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1. Traffic information shown on the GARMIN 430 displays is provided
as an aid in visually acquiring traffic. Pilots must maneuver the
aircraft based only upon ATC guidance or positive visual
acquisition of conflicting traffic.
2. If the pilot is advised by ATC to disable transponder altitude
reporting, the SkyWatch must be turned OFF.
3. The L-3 Avionics Systems SkyWatch Traffic Advisory System
Model SKY497 Pilot’s Guide P/N 009-10801-001 Rev B (6/6/00) or
later must be available to the pilot during flight with the SkyWatch
operating.
4. The GARMIN 400 Series Pilot’s Guide Addendum for “Display
Interface for Traffic and Weather Data” P/N 190-001140-10 Rev B
or later revision must be available to the pilot during flight with the
SkyWatch operating.
Section 3 - Emergency Procedures
No Change
Revision 01: 10-12-05
P/N 11934-S15 3 of 6
Cirrus Design Section 9
SR20 Supplements
Section 4 - Normal Procedures
After Engine Start
1. Avionics Power Switch ...............................................................ON
2. SkyWatch will turn on, complete a self-test, and then enter the
STBY mode.
• Note •
During the takeoff run, SkyWatch will automatically switch to
operational mode approximately 8 seconds after 35 KIAS is
achieved.
During the landing roll out, SkyWatch will automatically switch
back to STBY approximately 24 seconds after the airplane
slows to 35 KIAS or below.
Serials 1582 and subsequent: To minimize pilot distraction,
Skywatch system sensitivity will automatically be set to level B
(reduced) and aural warnings will be inhibited when flaps are
set to 50% and 100%.
3. Refer to the GARMIN 400 Series Pilot’s Guide Addendum for
“Display Interface for Traffic and Weather Data” P/N 190-001140-
10 Rev B for additional SkyWatch operational data not included in
this supplement.
Operator Initiated Control of SkyWatch
Self-Test
In addition to the power-up self-test, an automatic self-test is
performed several times each minute. If the SkyWatch is in STBY or
FAILED modes, an operator initiated self-test may be performed using
the GNS 430 controls as described below:
1. Rotate the small PUSH CRSR knob to select the Traffic / Weather
page.
2. From the Traffic Screen, press the MENU key to select the Menu
page.
3. Rotate the small PUSH CRSR knob to select SELF TEST and
then press the ENT key.
Revision 01: 10-12-05
4 of 6 P/N 11934-S15
Section 9 Cirrus Design
Supplements SR20
Switch to Normal from the Standby Screen
SkyWatch must be switched out of STBY to display traffic information.
The ability to switch out of STBY on the ground is useful for scanning
the airspace around the airfield prior to takeoff. Using the GNS 430
controls:
1. Turn the cursor on and highlight STBY.
2. Use the small PUSH CRSR knob to select OPER?
3. Press the ENT key to place SkyWatch in the OPER (operational)
mode. SkyWatch will switch into the 6 nmi display range.
Switch into Standby from the Traffic Screen
SkyWatch cannot be switched to Standby while airborne. With the
airplane on the ground, use the GNS 430 controls as described below:
1. Turn the cursor on and highlight OPER.
2. Use the small PUSH CRSR knob to select STBY?
3. Press the ENT key to place SkyWatch in the STBY (standby)
mode.
Change Altitude Display
1. From the Traffic Screen, turn the cursor on, highlight the current
mode, and use the small PUSH CRSR knob to cycle through the
options.
2. With each turn, the display changes to display the traffic in the
selected display range (ABV, look up; NRM, normal: BLW, look
down; or UNR, unrestricted). Refer to the L-3 Avionics Systems
SkyWatch Traffic Advisory System Model SKY497 Pilot’s Guide P/
N 009-10801-001 Rev B (6/6/00) or later for information regarding
the display ranges.
Respond to Traffic Advisories
1. When the SkyWatch issues a TA (Traffic Advisory), visually scan
outside for the intruder aircraft. Call ATC for Guidance. If you
visually acquire the intruder aircraft, use normal right-of-way
procedures to maintain separation.
• Note •
Revision 01: 10-12-05
P/N 11934-S15 5 of 6
Cirrus Design Section 9
SR20 Supplements
Do not maneuver solely on traffic information shown on the
display. Information shown on the display is provided as an aid
in visually acquiring traffic - It is not a replacement for ATC and
See & Avoid techniques.
Section 5 - Performance
No Change
Section 6 - Weight & Balance
　
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本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 1148-126(107)