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CHEROKEE CRUISER
c.
EMERGENCY OPERATION
(1)
In an emergency the AutoControl can be disconnected by:
(a)
Placing the
AlP ONIOFF
switch to the "OFF" position.
(b)
Pulling the Autopilot circuit breaker (aircraft
SIN 28-7625001
through 28-7625275).
(2)
The AutoControl can be overpowered at either control wheel.
(3)
An Autopilot runaway, with a 3 second delay in the initiation of
recovery, while operating in a climb, cruise or descending flight could
result in a 60° bank and 100 foot altitude loss.
(4)
An Autopilot runaway, with a 1 second delay in the initiation of
recovery, during an approach operation, coupled or uncoupled, could
result in a 10° bank and 10 foot altitude loss.
3.
PERFORMANCE
No change.
REPORT: VB-557 PAGE 3-22
MODEL: PA-28-140
FAA APPROVED JUNE 13, 1974
REVISED: JULY 13, 1984
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