT, VCCS
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PA46 Aircraft General
Meridian – PA46-500TP
Forward Section
Non-pressurized
Engine compartmentPT6A-42A
Engine accessories
Nose Landing Gear (NLG) Assembly
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PA46 Aircraft General
Meridian – PA46-500TP
Cabin Section
Cockpit or Flight DeckMain Cabin DoorOver wing Emergency ExitPilot Oxygen SystemCo-Pilot OxygenStorage CabinetCabin SeatingPassenger OxygenCabin LightingCabin VentsCabin CommunicationsBaggage CompartmentCabin SeatsPressure bulkheadsPilot/Co-Pilot WindscreensCrew Seats
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PA46 Aircraft General
Meridian – PA46-500TP
Aft Section
Non-Pressurized
Empennage AssemblyVertical
StabilizerRudder
AssemblyHorizontal
StabilizerElevator
Assembly
Equipment Bay
ELT
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PA46 Aircraft General
Meridian – PA46-500TP
Aircraft General
Max Gross Weight: 5092 lbsMax Landing Wgt: 4850 lbsMax Baggage Cap: 100 lbsSeating: 6 – Pilot/Co-pilot +4
Engine:Pratt & Whitney CanadaPT6a-42A500 SHPCompressor Turbine Speed (Ng)
38100 RPMsPropeller Speed (Np) 2000 RPMs
Propeller – Constant Speed:•Hartzell, E850B-3.5, 4 Blades•Diameter
81.5 inches minimum82.5 inches maximum
•Hydraulically actuated•Full feathering•Reversible type
Fuel: JET FUEL ONLYCapacity: 1160 pounds (173 gals)Usable: 1140 pounds (170 gals)Type: JETA or JETA-1Anti-Icing Additive: conforming to
MIL-I-27686Oil Capacity: 3 gallons (12 quarts)
Specs: See POH Sect 8.21
Cabin Information:Width: 49.5 inchesHeight: 47.0 inchesLength: 148 inches
Entry Door:Width: 24 inchesHeight: 46 inches
PA46 Aircraft GeneralMeridian – PA46-500TP
The fuselage of the Meridian is an all metal, semi-monocoque structure with flush riveted skin for reduced drag and corrosion resistance.
The Meridian fuselage has 3 major sections; the nose containing NLG assembly and engine compartment, the cabin section containing the flight deck , passenger and baggage areas and the aft section containing the empennage components and an equipment bay.
The pilot’s windshield is made of glass and should be cleaned only with mild soap and with a bare hand. The (DOOR AJAR) annunciator is activated by upper and lower microswitches located in the door frame. The emergency exit is located on the right side of the fuselage behind the copilot.
Review
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Section Quiz-Aircraft General
Aircraft General1-24
1. The fuselage of the Meridian is aA. Composite style fuselage with flush rivetingB. Completely fiberglass constructed with metal control surfacesC. All metal, semi-monocoque structure with flush riveted skinD. Steel construction with fiberglass and aluminum surfaces
2. The pilot’s windshield is made of glass and should only be cleanedA. With any aerosol spray and soft clothB. Never needs cleaningC. Any type cleaner is approved for useD. Only mild soap and with a bare hand
3. The (DOOR AJAR) annunciator is activated byA. The pilotB. Upper and lower microswitches located in the door frameC. Only a single micro switchD. Activates from a relay in the door handle
4. The emergency exit is locatedA. On the left side of the fuselage behind the pilot seatB. There is no emergency exit for the MeridianC. On the left rear fuselageD. On the right side of the fuselage behind the copilot
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PA46 Performance
Take-off Performance
Climb Performance
Cruise Performance
Landing Performance
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Normal takeoff: Flaps: zeroTemp: 29CPressure Alt: 1000 ftWeight: max grossHeadwind: 10 knotsRunway Gradient: 2° up
Rotation Speed:82 KIAS
Liftoff Speed:86 KIAS
Ground Roll:1850 ft
Clear 50’ Obstacle 2903 ft
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Climb Performance: Weight: maximum gross wgtOAT: 29 CPower: Max ContinousESC: NormalFlaps: RetractedGear: RetractedClimb Speed: 125 KIAS
Rate of Climb: 1459 fpmTime to FL 250: 20 minutesFuel to FL 250:152lbs/69kgDistance to Climb: 54 nm
