wright aviation services llc presents piper meridian systems training program flight controls...
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Wright Aviation Services LLCPresents
Piper MeridianSystems Training Program
Flight Controls2011©WrightAviationServicesLLC
All rights reserved
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PA46-500TP Meridian
FlightControls
Overview
Primary Flight Controls: Elevator, Rudder and Ailerons are conventional, utilizing dual control wheels and foot pedals that are manually activated and mechanically actuated through a series of levers, cables, pulleys, push/pull rods and bellcranks to provide pitch, roll and yaw control.Note: Rudder/Aileron are interconnected through a spring system which activates only when these controls are out of harmony.
Secondary Flight Controls:Flaps: Electrically activated, mechanically actuated through jack screw, torque tube, push/pull rods and bellcranks.Pitch Trim: Electrically and manually activated, mechanically actuated through cables, pullies and bellcranks controlling a trailing edge trim tab.Yaw Trim: Electrically activated, mechanically actuated
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Rudder
PA46 Aircraft General
Meridian – PA46-500TP
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Rudder TrimTrim TabElectrically OperatedMechanically Activated
PA46-500TP Meridian
FlightControls
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PA46-500TP Meridian
FlightControls
Aileron Controls
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Elevator&
Elevator Trim
PA46-500TP Meridian
FlightControls
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PA46-500TP Meridian
FlightControls
Flaps
Single PieceFowler TypeElectrically OperatedMechanically Activated4 Positions
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FLAP DRIVE ASSEMBLY
28 volt flap motorJackscrewsPush/pull rodsBellcranks linkages Feedback Linkage
4 Position DetentsZero10 degrees25 degreesfull flaps
PA46-500TP Meridian
FlightControls
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PA46-500TP Meridian
FlightControls
Overview
Summary / ReviewPrimary Flight Controls:
Conventional rudder, elevator, aileron set up manually activated, mechanically actuated through cable, pullies and bellcranks.
Secondary Flight Controls:Flaps: Electrically activated, mechanically actuated through jack screw, torque tube, push/pull rods and bellcranks.Pitch Trim: Electrically and manually activated, mechanically actuated through cables, pullies and bellcranks controlling a trailing edge trim tab.Rudder trim: Electrically activated, mechanically actuated through cables, pullies and bellcranks controlling a trailing edge rudder trim tab.Yaw Trim: Electrically activated, mechanically actuated.
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Piper Meridian Presentation
By Wright Aviation
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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
1/10/11