REDUNDANT FLIGHT CONTROL SYSTEM MANUAL

This is achieved by introducing novel approaches and methods for flight mechanics and control, mainly revolving around original implementations of traditional formulations of the Control Allocation (CA) problem. STOL kit installation (wing leading edge cuffs, drooped tips, stall fences, and aileron gap seals).The objective of the present dissertation is to show how redundant control surfaces can be exploited to shape an aircraft dynamic behavior and obtain desired flight mechanics performance.

Installation of Grimes aviation white anti-collision strobe light system two light or three light Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Installation of S-TEC System 55 two axis automatic flight guidance system, Model ST-563, with Installation of V25101 overvoltage sensor. Installation of an R25400 alternator control unit Installation of S-TEC System 65 two axis automatic flight guidance system, model ST-470.

REDUNDANT FLIGHT CONTROL SYSTEM MANUAL

Installation of S-TEC Manual Electric Trim System Model ST-447. Installation of an engine electronic tachometer, Model P-1000. (172N LANDING GEARĪuthorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator Installation of Aero Ski Manufacturing Co.

Installation of FluiDyne A2500A or AT2500A skis. Installation of PeeKay model 2300 or B2300 seaplane floats and associated hardware Installation of Auto-Vac-2 manifold vacuum system per certain engine STC's.Īdd sheet metal flap seals and/or flexible fabric aileron gap seals. Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. Leading edge cuffs, stall fences, aileron seals, wing tips. Installation of aileron and/or flap gap seals. Installation of Lompoc Aero Specialties inner plexiglass pane Installation strut/wing and strut/fuselage fairings, lightning hole covers, and aerodynamic putty. Installation of on-board engine analyzer system. Installation of an adjustable nine-inch trim tab on left aileron.Ĭontinental IO-360-K or KB engine installation rerated to 210 hp (2800 rpm) at takeoff and 195 Installation of a GDC 31 Roll Steering Converter Installation of airflow register into baggage compartment cover and insert a screened vent into Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems, Model Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3. Installation of hourmeter airspeed switch. For models 172I through 172P, a gross weight of 2350 Installation of Baumann Model BF2550A floats. Installation of aileron gap seal per Aircraft Development Co. Installation of flap gap seal per Aircraft Development Co. Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna Installation of replacement wing tip fairing assembly. Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Installation of Baumann Model BF-2550 floats. Includes provisions only for a push-to-talk (PTT) switch. Installation of replacement wing root vent described by Dwg Nos. Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Installation of replacement flap trailing edge bulbs. Installation of fiberglass replacement wing tips. GPS Steering Assist Module (SAM) with roll steering (p/n Installation of Centurion Consulting, Inc. Installation of carbon steel brake discs that have melonite surface treatment. Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. Installation of flap and aileron gap seals.įabrication of interchangeable float spreader bars. Approved in combination with SE1436CE which approves the Continental IO-360-K and –KB to 210 horsepower. SA1437CE Increases horsepower from 195 to 210. Performance STC Modifications R172K (‘HAWK XP)

Redundant flight control system