INSTRUCTION SHEET

FAA Approved Airplane Flight Manual Supplement

P/N 140-590039-0113
for
TERRAIN AWARENESS and WARNING SYSTEM (TAWS+)

Revision 1: November 19, 2009

This Supplement is Applicable to the Following Airplane Flight Manual:

P/N 140-590039-0005

INSTRUCTIONS

1. Turn to SECTION - 7 SUPPLEMENTS and compare the date of the existing LOG OF
SUPPLEMENTS page with the date of the enclosed LOG OF SUPPLEMENTS page.

Retain the LOG OF SUPPLEMENTS page that has the later date and discard the older LOG
OF SUPPLEMENTS page.

The latest LOG OF SUPPLEMENTS can be printed by using the HBC website at:
http://www.hawkerbeechcraft.com/service_support/pubs/docs/nontechnical/140-590039-
0005-los.pdf

2. Remove and discard Supplement 140-590039-0113 Original Issue, dated September 22,
2009.

3. Arrange the Supplements in SECTION - 7 SUPPLEMENTS in the order shown on the

LOG OF SUPPLEMENTS page and place this Supplement, P/N 140-590039-0113
Revision 1, Pages 1 of 20 thru 20 of 20 in the position indicated on the LOG OF
SUPPLEMENTS page.

4. After compliance with these instructions, this Instruction Sheet may be discarded.

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 Instruction Sheet

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Page 2 of 2
 FAA APPROVED
AIRPLANE FLIGHT MANUAL SUPPLEMENT
P/N 140-590039-0113
Revision 1
for
TERRAIN AWARENESS and WARNING SYSTEM
(TAWS+)

THIS SUPPLEMENT IS APPLICABLE TO

FAA APPROVED AIRPLANE FLIGHT MANUAL
P/N 140-590039-0005
for
Airplane Serials HB-67 and After

Airplane Serial Number: .....................................................................................................

Airplane Registration Number: ...........................................................................................

Copyright © 2009 Hawker Beechcraft Corporation. All rights reserved.

Hawker and Beechcraft are trademarks of Hawker Beechcraft Corporation.

Revision 1: Nov 19, 2009 Section - 7 Page 1 of 20

 FAA Approved Airplane Flight Manual Supplement

LIST OF EFFECTIVE PAGES

Supplement Status Date

Original Issue Sep 22, 2009

Revision 1 Nov 19, 2009

Use the List Of Effective Pages to determine the current status of this supplement.
Pages affected by the current revision are indicated by an asterisk (*).

Page Page Revision

Number (s) Status Number
* 1 of 20 Revised 1

* 2 of 20 Revised 1

* 3 of 20 Revised 1

* 4 of 20 Revised 1

* 5 of 20 Revised 1

* 6 of 20 Revised 1

* 7 of 20 Revised 1

* 8 of 20 Revised 1

* 9 of 20 Revised 1

* 10 of 20 Revised 1

* 11 of 20 Revised 1

* 12 of 20 Revised 1

* 13 of 20 Revised 1

* 14 of 20 Revised 1

* 15 of 20 Revised 1

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* 18 of 20 Revised 1

* 19 of 20 Revised 1

* 20 of 20 Revised 1

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FAA Approved Airplane Flight Manual Supplement

LOG OF REVISIONS

Rev Page Date

Description FAA Approved
No. No(s) of Revision

1 of 20
0 thru Original Issue
20 of 20

1 of 20
Revised all page
thru
footers for Revision 1.
20 of 20
Revised title and
1 of 20 signature block for
Revision 1.
1
Updated List of
2 of 20 Effective Pages for
Revision 1.
Recorded all
3 of 20 Revision 1 changes in
Log of Revisions.

