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SECTION 9
SUPPLEMENT
7
SECTION I - GENERAL
PIPER AIRCRAFT CORPORATION
PA-28R-201, ARROW
This supplement supplies information necessary for the operation of the
(
airplane when the optional King KA P 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 - LIMIT A TlONS
A. During autopilot operation, a pilot with scat belt fastened must be
seated at the left pilot position.
R.
The autopilot must be OFF during takeoff and landing.
C. The system is approved for Category I operation only (Approach
mode selected).
D. Autopilot flap limitation: Maximum flap extension
100
(first
(.
notch).
E. Autopilot airspeed limitation: Maximum 170 KIAS.
NOTE
In accordance with FAA recommendation
(ACOO-24A), use of basic PITCH ALTITUDE
HOLD mode is not recommended during
operation in severe turbulence:
SECTION
3 -
EMERGENCY PROCEDURES
A. In case of Autopilot malfunction: (accomplish Items I and 2
simultaneously)
I.
Airplane Control Wheel - GRASP FIRMLY and regain
aircraft control.
'2,
AP D1SC/TRIM INTER Switch - PRESS and HOLD.
(
REPORT: VB-1365
ISSUED: SEPTEMBER 15. 1988
9-56,
2 of 28
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