MOONEY
M20V ACCLAIM ULTRA
SECTION IV
NORMAL PROCEDURES
4 - 16
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
NORMAL DESCENT - GEAR DOWN
Seats, Seat Belts/Shoulder Harness
ADJUST AND SECURE
. . . . . . . . . . . . . . . . . . . . . . . . . . .
Wing Flaps
UP
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Power Settings
2400 RPM and approximately 25 inches Hg
. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed
140 KIAS or less
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Landing Gear
DOWN
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airspeed
164 KIAS or less
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Power Settings
AS REQUIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture
AS REQUIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOW Boost Pump
OFF Below 18,000 Ft.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rudder Trim
AS DESIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-NOTE-
Using landing gear as a descent aid will result in a steeper descent rate for a giv-
en power setting and airspeed. Alternatively, for a fixed descent rate more power
will be required. This can be helpful for maintaining minimum oil and cylinder
head temperatures. Plan for additional fuel consumption accordingly.
APPROACH FOR LANDING
The
airplane
must
be
within
allowable
weight
and
balance
envelope
for
landing
(REF.
SECTION
VI).
It
will
require
a
minimum
of
one
hour
of
flight
before
a
permissible
land-
ing
weight
is
attained
when
takeoffs
are
made
at
maximum
gross
weight.
If
landing
at
a
weight
exceeding
maximum
landing
weight
(3200
Lbs.)
(1452
Kgs.)
is
required,
see
.
-CAUTION-
Seats, Seat Belts/Shoulder Harness
ADJUST AND SECURE
. . . . . . . . . . . . . . . . . . . . . . . . . . .
Internal/External lights
AS DESIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Landing Gear
EXTEND below 140 KIAS
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Check Gear Down light ON- Check visual indicator)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture
FULL RICH (on final)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Propeller
HIGH RPM (on final)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel Boost Pump Switches
OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel Selector
FULLEST TANK
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Wing Flaps (below 110 KIAS in all extended positions)
T/O POSITION
. . . . . . . . . . . . . . . . . . .
(FULL DOWN)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
To minimize control wheel forces when entering landing configuration, timely nose- up
trimming is recommended to counteract nose down pitching moment caused by re-
duction of power and/or extension of flaps.
-CAUTION-
Elevator Trim
AS DESIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Rudder Trim
AS DESIRED
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Parking Brake
VERIFY OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-NOTE-
The parking brake should be rechecked to preclude partially applied brakes dur-
ing touchdown.
