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Honeywell KGP 560 Pilot Operating Handbook page 4

Terrain awareness/warning system
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Section 9
Supplements
Activate TAWS
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 (V
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.
4 of 12
• Note •
Cirrus Design
SR22
) until terrain
x
P/N 13772-121
Revision 1: 12-15-07

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