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switch on the annunciator panel to prevent unwanted aural
alerting.
Section 4 - Normal Procedures
• Note •
Only vertical maneuvers are recommended responses to
warnings and alerts unless operating in VMC or the pilot
determines, using all available information and instruments,
that a turn, in addition to the vertical escape maneuver, is the
safest course of action.
During certain operations, warning thresholds may be
exceeded due to specific terrain or operating procedures.
During day VFR flight, these warnings may be considered as a
cautionary.
If the TAWS issues an alert when the Terrain Awareness
Display Page is not selected, a pop up message will appear
on the active display page of the MFD. To clear the alert, the
pilot must acknowledge the pop up message by pressing the
Soft Key next to the displayed “OK”.
Pilots are authorized to deviate from their current air traffic
control (ATC) clearance to the extent necessary to comply
with a TAWS warning.
Revision 01: 12-15-07
4 of 12 P/N 11934-S30
Section 9 Cirrus Design
Supplements SR20
Activate TAWS
• Note •
If the aircraft horizontal position derived from the Garmin
Navigator (GPS 1) is invalid, TAWS will be inoperative and the
TERR INOP annunciator will illuminate.
1. SKYWATCH/TAWS Circuit Breaker............................................. IN
2. MFD Circuit Breaker.................................................................... IN
3. Battery Master Switch ............................................................... ON
4. Avionics Power Switch .............................................................. ON
5. Verify TERR INOP Annunciator ...............................................OFF
6. At MFD prompt, any Key .....................................................PRESS
7. MFD Soft Keys .......................................................... SET to TAWS
Response To Ground Proximity Warnings
Aural “PULL UP” Warning
Red TERR WARN Annunciation
1. Level the wings, simultaneously adding full power.
2. Increase pitch attitude to 15 degrees nose up.
3. Adjust pitch attitude to ensure terrain clearance while respecting
stall warning. If flaps are extended, retract flaps to the UP position.
4. Continue climb at best angle of climb speed (Vx) until terrain
clearance is assured.
Aural “SINK RATE” Warning
Aural “DON’T SINK” Warning
Amber TERR CAUT Annunciation
1. Initiate appropriate corrective action to remove the cause of the
warning.
Revision 01: 12-15-07
P/N 11934-S30 5 of 12
Cirrus Design Section 9
SR20 Supplements
Response To Awareness Alerts
Aural “TERRAIN AHEAD” Alert
Aural “OBSTACLE AHEAD” Alert
Amber TERR CAUT Annunciation
1. Take positive corrective action until the alert ceases. Stop
descending, or initiate a climb turn as necessary, based on
analysis of all available instruments and information.
Aural “TERRAIN AHEAD; PULL UP” Alert
Aural “OBSTACLE AHEAD; PULL UP” Alert
Red TERR WARN Annunciation
1. Level the wings, simultaneously adding full power.
2. Increase pitch attitude to 15 degrees nose up.
3. Adjust pitch attitude to ensure terrain clearance while respecting
stall warning. If flaps are extended, retract flaps to the UP position.
4. Continue climb at best angle of climb speed (Vx) until terrain
clearance is assured.
Deactivate TAWS
1. SKYWATCH/TAWS Circuit Breaker........................................PULL
or
2. Avionics Power Switch .............................................................OFF
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
Installation of the Honeywell KGP 560 Terrain Awareness and Warning
System adds the following optional (Sym = O) equipment at the weight
and arm shown in the following table.
ATA /
Item
Description Sym Qty Part Number
Unit
Wt
Arm
34-01 KGP 560 Processor O 1 15963-001 1.25 117.0
Revision 01: 12-15-07
6 of 12 P/N 11934-S30
Section 9 Cirrus Design
Supplements SR20
Section 7 - Systems Description
The Honeywell KGP 560 Terrain Awareness and Warning System
compares GPS information from the Garmin Navigator (GPS 1) to the
integrated Terrain/Obstacle Database to produce a real-time model of
the surrounding terrain. This “virtual” picture is then sent to the MFD to
provide enhanced situational awareness to the pilot.
The system consists of the 560 GA-EGPWS Processor mounted on
the underside of the pilot-side kickplate, a Terrain/Obstacle Database
　
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