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FAA Approved Airplane Flight Manual Supplement

CONTENTS
Page

TITLE PAGE ........................................................................................................... 1 of 20

LIST OF EFFECTIVE PAGES ................................................................................ 2 of 20

LOG OF REVISIONS .............................................................................................. 3 of 20

INTRODUCTION ..................................................................................................... 6 of 20

SECTION 1 - GENERAL......................................................................................... 7 of 20

ABBREVIATIONS and ACRONYMS.................................................................7 of 20

TAWS+ SYSTEM INFORMATION ....................................................................8 of 20

SWITCH ANNUNCIATORS...............................................................................9 of 20

MESSAGES and AURALS .............................................................................. 10 of 20

ANNUNCIATORS, VOICE ALERTS and VOICE WARNINGS........................ 11 of 20

SECTION 2 - LIMITATIONS ................................................................................. 12 of 20

AVIONICS LIMITATIONS................................................................................ 12 of 20

TAWS+ SYSTEM LIMITATIONS ................................................................. 12 of 20

SECTION 3 - EMERGENCY PROCEDURES....................................................... 13 of 20

AVIONICS ....................................................................................................... 13 of 20

TAWS+ TERRAIN WARNING ..................................................................... 13 of 20

TAWS+ TERRAIN AVOID ........................................................................... 14 of 20

TAWS+ WINDSHEAR WARNING ............................................................... 15 of 20

TAWS+ SYSTEM DEACTIVATION ............................................................. 15 of 20

FLIGHT DISPLAY FAILURE FLAGS........................................................... 15 of 20

DITCHING ....................................................................................................... 15 of 20

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 FAA Approved Airplane Flight Manual Supplement

CONTENTS
continued

Page

SECTION 4 - ABNORMAL/NORMAL PROCEDURES........................................ 16 of 20

Sub-section 4.05 - ABNORMAL PROCEDURES ............................................. 16 of 20

AVIONICS ........................................................................................................16 of 20

TAWS+ CAUTION ALERT ...........................................................................16 of 20

TAWS+ WINDSHEAR CAUTION ALERT ....................................................17 of 20

TAWS+ MODE FAILURE .............................................................................17 of 20

UNRELIABLE GPS POSITION ....................................................................17 of 20

Sub-section 4.10 - NORMAL PROCEDURES .................................................. 18 of 20

EXPANDED NORMAL PROCEDURES...........................................................18 of 20

TAWS+ SYSTEM INFORMATION ...............................................................18 of 20

SECTION 5 - PERFORMANCE............................................................................ 19 of 20

SECTION 6 - WEIGHT & BALANCE ................................................................... 19 of 20

EQUIPMENT LIST ...........................................................................................19 of 20

INTRODUCTION
NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

The information provided in this supplement is applicable to Hawker 750 airplanes with Terrain
Awareness and Warning System (TAWS+) installed.

For limitations, procedures and performance information not listed within this supplement,
consult the basic Airplane Flight Manual.

Refer to Rockwell Collins Pro Line 21 Avionics System Operator’s Guide for the Hawker 750,
P/N 523-0808876 at the latest revision.

Refer to TAWS+ Pilot’s Guide, ACSS Document No. 8006772-001, dated July 2007 or later
revision.

The following information supplements the two documents listed above.

Page 6 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

SECTION 1 - GENERAL
NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

ABBREVIATIONS and ACRONYMS

ACSS..........................................Aviation Communication and Surveillance Systems
AGL ............................................Above Ground Level
APM............................................Aircraft Personality Module
ATC ............................................Air Traffic Control
CPA ............................................Collision Prediction and Alerting
DH ..............................................Decision Height
GND PROX ................................Ground Proximity
GPS ............................................Global Positioning System
GPWS.........................................Ground Proximity Warning System
ILS ..............................................Instrument Landing System
IMC .............................................Instrument Meteorology Conditions
INHIB ..........................................Inhibit
KIAS ...........................................Knots Indicated Airspeed
MDA............................................Minimum Descent Altitude
MFD............................................Multi-Function Display
MTCD .........................................Minimum Terrain Clearance Distance
N/A..............................................Not Applicable
nm...............................................Nautical Mile
OCPA .........................................Obstacle Collision Prediction and Alerting
OVRD .........................................Override
PFD ............................................Primary Flight Display
RDR............................................Radar
STC ............................................Supplemental Type Certificate
TAD ............................................Terrain Advisory Display
TAWS .........................................Terrain Awareness and Warning System
TAWS+ .......................................Terrain Awareness and Warning System plus
TERR..........................................Terrain
VMC............................................Visual Meteorology Condition

