Piper PA-28-236 DAKOTA, Руководство по эксплуатации для пилотов

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SECTION 9 PIPER AIRCRAFT CORPORATION
SUPPLEMENT 11 PA-28-236, DAKOTA
REPORT: VB-910 ISSUED: OCTOBER 14, 1986
9-88
NOTE
The autopilot will not decouple from the GS or
localizer in the event of radio failure, however,
warnings will flash in the mode appropriate to
the failure. Monitor course guidance raw data
during the approach to assure signal quality.
d. Instrument Approach Go-Around Maneuver
(1.) Disconnect the autopilot and manually control the aircraft.
(2.) Add takeoff power, or power as desired.
(3.) Check that correct attitude and that a positive rate of climb is
indicated, then raise gear and flaps.
(4.) Set the heading bug to the desired missed approach heading.
(5.) Re-engage the autopilot.
SECTION 5 - PERFORMANCE
No change.
SECTION 6 - WEIGHT AND BALANCE
Factory installed optional equipment is included in the licensed weight
and balance data in Section 6 of the basic Pilot’s Operating Handbook.
SECTION 7- DESCRIPTION AND OPERATION
The Century 31 Autopilot is a light weight electronic autopilot system
utilizing vertical and directional gyro signals and de electric servos to
provide three axis sensing and two surface control. The system includes
lateral and vertical radio coupling, command and automatic elevator trim;
and navigation and autopilot failure monitor and warning systems.