P/N 11934-S27
9 of 16
Cirrus Design
Section 9
SR20
Supplements
e.
Altitude Hold .................................................................... TEST
1.) Depress ALT button on autopilot programmer/computer.
Note that ALT annunciator comes on, VS annunciator
goes out, and yoke does not move.
f.
Overpower Test:
1.) Grasp control yoke and input left aileron, right aileron,
nose up, and nose down to overpower autopilot.
Overpower action should be smooth in each direction with
no noise or jerky feel.
g.
Radio Check:
1.) Turn on NAV1 radio, with a valid NAV signal, and select
VLOC for display on the PFD.
2.) Use autopilot programmer/computer to engage NAV
mode and move Course Select knob so that VOR
deviation needle moves left or right. Note that control
yokes follow direction of needle movement.
h.
Autopilot Disconnect Tests:
1.) Press Pilot A/P DISC/Trim Switch (control yoke). Note that
the autopilot disengages. Move control yoke to confirm
that pitch and roll control is free with no control restriction
or binding.
2.) Repeat step using Copilot A/P DISC/Trim Switch.
In-Flight Procedures
1.
Autopilot RDY Light ...................................................... CHECK ON
2.
Trim airplane for existing flight conditions.
3.
Engage desired mode by pressing mode selector button on
autopilot programmer/computer.
Heading Mode
1.
Begin by selecting a heading on PFD within 10° of the current
airplane heading.
2.
Press HDG button on autopilot programmer/computer. The HDG
annunciator will illuminate and the airplane will turn to the selected
heading.
Revision 2: 07-18-05
Summary of Contents for SR20
Page 10: ...1 2 P N 11934 003 Section 1 Cirrus Design General SR20 Intentionally Left Blank Revision A3 ...
Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...