General Emergency Procedures - Honeywell KFC 150 Pilot's Manual

Flight control system
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GENERAL EMERGENCY PROCEDURES
1. Disengage APPlaw Damp
a. Simultaneously regain control of
aircraft and hold down Autopilot
Disconnecflrim Interrupt button.
b. Pull
A/p
circuit breaker.
c. Release
A/p
Disconnecflrim
2. The
following conditions will cause AP to
Interrupt button.
automatically disengage:
a. External power failure.
b. Actuating manual electric trim.*
c. Internal Flight Control System failure.
d. With KCS 55A system, a loss of
compass valid (displaying HDG flag)
disengages the
AP
and FD when a
mode using heading information is
engaged. With compass flag
present, only
FD
and vertical modes
can be selected.
I
CAUTION: Exact Emergency Procedures
vary from aircraft to aircraft because of dif-
ferences in electrical systems, instrument
arrangements and flight characteristics.
Consult the Flight Manual Supplement for
your particular aircraft for detailed instruc-
tions on emergency procedures.
1
3 .
Engine Failure in Multiengine Aircraft
(COUPld)
a.
b.
C.
d.
Simultaneously control aircraft and
hold down Autopilot Disconnecvrim
Interrupt button.
Release button.
Follow basic Airplane Flight Manual
single engine procedures.
Airplane rudder and aileron axes
should be manually trimmed prior to
engaging autopilot for single engine
operations.
I
/
*If Trim Circuit Breaker has been pulled,
M.E.T. switch will not disengage AJP.
111

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Kap 100Kap 150

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