Piper PA-28-236 DAKOTA, Pilot Operating Handbook

Page: 286 / 367

SECTION 9 PIPER AIRCRAFT CORPORATION
SUPPLEMENT 8 PA-28-236, DAKOTA
REPORT: VB-910 ISSUED: JUNE 9, 1982
9-36
3. Heading Selector Knob - ROTATE Bug to the ILS front
course inbound heading.
NOTE
When BC is selected, the lateral operating mode
will change from HDG (if selected) to wings
level for 5 seconds. A 45° intercept angle will
then be established based on the position of the
bug.
If the D-Bar is greater than 2 to 3 dots: the autopilot will
annunciate HDG and BC modes with APR flashing;
when the computed capture point is reached the
HDG annunciator will go out, the APR annunciator
will illuminate steady and the selected course will be
automatically captured and tracked.
If the D-Bar is less than 2 to 3 dots: the HDG mode
will disengage upon selecting BC mode; the APR BC
annunciator will illuminate steady and the capture / track
sequence will automatically begin.
(7) Missed Approach
a. AP DISC/TRIM INTER - PRESS to disengage AP.
b. MISSED APPROACH - EXECUTE.
c. AP ENG Button - PRESS (if AP operation is desired). Note
AP annunciator ON.
(8) Before Landing
AP DISC/TRIM INTER - PRESS to disengage AP.
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.