MOONEY
M20V ACCLAIM ULTRA
SECTION III
EMERGENCY PROCEDURES
3 - 26
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS
-NOTE-
Loss of an engine parameter is indicated by a red X through the data field. Erro-
neous information may be identified by indications which do not agree with other
system information. Erroneous indications may be determined by comparing a
display with other displays and other system information.
1.
Set power based on throttle lever position, engine noise and speed.
2.
Monitor other indications to determine the health of the engine.
3.
Use
known
power
settings
in
the
for
approximate
fuel
flow
values.
4.
Use other system information, such as annunciator messages, fuel quantity and flow, to safely
complete the flight.
ERRONEOUS OR LOSS OF WARNING/CAUTION ANNUNCIATORS
-NOTE-
Loss of an annunciator may be indicated when engine or fuel displays show an
emergency situation and the annunciator is not present. An erroneous annuncia-
tor may be identified when an annunciator appears which does not agree with
other displays or system information.
1.
2.
If a display indicates an abnormal condition but no annunciator is present, use other system
information,
such
as
engine
displays,
fuel
quantity
and
flow,
to
determine
if
the
condition
ex-
ists.
If
it
cannot
be
determined
that
the
condition
does
not
exist,
treat
the
situation
as
if
the
condition
exists.
Refer
to
the
or
the
procedures
contained
in
this
AFMS.
LANDING GEAR
FAILURE OF LANDING GEAR TO EXTEND ELECTRICALLY
Airspeed
140 KIAS or less
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Landing Gear Actuator Circuit Breaker
PULL
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Landing Gear Switch
DOWN
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Manual Emergency Extension Mechanism
LATCH FORWARD/LEVER BACK
. . . . . . . .
to engage manual extension mechanism
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-NOTE-
Slowly pull “T” handle 1 to 2 inches (2.5 to 5.1 cm.) to rotate clutch mechanism
and allow it to engage drive shaft.
T- Handle
PULL (12 to 20 times)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
and RETURN until gear is down and locked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
GEAR DOWN light ILLUMINATED; STOP when resistance is felt
. . . . . . . . . . . . . . . . . . . . . . . . .
Visual Gear Down Indicator
CHECK ALIGNMENT
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
by viewing from directly above indicator
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Continuing to pull on T- Handle, after GEAR DOWN light ILLUMINATES, may bind
actuator; electrical retraction MAY NOT be possible until binding is eliminated by
ground maintenance. Return lever to normal position and secure with latch. Reset
landing gear actuator circuit breaker.
-CAUTION-
Do not operate landing gear electrically with manual extension system engaged. Do
not fly aircraft until maintenance/inspection is done on landing gear system.
-WARNING-
Revision A: 08-18-2017
