1. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

2. Questions / Comments

3. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

4. Flight Control Systems Adverse Yaw
This results in the aircraft yawing toward the wing which had experienced an increase in lift (and drag).
From the pilot’s perspective, the yaw is opposite the direction of the bank.

5. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

6. Flight Control Systems Adverse Yaw
Application of rudder is used to counteract adverse yaw.
The amount of rudder control required is greatest at low airspeeds, high angles of attack, and with large aileron deflections.

7. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

8. Flight Control Systems Adverse Yaw
Additionally, because more lift is required during a turn than when in straight-and-level flight, the angle of attack (AOA) must be increased by applying elevator back pressure.

9. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

10. Flight Control Systems T-Tail
In a T-tail configuration, the elevator is above most of the effects of downwash from the propeller as well as airflow around the fuselage and/or wings during normal flight conditions.

11. Warm-Up – 1/10 – 10 minutes
Utilizing your notes and past knowledge answer the following questions:
From a pilot’s perspective, what is the direction of the yaw and what do we refer to this type of motion?
How do you counter the effects of adverse yaw?
What must a pilot do to maintain steady altitude during a roll or bank of an aircraft?
In an aircraft with a T-tail configuration during normal flight conditions, what effects are removed from influencing the elevator?
At slow speeds, the elevator on a T-tail aircraft must be moved through a (larger or smaller) number of degrees of travel to raise the nose the same amount as on a conventional aircraft.

12. Flight Control Systems T-Tail
An additional benefit is reduced vibration and noise inside the aircraft.
At slow speeds, the elevator on a T-tail aircraft must be moved through a larger number of degrees of travel to raise the nose a given amount than on a conventional-tail aircraft.

13. Questions / Comments

14. THIS DAY IN AVIATION January 10
In The US Army announces the delivery of its first troop-transport gliders.

15. THIS DAY IN AVIATION January 10
In The Gulfstream III Spirit of America sets a round-the-world record for an executive jet of 43 hours, 39 minutes and 6 seconds in Taterboro, New Jersey.

16. THIS DAY IN AVIATION January 8
1982 — The Airbus A300 becomes the world's first wide-bodied airliner to be certified for operation by a flight crew of two.

17. Questions / Comments

18. January 2014 1 2 3 4 5 6 Chapter 5 Flight Controls
Sunday
Monday
Tuesday
Wednesday
Thursday
Friday
Saturday 1 2 3 4 5 6
Chapter 5 Flight Controls
Primary Flight Controls 7 8
Ailerons
Adverse Yaw Elevators 9 10
T-Tail
Stabilator
Quiz 11 12 13 14
Canards
Flaps 15 16
Trim Systems
Autopilot
Chapter TEST
Grades Due 17
NO SCHOOL 18 19 20 21 22
Chapter 6 Aircraft Systems 23 24 25 26 27 28 29 30 31

19. Questions / Comments

20. Chapter 5 – Flight Controls
FAA – Pilot’s Handbook of Aeronautical Knowledge

21. Today’s Mission Requirements
Identify in writing the flight control systems a pilot uses to control the forces of flight, and the aircraft’s direction and attitude.
Describe how the flight control systems and characteristics can vary greatly depending on the type of aircraft flown.
Describe in writing the basic flight control system designs.
EQ:
Describe the importance of Aeronautical Knowledge for the student pilot learning to fly.

22. Flight Control Systems T-Tail
This is because the conventional-tail aircraft has the downwash from the propeller pushing down on the tail to assist in raising the nose.

23. Flight Control Systems T-Tail
The forces required to raise the nose of a T-tail aircraft are greater than those for a conventional-tail aircraft.
The pilot must be aware that the required control forces are greater at slow speeds during takeoffs, landings, or stalls than for similar size aircraft equipped with conventional tails.

24. Flight Control Systems T-Tail
When flying at a very high AOA with a low airspeed and an aft CG, the T-tail aircraft may be susceptible to a deep stall.
In a deep stall, the airflow over the horizontal tail is blanketed by the disturbed airflow from the wings and fuselage.

25. Flight Control Systems T-Tail
In these circumstances, elevator or stabilator control could be diminished, making it difficult to recover from the stall.

26. Flight Control Systems Stabilator
A stabilator is a one-piece horizontal stabilizer that pivots from a central hinge point.

27. Flight Control Systems Stabilator
Because stabilators pivot around a central hinge point, they are extremely sensitive to control inputs and aerodynamic loads.
Antiservo tabs are incorporated on the trailing edge to decrease sensitivity.

28. Flight Control Systems Stabilator
They deflect in the same direction as the stabilator.
This results in an increase in the force required to move the stabilator, thus making it less prone to pilot-induced overcontrolling.

29. Questions / Comments

30. Chapter 5 Quiz Chapter 5 – Flight Controls Passcode 1369
FAA – Pilot’s Handbook of Aeronautical Knowledge
Chapter 5
Quiz
Passcode
1369