Piper Meridian Flight Controls Systems Training Program

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Presentation transcript:

Piper Meridian Flight Controls Systems Training Program Wright Aviation Services LLC Presents Piper Meridian Systems Training Program Flight Controls 2011©WrightAviationServicesLLC All rights reserved 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls 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 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46 Aircraft General Meridian – PA46-500TP Rudder 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls Rudder Trim Trim Tab Electrically Operated Mechanically Activated 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls Aileron Controls 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls Elevator & Elevator Trim 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls Flaps Single Piece Fowler Type Electrically Operated Mechanically Activated 4 Positions 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls FLAP DRIVE ASSEMBLY 28 volt flap motor Jackscrews Push/pull rods Bellcranks linkages Feedback Linkage 4 Position Detents Zero 10 degrees 25 degrees full flaps 1/10/11 Click Mouse to Advance Wright Aviation Services

PA46-500TP Meridian Flight Controls Overview Summary / Review Primary 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. 1/10/11 Click Mouse to Advance Wright Aviation Services

Click Mouse to Advance Wright Aviation Services Piper Meridian Presentation By Wright Aviation THE END 1/10/11 Click Mouse to Advance Wright Aviation Services

Presented by Wright Aviation Services LLC Scottsdale/Phoenix AZ Copyright 2010/2011 – Wright Aviation Services All rights reserved Website: www.wrightaviation.net Email: info@wrightaviation.net Phone: 480-203-0599 1/10/11 Click Mouse to Advance Wright Aviation Services