SAFE FLIGHT INSTRUMENT, LLC

Class 009: Wing leading edge lift transducer and cock-pit glare shield mounted indexer computer providing angle of attack

Wing leading edge lift transducer and cock-pit glare shield mounted indexer computer providing angle of attack for experimental aircraft

Automatic throttle control system for aircraft, namely, computers for controlling power output of aircraft engines; instruments used in aircraft automatic throttle systems; electronic controllers for engaging and disengaging automatic throttle systems for aircraft; control and display screens used in aircraft for automatic throttle system; systems for automatically maintaining a particular airspeed or engine setting in aircraft

Computers for managing aircraft engine thrust; [ Computers with dual monitors for managing aircraft control devices; ] Avionic instruments for measuring angle of attack of an aircraft in flight; Computers for warning of impending aircraft loss of lift and preventing loss of lift; Heater current monitor; Converters for translating aircraft angle of attack into different electrical formats; Avionic sensor systems, namely, processors for optimizing aircraft takeoff, climb and descent; Instruments for aligning aircraft angle-of-attack transducers, transmitters and sensors; [ Instruments used in aircraft automatic throttle systems including a processor for to prevent forces from the engine linkage from moving the throttles in the cockpit; ] Computers that warn of airflow downburst requiring corrective action; Automatic throttle control systems for aircraft; Electronic controllers for engaging and disengaging automatic throttle systems for aircraft; Autopower computer; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Control and display screens used for automatic throttle system for aircraft; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Avionic sensor systems, namely, processors for minimizing modification of throttle control assemblies in aircraft; Avionic sensor systems, namely, aircraft approach speed indicators; Avionic sensor systems, namely, aircraft speed control indicators; Avionic sensor systems, namely, instruments for indicating angle of attack of an aircraft in flight; Avionic sensor systems, namely, instruments for sensing angle of attack of an aircraft in flight; Avionic sensor systems, namely, processors for indicating angle of attack of an aircraft in flight; Ice detector; Optical ice detector; [ Sensors for detecting aircraft flap deflection angle; ] Computers for controlling aircraft performance; Avionic sensor systems, namely, processors for monitoring helicopter engine and rotor system and warning of maximum ratings for the engine, transmission or rotor system; Avionic sensor systems, namely, processors for monitoring and warning of aircraft operation near live transmission lines; Avionic sensor systems, namely, processors for converting antenna impedance; [ Avionic sensor systems, namely, processors for monitoring aircraft landing lights; ] Avionic sensor systems, namely, processors for optimizing aircraft performance in takeoffs, climbs, approaches and upset recovery; Avionic sensor systems, namely, processors for preventing aircraft stall; Avionic sensor systems, namely, processors for providing warning of impending aircraft stall; Horn used in aircraft for providing warning of impending aircraft stall; Horn assemblies for installation in aircraft cockpit

Computers for managing aircraft engine thrust; Computers with dual monitors for managing aircraft control devices; Avionic instruments for measuring angle of attack of an aircraft in flight; Computers for warning of impending aircraft loss of lift and preventing loss of lift; Heater current monitor; Converters for translating aircraft angle of attack into different electrical formats; Avionic sensor systems, namely, processors for optimizing aircraft takeoff, climb and descent; Instruments for aligning aircraft angle-of-attack transducers, transmitters and sensors; Instruments used in aircraft automatic throttle systems including a processor for to prevent forces from the engine linkage from moving the throttles in the cockpit; Computers that warn of airflow downburst requiring corrective action; Automatic throttle control systems for aircraft; Electronic controllers for engaging and disengaging automatic throttle systems for aircraft; Autopower computer; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Control and display screens used for automatic throttle system for aircraft; Avionic sensor systems, namely, processors for automatically maintaining a particular airspeed or engine setting; Avionic sensor systems, namely, processors for minimizing modification of throttle control assemblies in aircraft; Avionic sensor systems, namely, aircraft approach speed indicators; Avionic sensor systems, namely, aircraft speed control indicators; Avionic sensor systems, namely, instruments for indicating angle of attack of an aircraft in flight; Avionic sensor systems, namely, instruments for sensing angle of attack of an aircraft in flight; Avionic sensor systems, namely, processors for indicating angle of attack of an aircraft in flight; Ice detector; Optical ice detector; Sensors for detecting aircraft flap deflection angle; Computers for controlling aircraft performance; Avionic sensor systems, namely, processors for monitoring helicopter engine and rotor system and warning of maximum ratings for the engine, transmission or rotor system; Avionic sensor systems, namely, processors for monitoring and warning of aircraft operation near live transmission lines; Avionic sensor systems, namely, processors for converting antenna impedance; Avionic sensor systems, namely, processors for monitoring aircraft landing lights; Avionic sensor systems, namely, processors for optimizing aircraft performance in takeoffs, climbs, approaches and upset recovery; Avionic sensor systems, namely, processors for preventing aircraft stall; Avionic sensor systems, namely, processors for providing warning of impending aircraft stall; Horn used in aircraft for providing warning of impending aircraft stall; Horn assemblies for installation in aircraft cockpit