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TAWS+ SYSTEM INFORMATION

The following must be operational for the proper functioning of Modes 1 through 7
of the TAWS+:

1. Terrain Awareness and Warning (TAWS+) Computer

2. Radio Altimeter
3. Vertical Speed from the Air Data Computer
4. Airspeed from the Air Data Computer
5. Glideslope and Localizer Deviation
6. Landing Gear position
7. Flap position
8. Roll attitude from Pilot’s Attitude System
9. Decision Height System
10. AOA vane and AOA computer

The following must be operational for the proper functioning of the predictive features
of the TAWS+:

1. Terrain Awareness and Warning System (TAWS+) Computer

2. Heading/Flight Path Angle/Attitude from the No. 1 Compass System
3. GPS position
4. Terrain and Airport Database
5. Obstacle Database
6. Landing Gear
7. Flap Position

The following predictive features are available:

1. Terrain Display
2. Collision Prediction and Alerting (CPA)
3. Obstacle Collision Prediction and Alerting (OCPA)

TAWS+ Power Supply

The TAWS+ system is powered from the PS1 bus bar through a 5 AMP circuit breaker labelled
TAWS, located behind the copilot on the DA-A circuit breaker panel, location F8.

Page 8 of 20 Section - 7 P/N 140-590039-0113

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SWITCH ANNUNCIATORS
The following switch annunciators are located in front of the pilot between the pilot Multi-Function
Display (MFD) and the copilot MFD on the center instrument panel.

FLAP TERR

OVRD INHIB

ALT
GS
CALLS
INHIB OVRD

Use of this switch is for operations when the normal landing flap position is not
FLAP used. Pushing the switch disables the TOO LOW FLAPS portion of the
OVRD Ground Proximity Warning System (GPWS) Mode 4b alert boundaries and
also selects the Mode 2b envelope. The OVRD annunciator illuminates amber
when the switch is pushed.

Use of this switch is to prevent nuisance alerts due to terrain or airport data-
TERR base errors, omissions, or low resolution. Pushing the switch deselects all
INHIB CPA and OCPA functions of the TAWS+ system. The INHIB annunciator
illuminates amber when the switch is pushed.

Use of this switch is for Instrument Landing System (ILS) operations without
GS a glideslope. Pushing the switch inhibits the GPWS Mode 5 GLIDESLOPE
alerting below 2000 feet AGL. The INHIB annunciator illuminates amber when
INHIB GPWS Mode 5 GLIDESLOPE alerting is inhibited.

Use of this switch is to inhibit disruptive aural alerts due to system failures.
ALT
Pushing the switch inhibits all altitude callouts. The OVRD annunciator
CALLS
illuminates amber when the switch is pushed.
OVRD
NOTE: At the pilot’s discretion, this switch may be used when below
500 feet AGL.

P/N 140-590039-0113 Section - 7 Page 9 of 20

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MESSAGES and AURALS

The following messages and aurals are provided for GPWS Modes 1 through 7.
See this supplement Section 3 - EMERGENCY PROCEDURES and Section 4 - ABNORMAL/
NORMAL PROCEDURES, Sub-section 4.05 - ABNORMAL PROCEDURES for the appropriate
procedure associated with each caution and warning alert.

