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Garmin TERRAIN is a terrain awareness system incorporated into
GNC 420 units to increase situational awareness and aid in reducing
controlled flight into terrain. The TERRAIN function displays altitudes
of terrain and obstructions relative to the aircraft’s altitude and are
advisory in nature only. Individual obstructions may be shown if
available in the database, however, not all obstructions may be
available in the database and data may be inaccurate. TERRAIN
information should be used as an aid to visual acquisition and not use
to navigate or maneuver to avoid terrain.
For for a more detailed description of the TERRAIN function, refer to
the Garmin GNC 420 Pilot's Guide and Reference, P/N 190-00140-20,
Revision H dated May 2006 or later revision.
Revision 02: 08-15-07
8 of 8 P/N 11934-S23
Section 9 Cirrus Design
Supplements SR20
Revision 02: 08-15-07
Intentionally Left Blank
P/N 11934-S30 1 of 12
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Honeywell KGP 560 Terrain/
Awareness Warning System
When the Honeywell KGP 560 Terrain Awareness and Warning
System is installed in the Cirrus Design SR20, this Supplement is
applicable and must be inserted in the Supplements Section (Section
9) of the Cirrus Design SR20 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 SR20 Pilot’s Operating Handbook.
• Note •
This POH Supplement Revision dated Revision 01: 12-15-07
supersedes and replaces the original release of this supplement dated
Original: 07-03-04.
Revision 01: 12-15-07
2 of 12 P/N 11934-S30
Section 9 Cirrus Design
Supplements SR20
Section 1 - General
The airplane is equipped with an Honeywell KGP 560 Terrain
Awareness and Warning System that performs the functions of a
Class C Terrain Awareness and Warning System (TAWS) in
accordance with TSO C151b.
Incorporating much of the technology found in TAWS for air transport
aircraft, the KPG 560 supports:
• Alerting for premature descent.
• Alerting for excessive rate of climb/descent.
• Altitude callout (500 ft) and alerting within 5 nm of 2000 ft public
runways.
• Look-ahead algorithms and integrated terrain/obstacle
database.
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 KGP 560 receives data from the GPS sensor, Transponder,
Primary Flight Display, and the Multifunction Display (MFD). Aural
alerts are communicated to the pilot via the GMA 340 Audio Panel. To
enhance the situational awareness to the pilot, color-coded terrain
display is interfaced on the MFD.
For specific MFD operational details refer to the Avidyne FlightMax
EX5000C Pilot’s Guide.
For specific KGP 560 operational details, refer to the KGP 560 & 860
EGPWS Pilot’s Guide, P/N 006-18254-001, Revision 04 or later.
Revision 01: 12-15-07
P/N 11934-S30 3 of 12
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
1. Do not use the Terrain Awareness Display for navigation of the
aircraft. The KGP 560 Terrain Awareness and Warning System is
intended to serve as a situational awareness tool only and may not
provide the accuracy fidelity on which to solely base terrain or
obstacle avoidance maneuvering decisions.
Section 3 - Emergency Procedures
Off-Airport Landings
1. For ditching or other off-airport landings, inhibit the Terrain
Awareness System functions by selecting the TERR INHIBIT
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
　
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本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 1148-126(115)