Flap and Slat Position Control Module
Landing Gear Controls
Bay Door Controls
Position Indicator (Door)
Rotor Pitch Controls
What Is A Throttle Control Module?
A throttle control module (TCM) on an airplane is a component in the cockpit that allows pilots to control the engine thrust by sending electronic signals to the engine's Full Authority Digital Engine Control (FADEC) system, essentially acting as the physical interface for adjusting power levels during flight; it's essentially the control unit for the throttle levers, enabling manual or automated engine power adjustments depending on the flight situation
What Is A Flap and Slat Position Control Module ?
A "flap and slat position control module" on an airplane is a computer system that manages the movement and position of the flaps and slats on the wings, essentially controlling how much lift is generated during takeoff and landing by adjusting the angle of these high-lift devices based on pilot input and flight conditions; it ensures proper coordination between the flaps and slats to optimize performance and safety.
What Is A Landing Gear Control ?
A "landing gear control" on an airplane is a switch or lever in the cockpit that allows the pilot to manually extend or retract the landing gear, essentially controlling when the wheels are down for landing or retracted during flight to reduce drag; it operates through a system of hydraulics and sensors to ensure the gear is properly positioned and locked in place.
What Is A Bay Door Control ?
"Bay door controls" on an airplane refer to the switches and mechanisms used to open and close the doors of a compartment within the aircraft, typically called a "bay," which is often used to store cargo, weapons (on military aircraft), or other equipment; essentially, it's the control system for accessing the bay doors on a plane.
What Is A Position Indicator On A Door ?
A "position indicator" for a door on an airplane is a visual or audible signal that tells the crew whether a particular door is fully closed, latched, and locked, essentially indicating its current position, usually displayed on the cockpit panel with lights or messages depending on the door's status.
What Is A Pitch Control ?
On a helicopter rotor, "pitch" refers to the angle of the blades relative to the plane of rotation, essentially how much the blades are tilted, which is controlled by the pilot to adjust the helicopter's lift and direction; it's the key factor in maneuvering the aircraft by changing the angle of attack of the blades throughout their rotation.