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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.
Original: 07-03-04
P/N 13772-121 5 of 12
Cirrus Design Section 9
SR22 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
Original: 07-03-04
6 of 12 P/N 13772-121
Section 9 Cirrus Design
Supplements SR22
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
integral to the processor, the Configuration Module integral to the
system’s wire harness, and the TAWS annunciator panel mounted on
the lower LH portion of the instrument panel.
The 560 GA-EGPWS Processor is powered by 28 VDC through the 5-
amp SKYWATCH/TAWS circuit breaker on the Avionics Nonessential
Bus.
For a additional system information, refer to the KGP 560 & 860
EGPWS Pilot’s Guide, P/N 006-18254-001, Revision 4 or later.
System Constraints
• If there is no terrain data in the database for a particular area,
then TAWS alerting is not available for that area. The affected
area on the Terrain Awareness Display Page will be colored a
MAGENTA dot pattern.
• If the TAWS has been inhibited (e.g. the pilot selected TERR
INHIBIT) the system will not give aural alerts. The MFD will
display a purple message block with cyan text reading, “TAWS
Inhibited”.
• The TAWS will not be available and the TERR INOP
annunciator will illuminate if any of the following components
are inoperative: MFD, PFD, GPS 1, Transponder, or Attitude
Encoder.
Original: 07-03-04
P/N 13772-121 7 of 12
Cirrus Design Section 9
SR22 Supplements
GNS-430
GPS
Avidyne PFD
Transponder
TAWS
5
AVIONICS
NON-ESSENTIAL
BUS
Configuration
Module
GMA 340
Audio Panel
SR20_FM09_2031
Avidyne MFD
KGP 560
Processor
　
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本文鏈接地址：AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(129)