Honeywell KGP 560 Betriebsanleitung

P/N 13772-121 1 of 12

Cirrus Design Section 9

SR22 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 SR22, this Supplement is

applicable and must be inserted in the Supplements Section (Section

9) of the Cirrus Design SR22 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 SR22 Pilot’s Operating Handbook.

• Note •

This POH Supplement Revision dated Revision 1: 12-15-07

supersedes and replaces the original release of this supplement dated

Original: 07-03-04.

Revision 1: 12-15-07

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Section 9 Cirrus Design

Supplements SR22

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 4 or later.

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Cirrus Design Section 9

SR22 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

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.

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Section 9 Cirrus Design

Supplements SR22

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.

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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

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 1: 12-15-07

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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.

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Cirrus Design Section 9

SR22 Supplements

GNS-430

GPS

Avidyne PFD

Transponder

TAWS

AVIONICS

NON-ESSENTIAL

BUS

Configuration

Module

GMA 340

Audio Panel

SR20_FM09_2031

Avidyne MFD

KGP 560

Processor

TAWS

Annunciator Panel

Figure - 1

Honeywell KGP 560 TAWS Simplified Schematic

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Section 9 Cirrus Design

Supplements SR22

TAWS Annunciator Panel

TAWS terrain annunciations and control functions are incorporated

into the Annunciator Panel. The panel consists of a momentary

pushbutton switch (SELF TEST), an illuminated pushbutton switch

(TERR INHIBIT), and three LEDS for Terrain Warning (TERR WARN),

Terrain Caution (TERR CAUT), Terrain Inoperative (TERR INOP).

• SELF TEST - Provides test function for the TAWS.

• TERR INHIBIT - To inhibit nuisance or unwanted warnings at

airports that are not in the system database, the pilot may

select the TERR INHIBIT switch. Although selection will inhibit

all TAWS visual and aural alerts, the Terrain Awareness Display

will remain functional with the message “Warnings Inhibited”

displayed on the MFD. When activated the switch will illuminate

amber.

• TERR INOP - Indicates the TAWS inoperative. When activated

the LED will illuminate amber.

• TERR CAUT - Indicates a possible terrain or obstacle conflict

within 40-60 seconds. When activated the LED will illuminate

amber.

• TERR WARN - Indicates a possible terrain or obstacle conflict

within 30 seconds. When activated the LED will illuminate red.

The annunciators are dimmed via the instrument panel lighting

dimmer switch. The TAWS annunciator panel is powered by 28 VDC

through the 2-amp ANNUN circuit breaker on the Essential Bus

Alert Priority

When any of the TAWS aural alerts are in progress, all aural TRAFFIC

alerts are inhibited.

Advisory Callout

The advisory callout “FIVE HUNDRED”, occurs at approximately 500

feet AGL.

Revision 1: 12-15-07

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Cirrus Design Section 9

SR22 Supplements

Annunciator Color Function

SELF TEST N/A Provides test function for TAWS

TERR INHIBIT AMBER All TAWS alerting functions inhibited

TERR INOP AMBER Indicates TAWS inoperative

TERR CAUT AMBER Possible terrain or obstacle conflict within 40-60 seconds

TERR WARN RED Possible terrain or obstacle conflict within 30 seconds

TAWS

SELF

TEST

TERR

INHIBIT

TERR

INOP

TERR

CAUT

TERR

WARN

SR22_FM09_2032

Figure - 2

TAWS Annunciator Panel

Revision 1: 12-15-07

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Section 9 Cirrus Design

Supplements SR22

MFD Terrain Awareness Display

• WARNING •

Do not use the Terrain Awareness Display for navigation of the

aircraft. The TAWS 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.

To select the Terrain Awareness Display Page on the MFD, rotate the

page knob to TAWS.

Terrain and obstacle alerts are the most critical situations displayed by

TAWS. There are two levels of alerts:

•Caution Alert - Possible terrain or obstacle conflict within 40-

60 seconds. When triggered, the terrain or obstacle that

caused the alert is displayed in bright yellow. In addition, a

message describing the nature of the alert is presented in the

MFD message bar.

•Warning Alert - Possible terrain or obstacle conflict within 30

seconds. When triggered, the terrain or obstacle that caused

the alert is displayed in bright red. In addition, a message

describing the nature of the alert is presented in the message

bar

When a caution or warning alert is active, the display image

surrounding the target is enlarged somewhat to allow the terrain or

obstacle to be better seen on the display.

If a terrain or obstacle alert occurs while a page other than Terrain

Awareness Display Page is being displayed, a terrain or obstacle alert

message is displayed in the Message Bar. When the pilot

acknowledges this message, the MFD will automatically switch to the

Terrain Awareness Display Page.

The message bar will be removed from the display when the TAWS is

no longer in alert status, or if the pilot acknowledges the message from

the Terrain Awareness Display Page.

Revision 1: 12-15-07

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