Mooney M20V Acclaim Ultra, Руководство по эксплуатации для пилотов

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MOONEY
M20V ACCLAIM ULTRA
SECTION X
SAFETY INFORMATION
10 - 10
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
STANDARD PROCEDURE FOR SPIN RECOVERY
In the event of an inadvertent spin, the following recovery procedure should be used:
Throttle RETARD to IDLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Ailerons NEUTRAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rudder Apply FULL RUDDER opposite the direction of spin. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Control Wheel FORWARD of neutral in a brisk motion to break stall. . . . . . . . . . . . . . . . . . . . . .
Additional FORWARD elevator control may be required if rotation does not stop. . . . . . . . . . . .
Flaps (If extended)
RETRACT as soon as possible . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rudder NEUTRALIZE when spin stops. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Control Wheel Smoothly MOVE AFT to bring the nose up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
to a level flight attitude after spin has stopped. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
VORTICES - WAKE TURBULENCE
Every airplane generates wakes of turbulence while in flight. Part of this is from the propeller or
jet engine and part from the wing tip vortices. The larger and heavier the airplane the more
pronounced wake turbulence will be. Wing tip vortices from large heavy airplanes are very se-
vere at close range, degenerating with time, wind and space. These are rolling in nature from
each wing tip. In test, vortex velocities of 133 knots have been recorded. Exhaust velocities from
large airplanes at takeoff have been measured at 25 MPH, 2100 feet behind medium, large air-
planes.
Encountering the rolling effect of wing tip vortices within two minutes or less after passage of
large airplanes is hazardous to light airplanes. This roll effect can exceed the maximum counter
roll obtainable in an airplane.
The turbulent areas may remain for as long as three minutes or more, depending on wind condi-
tions, and may extend several miles behind the airplane. Plan to fly slightly above or to the up
wind side of the other airplane’s flight path.
Because of the wide variety of conditions that can be encountered, there is no set rule to follow to
avoid wake turbulence in all situations. However, the Aeronautical Information Manual goes into
considerable detail for a number of wake turbulence avoidance procedures. Use prudent judg-
ment and allow ample clearance time and space following or crossing the wake turbulence of
other airplanes in all takeoff, climb out, approach and landing operations. Be observant of wake
turbulence from all aircraft, regardless of size.
The Aeronautical Information Manual contains a section on wake turbulence. FAA Advisory Cir-
cular AC 90-23F is also recommended reading.
TAKE-OFF AND LANDING CONDITIONS
When taking off on runways covered with water or freezing slush, the landing gear should remain
extended for approximately ten seconds longer than normal, allowing the wheels to spin and
dissipate the freezing moisture. The landing gear should then be cycled up, then down, wait
approximately five seconds and then retract again. Caution must be exercised to assure that the
entire operation is performed below Maximum Landing Gear Operating Air speed.
Use caution when landing on runways that are covered by water or slush which cause hydro-
planing (aquaplaning), a phenomenon that renders braking and steering ineffective because of
the lack of sufficient surface friction. Snow and ice covered runways are also hazardous. The
pilot should be alert to the possibility of the brakes freezing.
Use caution when taking off or landing in gusty winds. Be aware of special wind conditions
caused by buildings or other obstructions located near runway in a crosswind pattern.