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

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PIPER AIRCRAFT CORPORATION SECTION 9
PA-28-236, DAKOTA SUPPLEMENT 11
ISSUED: OCTOBER 14, 1986 REPORT: VB-910
9-87
d. For navigation operations select modes as required by the
operation being conducted and in accordance with the mode
description provided in Section 7.1. For specific instructions
relating to coupled instrument approach operations, refer to
Special Operations and Information.
3. IN-FLIGHT PROCEDURE - COMMAND/AUTOTRIM SYSTEM
a. Trim master switch - ON.
b. When the autopilot is engaged, pitch trim is accomplished and
maintained automatically. 0
c. With the autopilot OFF, command trim is obtained by pressing
and rocking the combination TRIM-AP disconnect bar on the
pilot’s control wheel trim switch.
4. SPECIAL OPERATIONS AND INFORMATION
a. Altitude Hold Operation
For best results, reduce rate of climb or descent to 1000 FPM
before engaging altitude hold mode.
b. Flap Extension
For smooth control, changes in flap extension should be made one
notch at a time allowing time between changes for the airspeed to
stabilize.
c. Instrument Approach Operations
Initial and intermediate approach segments should be conducted
between 90-100 KIAS with flaps positioned 0° to full down
position. Upon intercepting the glide path or when passing the
final approach fix lower the landing gear and reduce power for
approximately 80-95 KIAS on the final approach segment. Adjust
power as necessary during remainder of approach to maintain
correct airspeed. Monitor course guidance information (raw data)
throughout the approach. All power changes should be of small
magnitude and smoothly applied for best tracking performance.
Do not change aircraft configuration during final approach while
autopilot is engaged. For approaches without glide path coupling,
adjust pitch attitude in conjunction with power to maintain desired
airspeed and descent rate.