SERVO MOTOR, [ SERVO MOTOR/GENERATOR, TRANSFORMER, REACTOR, CHOKE, INDUCTOR, TRANSISTOR, RECTIFIER, CAPACITOR, RELAY, SWITCH, CHOPPER, ELECTRIC ANTIICING HEATER, ELECTRIC LIGHT, ] ELECTRIC MOTOR [, ELECTRICAL CONNECTOR, INSULATOR, SOCKET, CABLE, WIRE AND CHASSIS, TERMINAL BOARD, LIGHT FILTER, VIBRATION ISOLATOR, METAL COMPONENT CARD AND PRINTED CIRCUIT CARD ]; AERONAUTICAL AND NAVIGATIONAL INSTRUMENTS-, namely, LIFT DETECTORS, LIFT TRANSDUCERS, LIFT TRANSDUCER TEST GAUGE, LIFT TRANSDUCER TEST WEIGHT, LIFT TRANSDUCER ADAPTER UNIT, LIFT TRANSDUCER TEST SET, LIFT COMPUTER, LIFT COMPUTER ADJUSTMENT UNIT, LIFT COMPUTER ADJUSMENT UNIT ANALYZER, SIGNAL SUMMING UNIT, SIGNAL SUMMING AND RELAY UNIT, LIFT SIGNAL COMPARATOR, LIFT SIGNAL ANALYZER, SIGNAL SUMMING AND RELAY UNIT ADJUSTMENT UNIT, SPEED CONTROL INDICATOR/LIFT COMPUTER, SPEED CONTROL INDICATOR, SPEED COMMAND INDICATOR, INDICATOR FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, LANDING SPEED INDICATOR, LIFT RATIO INDICATOR, [ SPEED RATIO INDICATOR, ] LIFT SYSTEM TEST INDICATOR, LIFT SIGNAL CALIBRATOR, [ LIFT DATA COMPUTER, LIFT SIGNAL COMPARATOR, SIGNAL COMPARATOR, LIFT COUPLER, ] SPEED COMMAND COMPUTER, COMPUTER FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, [ COMPUTER CHARACTERIZATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER ACCELERATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, COMPUTER CALIBRATION MODULE FOR SPEED COMMAND OF ATTITUDE AND THRUST SYSTEM, ROTATION/GO-AROUND COMPUTER, ] FLAP POSITION POTENTIOMETER, FLAP POSITION TRANSMITTER, INSTRUMENT VIBRATOR, INSTRUMENT PANEL VIBRATOR, CONTROL SHAKER, COAXIAL CONTROL SHAKER, RUDDER PEDAL SHAKER, WARNING UNIT, DUAL WARNING UNIT, DUAL WARNING AND FLASHER UNIT, LANDING GEAR WARNING UNIT, [ COUNTER, PENDULOUS ACCELEROMETER, GROUND PLANE ACCELEROMETER, VERTICAL ACCELEROMETER, VERTICAL GYROSCOPE, THRUST TRANSDUCER, ] ABSOLUTE PRESSURE TRANSDUCER, DIFFERENTIAL PRESSURE TRANSDUCER, SERVO ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, CLUTCH ASSEMBLY, CLUTCH, REVERSE LOCKING CLUTCH, GEARBOX ASSEMBLY FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, AMPLIFIER FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, COMPUTER/AMPLIFIER FOR AUTOMATIC POWER CONTROL FOR AIRCRAFT, AIRSTREAM ANGLE SENSOR, AIRSTREAM ANGLE DATA COMPUTER, INDICATOR [, INSTRUMENT PANEL ADAPTER, MAGNETIC AMPLIFIER, SERVO AMPLIFIER, SERVO DISCONNECT, POTENTIOMETER, RESISTOR AND DIODE ]

Aircraft Instruments and Components Thereof, Including Lift Detector, Lift Transducer, Lift Computer, Lift Computer Adjustment Unit, Speed Control Indicator/Lift Computer, Lift Coupler, Lift Signal Comparator, Lift Signal Analyzer, Lift System Test Indicator, Lift Computer Adjustment Unit Analyzer, Lift Transducer Test Gauge, Lift Transducer Test Weight, Signal Summing Unit, Signal Summing and Relay Unit, Signal Summing and Relay Unit Adjustment Head, Adapter Unit, Signal Comparator, Flap Potentiometer, Flap Position Potentiometer, Flap Transmitter, Flap Position Transmitter, Flap Condition Transmitter, Flap Condition Potentiometer, Instrument Vibrator, Instrument Panel Vibrator, Control Vibrator, Control Shaker, Coaxial Control Shaker, Rudder Pedal Shaker, Control Shaker Striker Assembly, Instrument Panel Adapter, Pre-Stall Warning Unit, Gear Pre-Stall Warning Unit, Automatic Power Controller, Servo Amplifier, Ground Plane Accelerometer, Thrust Transducer, Anti-Icing Heater, Lift Signal Calibrator, Indicators, Gyroscope, Magnetic Amplifier, Transformer, [ Reactor, Choke, Inductor, Resistor, Potentiometer, Solid State Diode, Transistor, Rectifiers, Capacitor, Relays (Power, Sensitive, Polar, Nonpolar, and Time Delay), Switch, Chopper, ] Anti-Icing Electric Heater, [ Electric Lights, ] Electric Motor, Servo Motor, [ Counter, ] Servo Amplifier, Servo Disconnect, [ Vibration Isolator, Connector, ] Absolute Pressure Transducer, Differential Pressure Transducer [, Light Filter, Insulator, Socket, Cable, Wire, Chassis, Terminal Board ]