SAFE FLIGHT

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 ]