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forward of the rear window and a processor unit mounted under the aft
baggage floor. The antenna detects the electrical and magnetic fields
generated by intra-cloud, inter-cloud, or cloud to ground electrical
discharges occurring within 200 nm of the airplane and sends the
“discharge” data to the processor. The processor digitizes, analyzes,
and converts the “discharge” signals into range and bearing data and
communicates the data to the MFD every two seconds. The
Stormscope processor is powered 28 VDC through the 3-amp
STORMSCOPE circuit breaker on the Avionics Non-essential Bus.
Revision 1: 07-18-05
4 of 4 P/N 13772-110
Section 9 Cirrus Design
Supplements SR22
Revision 1: 07-18-05
Intentionally Left Blank
P/N 13772-111 1 of 6
Cirrus Design Section 9
SR22 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 SR22, 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 Revision 02: 03-27-07
supersedes and replaces the Revision 1 of this supplement dated 10-
12-05.
Revision 02: 03-27-07
2 of 6 P/N 13772-111
Section 9 Cirrus Design
Supplements SR22
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.
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 02: 03-27-07
P/N 13772-111 3 of 6
Cirrus Design Section 9
SR22 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 1602, 1644, 1663 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
　
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