PFD Caution PFD Warning Warning

Mode Function Caution Aural
Message Message Aural
Excessive
1 GND PROX "Sink Rate" PULL UP "Pull Up"
Descent Rate
Excessive
2 Closure on GND PROX "Terrain, Terrain" PULL UP "Pull Up"
Terrain
Altitude Loss "Don’t Sink,
3 GND PROX N/A N/A
After Takeoff Don’t Sink"
Unsafe Terrain "Too Low
4a GND PROX N/A N/A
Clearance Gear"
Unsafe Terrain
4b GND PROX "Too Low Flaps" N/A N/A
Clearance
Excessive
5 Glideslope GND PROX "Glideslope" N/A N/A
Deviation
Excessive Bank "Bank Angle,
6 N/A N/A N/A
Angle Bank Angle"
"Two Thousand
Five Hundred",
"One Thousand",
"Five Hundred",
"Four Hundred",
6 Altitude Callouts N/A "Three Hundred", N/A N/A
"Two Hundred",
"One Hundred",
"Fifty", "Forty",
"Thirty",
"Twenty", "Ten"
Selected DH "Minimums,
6 N/A N/A N/A
Selected MDA Minimums"
"Windshear,
"Caution
7 Windshear WINDSHEAR WINDSHEAR Windshear,
Windshear"
Windshear"

Page 10 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

ANNUNCIATORS, VOICE ALERTS and VOICE WARNINGS

The following annunciators, voice alerts and voice warnings are provided for the Collision
Prediction and Alerting (CPA) function of the TAWS+.

See this supplement Section 3 - EMERGENCY PROCEDURES and Section - 4 ABNORMAL/

NORMAL PROCEDURES, Sub-section 4.05 - ABNORMAL PROCEDURES for the appropriate
procedure associated with each alert and warning.

PFD Caution PFD Warning Warning

Function Caution Aural
Message Message Aural
Terrain Alerting "Terrain, Terrain,
and Display "Caution Pull Up, Pull Up"
GND PROX PULL UP
Terrain" or
"Avoid Terrain"
Premature "Too Low,
GND PROX N/A N/A
Descent Alerting Terrain"
Obstacle "Obstacle, Obstacle,
Alerting and "Caution Pull Up, Pull Up"
GND PROX PULL UP
Display Obstacle" or
"Avoid Obstacle"

P/N 140-590039-0113 Section - 7 Page 11 of 20

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 FAA Approved Airplane Flight Manual Supplement

SECTION 2 - LIMITATIONS
AVIONICS LIMITATIONS
NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

TAWS+ SYSTEM LIMITATIONS

1. TAWS+ Pilot’s Guide, Aviation Communications and Surveillance Systems (ACSS)

Document Number 8006772-001, dated July 2007 or later revision, must be available to the
flight crew when operating the TAWS+.

2. Navigation must not be predicated upon use of TAWS. The terrain display is intended
to serve as a situational awareness tool only. It may not provide the accuracy and/or fidelity
on which to solely base decisions and plan maneuvers to avoid terrain and obstacles.

3. To avoid giving unwanted alerts, the TAWS must be inhibited when landing at an airport that
is not included in the airport database. Refer to ACSS Document 8006417 for airports
contained in the database (see "TAWS Airports" at www.acsscustomerservices.com).

4. The current local QNH altimeter setting must be entered in the pilot’s altimeter for proper
terrain alerting. In particular, the TERR INHIB annunciator switch must be selected when
operating in QFE mode.

Page 12 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

SECTION 3 - EMERGENCY PROCEDURES

AVIONICS
NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

TAWS+ TERRAIN WARNING

(PULL UP MESSAGE ON PFD and/or "PULL UP", or "TERRAIN, TERRAIN, PULL UP,
PULL UP" or "OBSTACLE, OBSTACLE, PULL UP, PULL UP" AURAL ALERT)

NOTES:

1. Pilots are authorized to deviate from the current ATC clearance to the extent
necessary to comply with a TAWS+ warning.

2. In the event of a predictive terrain alert, the two MFDs will automatically switch
to display terrain. The pilot and copilot’s Primary Flight Displays (PFDs) and the
MFDs will auto range to 10 miles following the generation of the terrain alert.

