PIPER AIRCRAFT CORPORATION
SECTION 9
PA-28-236, DAKOTA
SUPPLEMENT 11
ISSUED: OCTOBER 14, 1986
REPORT: VB-910
9-89
The Century 31 is activated with the aircraft master switch and operates
in a low power state until the autopilot is engaged. Mode selection is made
by pushing the desired mode switch on the mode programmer. The selected
mode will illuminate on the annunciator panel.
The annunciator panel contains an ambient light level sensor which will
automatically dim the annunciator light level during night operations. The
programmer contains mode recognition lights and dimming is provided by
the panel light dimmer switch.
The electric elevator trim system is a fully redundant type in both the
manual and auto trim modes. The trim system is powered through a separate
system master switch that must be ON during autopilot operations, and for
the control wheel trim command switch to function when the autopilot is
OFF.
Summary of Contents for PA-28-236 DAKOTA
Page 1: ......
Page 4: ......
Page 5: ...REPORT VB 910 ISSUED JUNE 1 1978 b...
Page 25: ...REPORT VB 910 ISSUED JUNE 1 1978 viii this page intentionally left blank...
Page 27: ...REPORT VB 910 ISSUED JUNE 1 1978 1 ii BLANK PAGE...
Page 41: ...REPORT VB 910 ISSUED JUNE 1 1978 2 ii BLANK PAGE...
Page 69: ...THIS PAGE INTENTIONALLY LEFT BLANK...
Page 99: ...THIS PAGE INTENTIONALLY LEFT BLANK...
Page 101: ...REPORT VB 910 ISSUED JUNE 1 1978 5 ii BLANK PAGE...
Page 197: ...REPORT VB 910 ISSUED JUNE 1 1978 7 ii THIS PAGE INTENTIONALLY LEFT BLANK...
Page 360: ...REPORT VB 910 ISSUED JUNE 1 1978 10 ii THIS PAGE INTENTIONALLY LEFT BLANK...
Page 363: ......
Page 364: ......
Page 365: ......
Page 366: ......
Page 367: ......