Mooney M20TN S type, Руководство по эксплуатации для пилотов

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MOONEY
M20TN - MODEL TYPE-S
SECTION III
EMERGENCY PROCEDURES
3 -- 20
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE -- 04-02-2008
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 POH Chapter V 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
abnormal or emergency situation and the annunciator is not present. An erro-
neous annunciator may be identified when an annunciator appears which does
not agree with other displays or system information.
1. If an annunciator appears, treat it as if the condition exists. Refer to the POH/AFM Emergency
or Abnormal procedures or the procedures contained in this AFMS.
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 POH/AFM Emergency or Abnormal procedures or the proce-
dures 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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
--CAUTION--
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. Re-
set landing gear actuator circuit breaker.
--WARNING--
Do not operate landing gear electrically with manual extension system engaged.
Do not fly aircraft until maintenance/inspection is done on landing gear system.