Go - Around button ................................Push

Thrust ......................................................Take-off N1
Pitch attitude ..........................................Increase and climb as required
to avoid terrain/obstacle.
APR..........................................................OVRD

FLAPS ............................................................Retract to 15°

LANDING GEAR ............................................Up
FLAPS ............................................................Up
AIR BRAKEs ..................................................SHUT
Terrain display................................................Monitor
Pitch attitude...................................................Maintain until safe terrain clearance is
assured.
ATC ................................................................Notify (if required)

P/N 140-590039-0113 Section - 7 Page 13 of 20

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 FAA Approved Airplane Flight Manual Supplement

TAWS+ TERRAIN AVOID

(PULL UP MESSAGE ON PFD and/or "AVOID TERRAIN", or "AVOID OBSTACLE"

AURAL ALERT)

NOTES:

1. Pilots are authorized to deviate from the current ATC clearance to the extent
necessary to comply with a TAWS+ warning.

2. In the event of a predictive terrain alert, the two MFDs will automatically switch
to display terrain. The pilot and copilot’s PFDs and the MFDs will auto range
to 10 miles following the generation of the terrain alert.

Go - Around button ................................Push

Thrust ......................................................Take-off N1
Pitch attitude ..........................................Increase and climb as required
to avoid terrain/obstacle.
Turn .........................................................Using all available information,
immediately initiate a turn in
the safest direction.
APR..........................................................OVRD

FLAPS ........................................................... Retract to 15°

LANDING GEAR............................................ Up
FLAPS ........................................................... Up
AIR BRAKEs.................................................. SHUT
Terrain display ............................................... Monitor
Pitch attitude .................................................. Maintain until safe terrain clearance is
assured.
ATC................................................................ Notify (if required)

NOTE: If the "Avoid Terrain" warning occurs when or just after a turn is initiated, reverse the
turn direction while executing the positive pull up.

Page 14 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

TAWS+ WINDSHEAR WARNING

(RED WINDSHEAR MESSAGE ON PFD and/or "WINDSHEAR, WINDSHEAR, WINDSHEAR"

AURAL ALERT)

Go - Around button ................................Push

Thrust ......................................................Take-off N1
Pitch attitude ..........................................Increase as required to arrest
descent, allowing airspeed to
decrease to intermittent stick
shaker activation.
APR..........................................................OVRD

AIR BRAKEs................................................... SHUT

ATC................................................................. Notify (if required)

TAWS+ SYSTEM DEACTIVATION

If the pilot in command determines that activation of the TAWS+ will interfere in dealing with
emergency conditions, the system may be deactivated by pulling the TAWS circuit breaker.

FLIGHT DISPLAY FAILURE FLAGS

RA

Radio altitude failure is annunciated by a red RA on the PFD. Radio altitude data is invalid.
The radio altitude digital display, radio minimums and the analog radio altitude display on the PFD
will be inoperative.

NOTE: TAWS and TCAS functions will continue to operate but GPWS modes will not be
available.

DITCHING
In the event that ditching or an off-airport landing is necessary, inhibit the visual and voice alerts
by pulling the TAWS circuit breaker.

P/N 140-590039-0113 Section - 7 Page 15 of 20

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 FAA Approved Airplane Flight Manual Supplement

SECTION 4 - ABNORMAL/NORMAL PROCEDURES

Sub-section 4.05 - ABNORMAL PROCEDURES
NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

AVIONICS

TAWS+ CAUTION ALERT GPWS and Voice Alert

The following standard procedures have been formulated to handle the majority of cases;
however it is the crew’s responsibility to analyze all available instruments and information to
determine the best course of action. ATC should be notified as necessary.

Mode Voice Alert Action

Level wings and reduce rate-of-descent until
1 "SINK RATE"
visual and voice alerts cease.
Immediately adjust flight path away from
2 "TERRAIN, TERRAIN"
terrain.
Level wings and immediately establish a
3 "DON’T SINK, DON’T SINK"
positive rate-of-climb.
"TOO LOW GEAR" Execute go-around if proper terrain clearance
4a or or landing gear position cannot be immediately
"TOO LOW TERRAIN" verified.
"TOO LOW FLAPS" Execute go-around if proper terrain clearance
4b or or flap position cannot be immediately verified.
"TOO LOW TERRAIN"
Immediately climb to re-establish proper glide
5 "GLIDESLOPE"
path or execute a go-around.
Reduce bank angle.
"BANK ANGLE,
6 NOTE: There will be no GND PROX message
BANK ANGLE"
with the caution.
Stop descending, or climb, and/or turn as
necessary, based on analysis of all available
CPA "CAUTION TERRAIN"
instruments and visual observation in order to
cancel the alert.
Stop descending, or climb, and/or turn as
necessary, based on analysis of all available
OCPA "CAUTION OBSTACLE"
instruments and visual observation in order to
cancel the alert.

