Piper PA-28-236 DAKOTA, Pilot Operating Handbook

Page: 300 / 367

SECTION 9 PIPER AIRCRAFT CORPORATION
SUPPLEMENT 9 PA-28-236, DAKOTA
REPORT: VB-910 ISSUED: JULY 23, 1982
9-50
SECTION 1 - GENERAL
This supplement supplies information necessary for the operation of the
airplane when the optional King KAP 150 Series Flight Control System is
installed. The Flight Control System must be operated within the limitations
herein specified. The information contained within this supplement is to be
used in conjunction with the complete handbook.
This supplement has been FAA Approved as a permanent part of this
handbook and must remain in this handbook at all times when the optional
King KAP 150 Series Flight Control System is installed.
SECTION 2- LIMITATIONS
(a) During autopilot operation, a pilot with seat belt fastened must be
seated at the left pilot position.
(b) The autopilot must be OFF during takeoff and landing.
(c) The system is approved for Category 1 operation only (Approach
mode selected).
(d) Autopilot flap limitation: Maximum flap extension 10° (first notch). ·
(e) Autopilot airspeed limitation: Maximum 155 KIAS.
NOTE
In accordance with FAA recommendation, use
of “altitude hold” mode is not recommended
during operation in severe turbulence.
SECTION 3- EMERGENCY PROCEDURES
(a) In case of Autopilot malfunction: (accomplish items 1. and 2.
simultaneously)
(1) Airplane Control Wheel - GRASP FIRMLY and regain aircraft
control.
(2) AP· DISC/TRIM INTER Switch - PRESS and HOLD.
(3) AP DISC/TRIM INTER Switch - RELEASE while observing
pitch trim wheel. If pitch trim wheel is in motion, follow the
Electric Trim Malfunction Procedure.