Normal flight
When a wing drops in normal flight the AOA increases and the wing generates more lift so that there is a natural tendency to roll back and the aircraft stabilizes by itself.
Stalled flight ...
Normal Flight: All manÅ"uvres needed in ordinary flying, such as level climbing and gliding flight, turns and side-slipping, but excluding aerobatics.
Case 1: In normal flight, rolling motions are very heavily damped, as discussed in section 5.4.
If the helicopter starts to drift, the pilot should make corrections with the cyclic just as in normal flight. Drastic sideways drift that cannot be corrected with cyclic may require that the pedals be used to align the landing gear with the drift.
Out of unaccelerated normal flight, it is best to grasp the B-lines on both sides above the line links and pull them down. There is no need to release the toggles while B-stalling.
In normal flight they are at 0, and act simply as part of the wing. When extended the minimum (10 degrees) for takeoff, they increase the aircraft's lift-to-drag ratio and thus shorten the takeoff run (zero them when airborne).
Certain very normal flight situations can cause vertigo. The turning of a head, looking down and sideways, or up all when combined with a constant rate turn will create vertigo. The inner ear is a most fallible device.
In addition to undertaking their normal flight review every 24 months, CFIs must revalidate their instructor certification every 24 months. There were 87,816 flight instructors in 2003.
Airline Transport Pilots ...
POSITIVE LOAD FACTOR - During normal flight, the load factor is 1 G or greater than 1 G. Whenever the load factor is one or greater the load factor is defined as positive.
Aerobatics Maneuvers not necessary for normal flight, but used in air show, competition, or combat flying. Some example maneuvers would be loops, rolls, spins, and stall turns.
A surface that is used to stabilise the aircraft during normal flight e.g. the tail fin and tailplane. Other designs such as a V-tail may be used to provide both pitch and yaw stability.
Stability ...
Intentional maneuvers involving an abrupt change in an aircraft's altitude, and abnormal attitude, or abnormal acceleration not needed for normal flight.
LEADING-EDGE - The edge of an airfoil which first meets the airstream in normal flight.
LIFT - The force generated by an airfoil section, acting at right angles to the airstream flowing past it ...
A set of environmental or operational circumstances applicable to the airplane, combined with a failure or other emergency situation that results in a significant increase in normal flight crew workload.
Related Definitions from Aviation Glossary ...
This principle holds good even when have rear surfaces which actually are lifting s faces in normal flight, the requisite being that t wings themselves shall in such cases be at an ever greater angle than the tail.
aerodynamic surfaces on the leading edge of the wings of fixed aircraft which, when deployed, allow the wing to operate at a higher angle of attack. They are usually used while landing or performing maneuvers but are retracted in normal flight to ...
A softfield takeoff is an example of a max angle takeoff, but the airplane is barely flying and doesn’t give us much energy to fight gusts or crosswinds, so it’s not an appropriate technique for normal flight operations.
speed, so by deploying slats an aircraft can fly slower or take off and land in a shorter distance. They are usually used while landing or performing maneuvers which take the aircraft close to the stall, but are usually retracted in normal flight to ...
 See also: Flight, Power, Pilot, Plane, Aircraft
  
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