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3. Rotate the small PUSH CRSR knob to select SELF TEST and
then press the ENT key.
Revision 02: 03-27-07
4 of 6 P/N 13772-111
Section 9 Cirrus Design
Supplements SR22
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 02: 03-27-07
P/N 13772-111 5 of 6
Cirrus Design Section 9
SR22 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
SkyWatch adds the following optional (Sym = O) equipment at the
weight and arm shown in the following table.
Section 7 - Systems Description
The SkyWatch model SKY497 is an airborne Traffic Advisory System
(TAS). SkyWatch monitors a radius of approximately 6 nautical miles
around the aircraft by interrogating transponders in the monitored area
and determining if a collision threat exists. To determine if a collision
threat exists, SkyWatch calculates the range, altitude, bearing, and
closure rate of all transponder equipped aircraft with the 6 nautical
mile range. When SkyWatch detects an intruder aircraft within.55
nautical mile horizontal distance and a ±800 ft relative altitude or
detects an intruder aircraft is on a course that will intercept the
SkyWatch airplane’s course within 20 seconds (non-altitude reporting
intruder aircraft) or 30 seconds (altitude reporting intruder aircraft),
SkyWatch will issue a Traffic Advisory (TA). Traffic Advisories are
indicated on the GNS 430 displays and aural “Traffic, Traffic” warnings
are announced in the headphones and cabin speaker.
ATA/
Item
Description Sym Qty Part Number
Unit
Wt
Arm
34-01 SkyWatch Inverter O 1 14484-001 0.5 118.0
34-02 SkyWatch Antenna Instl. O 1 14477-001 2.3 150.5
34-03 SkyWatch Track Box O 1 14477-050 10.0 140.0
34-04 SkyWatch Wiring Instl O 1 14479-001 2.0 145.0
Revision 02: 03-27-07
6 of 6 P/N 13772-111
Section 9 Cirrus Design
Supplements SR22
Aircraft Serial Numbers 0002 thru 2344 after installation of L3 Service
Bulletin SB805-10800-204, and Serial Numbers 2345 and
Subsequent, the SkyWatch® VIP system features extended aural
alerts of range, bearing and relative altitude. In addition, the number of
targets able to be displayed on the MFD simultaneously, will increases
from 8 to 10.
SkyWatch may be pilot controlled through the GNS 430 controller.
STBY (standby), OPER (operational), and SELF TEST modes as well
as altitude display (ABV, look up; NRM, normal: BLW, look down; or
UNR, unrestricted) can be selected.
The SkyWatch System consists of a Transmitter Receiver Computer
(TRC) installed under the copilot’s seat just forward of the spar tunnel
and a directional antenna installed on the airplane exterior above the
cabin. The system also utilizes inputs from the altitude encoder, the
　
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