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Cruise Endurance: Maximum Cruise Speed Flight Level: FL 250OAT: -15 CPower: Max CruiseTakeoff Fuel: 1139 lbs
Power Setting: 1147 ft/lbs torqueSpeed: 258 KTASFuel Burn: 250lbs/hr - 113.4 kg/hrCruise Endurance: 2:56 w/reserveRange w/IFR Reserve: 699 nm
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Cruise Endurance: Intermediate Cruise Speed Flight Level: FL 250OAT: -15 CPower: Max CruiseTakeoff Fuel: 1139 lbs
Power Setting: 900 ft/lbs torqueSpeed: 235 KTASFuel Burn: 206lbs/hr – 93.8 kg/hrCruise Endurance: 3:47 w/reserveRange w/IFR Reserve: 942 nm
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Decent Performance: From FL 250 to sea level Power Setting: 350 ft/lbs torqueCruise OAT: -20 CDescent Speeds: 174 KIASDescent Rate: 1506 fpm
Fuel Burn: 97 lbs / 22.7 kgTime to Descend: 16.6 minutesDistance covered: 60.2 nm
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PA46 PerformanceFor example & training only
Refer to your own aircraft Performance Information whenever making these calculations
Normal Landing: Flaps: full (36°)Temp: 25°CPressure Alt: 3500 ftWeight: max landingHeadwind: 10 knotsRunway Gradient: 2° up
Approach Power:
280 ft/lbsApproach Speed: 85 KIASTouchdown Speed: 78 KIASGround Roll:
2200 ftGrd Roll w/reverse:1043 ft
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PA46 Limitations
Air Speeds Air Speed Indicator Markings Power Plant limitations Propeller Engine Instrument Markings Fuel Starter Generator/Alternator/Electrical Power Control Chip Detection Weight and Balance Miscellaneous Kinds of Operations
Note: for limitations associated with your aircraft, refer to your aircraft Pilot Operating Handbook.
The Meridian limitations cover a wide range of things and these need to be considered whenever you are planning your operation. They include:
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PA46 Normal Procedures
Preflight Engine Start Before Take-off Take-off and Climb Cruise Descent Terminal Area Approach Approach to Land After Landing, Arrival & Securing
Your Meridian POH contain normal procedures in both checklist and expanded formats. Use of the checklist is essential to safe operations.
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PA46 Emergency Procedures
Power Plant Malfunctions & Failures Propeller Malfunctions & Failures Electrical System Malfunctions & Failures Cabin Pressure Malfunctions & Failures Avionics Malfunctions & Failures Fuel System Malfunctions Landing Gear Failures Flight Control Failures Anti-Ice System Failures Vacuum System Failures
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PA46 Weight & Balance
Procedures and principles are identical to all weight & balance exercises. This
can be accomplished using the charts, using a properly configured spreadsheet
or simply using the form, the tables and a calculator. During the flight portion of
the training, this will be covered in some detail.
The Envelope and Limitations
Weight & Balance Calculation Procedures
Planning Tools Available
Performance Considerations
Loading Recommendations
Configuration Variations
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PA46 Handling
General Ground Handling Hydraulic System Service Fuel and Oil Requirements Tire Inflation Battery Service Oxygen System Service Pressurization System Cleaning Interior, Exterior & Windows
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PA46 Servicing & Maintenance
Inspection Periods
Preventive Maintenance
Brake Servicing
Propeller Servicing
Fuel System Servicing
Alterations
Landings Gear Service
Lubrication
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Piper Operating Tips
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Piper Operating Tips
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Presented byWright Aviation Services LLC
Scottsdale/Phoenix AZCopyright 2010/2011 – Wright Aviation Services
All rights reservedWebsite: www.wrightaviation.net
Email: [email protected]: 480-203-0599
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Piper PA46 Meridian Presentation
By Wright Aviation
THE ENDwww.WrightAviation.net
480-203-0599