曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Pressing the VFR key a second time will restore the previous
identification code.
FUNC Key
Pressing the FUNC key changes the data shown on the right side of
the display. Pressing the FUNC key a second time will cycle the
display to the next data. Displayed data includes Pressure Altitude,
Flight Time, Count Up Timer, Count Down Timer, Contrast, and
Display Brightness.
PRESSURE ALT - Displays pressure altitude in feet. An arrow to the
right of the altitude indicates that the airplane is climbing or
descending.
FLIGHT TIME - Displays the flight time. The timer receives
groundspeed from GPS1. Flight time starts when the groundspeed
reaches 35 knots on takeoff and pauses when the groundspeed
descends below 35 knots on landing.
COUNT UP TIMER - The count up timer is controlled by the START /
STOP key. Pressing the CLR key zeros the display.
Original: 12-26-00
8 of 8 P/N 11934-S12
Section 9 Cirrus Design
Supplements SR20
COUNT DOWN TIMER - The count down timer is controlled by the
START / STOP key. The CRSR and “0 - 9” keys are used to set the
initial time. Pressing the CLR key resets the timer to the initial value.
CONTRAST - Allows adjustment of display contrast. When
CONTRAST is selected, pressing the “8” key reduces contrast and
pressing “9” increases contrast.
DISPLAY - The display function is not available in this installation.
Display brightness is automatically controlled through a photocell in
the front panel.
Original: 12-26-00
P/N 11934-S20 1 of 24
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
For
S-Tec System 55X Autopilot w/
Altitude Selector/Alerter
When the S-Tec System Fifty Five X (55X) Autopilot with Altitude
Selector/Alerter is installed in the Cirrus Design SR20, serials 1268
and subsequent, this Supplement is applicable and must be inserted
in the Supplements Section (Section 9) of the Cirrus Design SR20
Pilot’s Operating Handbook. This document must be carried in the
airplane at all times. Information in this supplement adds to,
supersedes, or deletes information in the basic SR20 Pilot’s Operating
Handbook.
• Note •
This POH Supplement Revision dated Revision 04: 08-15-07,
supersedes and replaces Revision 03 of this supplement
dated 07-18-05.
Revision 04: 08-15-07
2 of 24 P/N 11934-S20
Section 9 Cirrus Design
Supplements SR20
Section 1 - General
This airplane is equipped with an S-TEC System 55X Autopilot. The
System 55X autopilot is a two-axis autopilot system. The system
consists of a flight guidance programmer/computer, altitude encoder,
altitude selector / alerter, turn coordinator, and HSI. Mode selection
and vertical speed selection is made on the programmer/computer
panel. A button on each control yoke handle may be used to
disengage the autopilot. The autopilot makes roll changes through the
aileron trim motor and spring cartridge and makes pitch changes for
altitude hold through the elevator trim motor. The SR20 installation of
the S-Tec System 55X Autopilot features:
• Heading Hold and Command;
• NAV/LOC/GPS/GS tracking, high and low sensitivity, and
automatic 45° course intercept;
• GPS Steering (GPSS);
• Altitude Pre-select, Hold and Command, Altitude display, and
baro correction;
• Altitude and Decision Height (DH) alert; and
• Vertical Speed Hold and Command.
Refer to S-Tec System Fifty-Five X Autopilot Pilot’s Operating
Handbook (POH): Serials 1005 thru 1336; P/N 87109 dated 8
November 2000 or later OR Serials 1337 and subsequent; P/N 87247
original release or later for full operational procedures and description
of implemented modes. The System 55X POH also contains detailed
procedures for accomplishing GPS & VOR course tracking, front
course and back course localizer approaches, and glideslope tracking.
Refer to S-Tec Altitude Selector / Alerter Pilot’s Operating Handbook
(POH) P/N 8716 or P/N 87110 (original issue or later) for full
operational procedures and detailed description of operational modes
of the Altitude Selector / Alerter.
• Note •
The SR20 implementation of the System 55X Autopilot does
not utilize the optional remote annunciator, roll servo, and
optional trim servo. Therefore, all references to these items in
the S-Tec System 55X POH shall be disregarded. Additionally,
Revision 04: 08-15-07
P/N 11934-S20 3 of 24
Cirrus Design Section 9
SR20 Supplements
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機(jī)信息手冊(cè)CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(106)