曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

the turn to capture the course begins is dependent upon closure rate
and airplane position. When the course is intercepted and the HSI
course deviation needle centered (indicating course capture), the
Revision 04: 08-15-07
P/N 11934-S13 15 of 16
Cirrus Design Section 9
SR20 Supplements
autopilot automatically initiates a tracking gain program to reduce turn
rate to 45% standard rate, and then 15% standard rate.
REV (Reverse Course) – When REV is selected, the autopilot will
automatically execute high sensitivity gain for an approach where
tracking the front course outbound or tracking the back course inbound
is required. The APR and REV annunciators will illuminate when REV
is selected.
APR (Approach) – When APR is selected, the autopilot provides
increased sensitivity for VOR or GPS approaches. APR may also be
used to provide increased sensitivity for enroute course tracking.
GS (Glideslope) - The autopilot GS function will capture and track an
ILS glideslope. To arm the GS function, the following conditions must
be met: (1) the NAV receiver must be tuned to the appropriate ILS
frequency; (2) The glideslope signal must be valid - no flag; (3) the
autopilot must be in NAV/APR/ALT modes; and (4) the airplane must
be 60% or more below the glideslope centerline during the approach
to the intercept point, and within 50% needle deviation of the localizer
centerline at the point of intercept - usually the outer marker. When the
above conditions have existed for 10 seconds, the GS annunciator will
illuminate indicating GS arming has occurred (ALT annunciator will
remain on). When the glideslope is intercepted and captured, the ALT
annunciator will go out.
ALT (Altitude Hold), Mode - When ALT is selected, the autopilot will
hold the altitude at the time the mode was selected. Altitude hold will
not engage if an autopilot roll mode is not engaged. Altitude correction
for enroute barometric pressure changes may be made by rotation of
the VS knob on the autopilot programmer/computer. Clockwise
rotation will increase and counterclockwise rotation will decrease
altitude 20 feet for each 'click.' The maximum adjustment is ±360 feet.
Adjustments greater than 360 feet can be made by selecting VS mode
and flying the airplane to the new altitude and then re-engaging ALT
mode.
VS (Vertical Speed) Mode - When VS is selected, the autopilot will
synchronize to and hold the vertical speed at the time the mode was
selected. Altitude hold will not engage if an autopilot roll mode is not
engaged. The vertical speed is displayed in 100-foot increments at the
far right of the programmer/computer window next to the VS
annunciation. A plus (+) value indicates climb and a negative or minus
Revision 04: 08-15-07
16 of 16 P/N 11934-S13
Section 9 Cirrus Design
Supplements SR20
(-) value indicates descent. Vertical speed can be adjusted by rotating
the VS knob on the programmer/computer. Clockwise rotation
increases and counterclockwise rotation decreases rate of climb (or
descent) 100 FPM for each 'click.' The maximum adjustment is ±1600
FPM.
Revision 04: 08-15-07
P/N 11934-S15 1 of 6
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
L-3 Avionics Systems SkyWatch
Traffic Advisory System
When the L-3 Avionics Systems SkyWatch 497 is installed in the
Cirrus Design SR20, this POH Supplement is applicable and must be
inserted in the Supplements Section (Section 9) of the appropriate
Cirrus Design 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 Pilot’s Operating
Handbook.
• Note •
This POH Supplement Revision dated 10-12-05 supersedes and
replaces the original release of this supplement dated 08-20-01.
Revision 01: 10-12-05
2 of 6 P/N 11934-S15
Section 9 Cirrus Design
Supplements SR20
Section 1 - General
This airplane is equipped with a L-3 Avionics Systems SkyWatch
SKY497 Traffic Advisory System to advise the pilot of transponderequipped
aircraft that may pose a collision threat. SkyWatch advisory
information is displayed on the GARMIN 430 display. The display
indicates relative range, bearing, and altitude of intruder aircraft. Aural
warnings are integrated into the airplane’s audio system.
Section 2 - Limitations
• WARNING •
SkyWatch can only detect aircraft that are equipped with
operating transponders.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 1148-126(106)