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EASA AD No.: 20150035E EASA EMERGENCY AIRWORTHINESS DIRECTIVE AD No.: 20150035E Date: 27 February 2015 Note: This Emergency Airworthiness Directive (AD) is issued by EASA, acting in accordance with
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How to fill out tail rotor pitch control

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How to fill out tail rotor pitch control:

01
Before starting, ensure that you have a thorough understanding of the helicopter's manual or manufacturer's instructions regarding the tail rotor pitch control system. Familiarize yourself with the components and their functions.
02
Begin by locating the tail rotor pitch control lever or knob inside the cockpit. This lever is usually located near the main collective control or on the center console.
03
Check the current position of the tail rotor pitch control lever. It should be in the neutral or zero position before making any adjustments.
04
To increase or decrease the tail rotor pitch, gently move the lever or knob in the appropriate direction. Typically, moving it forward or pushing it up will increase the pitch, while pulling it back or pushing it down will decrease the pitch.
05
It is important to make gradual adjustments to avoid sudden or extreme changes in the tail rotor pitch, which could affect the stability and maneuverability of the helicopter. Small increments are recommended, and you should constantly monitor the helicopter's response to the adjustments.
06
Once you have made the desired adjustments, double-check the tail rotor pitch control lever to ensure it is in the correct position that you intended. It should be secure and in a steady position.
07
It is crucial to perform a thorough pre-flight check before the helicopter takes off to ensure the tail rotor pitch control is properly filled out and functioning correctly. Look for any signs of wear, damage, or irregularities that may need immediate attention from a qualified technician.

Who needs tail rotor pitch control?

01
Helicopter pilots: Tail rotor pitch control is essential for helicopter pilots as it allows for precise control of the tail rotor's angle of attack. This control determines the thrust generated by the tail rotor and helps counteract the torque produced by the main rotor, thus maintaining the helicopter's stability and directional control.
02
Helicopter mechanics and technicians: These professionals need a comprehensive understanding of the tail rotor pitch control system to perform maintenance, inspections, and repairs. They ensure that the system is properly adjusted, lubricated, and functioning optimally to guarantee safe operations.
03
Helicopter manufacturers: Tail rotor pitch control is a critical component in helicopter design. Manufacturers develop and incorporate efficient and reliable systems to ensure optimal performance, safety, and controllability of their helicopters. They conduct extensive testing and research to improve the tail rotor pitch control systems over time.
In summary, understanding how to fill out tail rotor pitch control and who relies on this system is crucial for helicopter pilots, mechanics, technicians, and manufacturers alike. It ensures safe and efficient operation of a helicopter by maintaining stability, controlling torque, and allowing precise directional control.
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Tail rotor pitch control is a system used to adjust the pitch of the tail rotor blades on a helicopter in order to control the yaw or side-to-side movement of the aircraft.
Pilots or maintenance personnel responsible for the maintenance and inspection of the helicopter's tail rotor pitch control system are required to file this documentation.
To fill out the tail rotor pitch control documentation, individuals must provide accurate information about the maintenance, adjustments, and inspections carried out on the tail rotor pitch control system.
The purpose of tail rotor pitch control is to ensure the proper functioning and safety of the tail rotor system, which is essential for controlling the yaw of a helicopter.
Information such as maintenance records, adjustments made, inspection findings, and any issues identified with the tail rotor pitch control system must be reported.
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