NOTE: In the event of a predictive terrain alert, the MFD will automatically switch to display
terrain, if not displaying terrain. The pilot’s PFD and the MFD will auto range to 10
miles.

Page 16 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

TAWS+ WINDSHEAR CAUTION ALERT WS on PFD and Voice Alert

During Voice Alert Action

Verify take-off thrust is set and maintain
TAKEOFF "CAUTION WINDSHEAR"
take-off pitch attitude.
Consider a go-around. If approach is
continued, closely monitor airspeed and
APPROACH "CAUTION WINDSHEAR"
glide path and avoid prolonged thrust
reduction.

TAWS+ MODE FAILURE Messages on PFD

One or more of the basic GPWS Modes (1-6) are inoperative

GPWS and some or all of the aural alerts and visual warnings and
cautions may not be provided.
Windshear GPWS Mode 7 is inoperative and associated aural
WS
alerts and visual warnings and cautions may not be provided.
CPA mode is inoperative and associated aural alerts and visual
TERR
warnings and cautions may not be provided.
TERRAIN FAIL Terrain and obstacle display is inoperative.

UNRELIABLE GPS POSITION

Operations with the Collision Prediction and Alerting (CPA) function active, and the Global
Position System (GPS) position unreliable, may result in nuisance terrain alerts. Select TERR
annunciator switch to INHIB.

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 FAA Approved Airplane Flight Manual Supplement

SECTION 4 - ABNORMAL/NORMAL PROCEDURES

Sub-section 4.10 - NORMAL PROCEDURES
EXPANDED NORMAL PROCEDURES

NOTE: This supplemental information supersedes all Honeywell Enhanced Ground Proximity
Warning System (EGPWS) information in the Airplane Flight Manual.

TAWS+ SYSTEM INFORMATION

1. The TAWS+ terrain display is available only on the Present Position Map and Arc formats.
Selection of Weather Radar and the Terrain Display are mutually exclusive.

2. In the event of a terrain alert, the MFD will automatically switch to display terrain, if not
currently displaying terrain, and the pilot’s PFD and the MFD will auto range to 10 miles.
After the alert has ceased, the display(s) can be returned to weather radar by pushing the
TERR/RDR line select key on the display(s).

3. Operations within 15 nm of an airport not contained in the TAWS+ database with the CPA
function active may result in nuisance terrain alerts. Select TERR annunciator switch to
INHIB. Refer to ACSS Document 8006417 for airports contained in the database (see
"TAWS Airports" in www.acsscustomerservices.com).

4. If there is no terrain data in the database for a particular area, the affected display area is
colored magenta.

5. The obstacle database accounts for limited cataloged obstructions. If a particular obstacle
is not in the database, the obstacle awareness alerting is not available for that particular
obstacle.

6. The obstacle database contains both "verified" and "unverified" obstacles as provided in the
state data (FAA, etc). A "verified" obstacle has been reviewed by the publishing state and
a reliability assessment has been assigned. "Unverified" obstacles have not been reviewed
by the publishing state and could potentially result in missing or nuisance alerts.

Page 18 of 20 Section - 7 P/N 140-590039-0113

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FAA Approved Airplane Flight Manual Supplement

SECTION 5 - PERFORMANCE
No change.

SECTION 6 - WEIGHT & BALANCE

EQUIPMENT LIST
Remove

Honeywell Mk V EGPWS computer

• weight 7.0 pounds
• fuselage station 159.84

Add

ACSS TAWS+ computer

• part number 9000000-86008
• weight 7.16 pounds
• fuselage station 159.84

ACSS APM
• part number 9000001-10001
• weight 0.11 pounds
• fuselage station 159.84

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