Garmin BELL 206B 400W Configuration guide

ARMIN Ltd. or its subsidiaries
/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
FAA APPROVED
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI AnON SYSTEM
As Installed In
Bell 206B
Reg. No. IN _
This do ument serves as a Rotor raft Flight Manual Supplement when the rotor raft is
equipped with the Garmin 400W Series unit. This do ument must be arried in the
rotor raft at all times when the Garmin 400W Series unit is installed in a ordan e with
STC SR02080SE.
The information ontained herein supplements or supersedes the information made
available to the operator by the manufa turer in the form of learly stated pla ards,
markings, or manuals or in the form of an FAA approved Rotor raft Flight Manual, only
in those areas listed herein. For limitations, pro edures and performan e information not
ontained in this do ument, onsult the basi pla ards, markings, or manuals or the basi
FAA approved Rotorcraft Flight Manual.
FAA APgOVED
J;<y Manager, Flight Test Branch
Federal Aviation Administration
Seattle Air raft Certifi ation Offi e
DATE:~
190-01226-06 Rev. 1
Page I of 14

ARMIN Ltd. or its subsidiaries
/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS.WAAS NAVI ATION SYSTEM
Bell 206B
LO OF REVISIONS
age
Rev. No. No. Date
Des ription FAA Approved
1 All
Complete
~,,-r~
Supplement
Original
Mgr. Fit.Test Br.
Federal Aviation Administration
Seattle Air raft Certifi ation Offi e
Date
'1/-.:, II")
190-01226-06 Rev. I
Page 2 of 14

ARMIN Ltd. or its subsidiaries
/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI ATION SYSTEM
Bell 206B
Table of Contents
Section I. LIMITATIONS 4
I. I Pilot's uide 4
1.2 System Software: 4
I.3 Navigation Database 5
1.4 Terrain Database 5
1.5 Navigation 5
1.6 Terrain Proximity Display [Units without HTAWS] 6
1.7 HTAWS Function [Units with HTAWS] 6
1.8 HTAWS Annunciations on the PFD [Units with HTAWS] 7
Section 2. EMER ENCY PROCEDURES 8
.1 Emergency Procedures 8
. Abnormal Procedures 8
Section 3. NORMAL PROCEDURES 9
3.1 Approa hes with Verti al Guidan e 9
3.2 WFDE Prediction Program 9
3.3 HTAWS Controls 10
3.4 IITAWSAlerts II
3.5 500H Interface 12
Section 4. PERFORMANCE 12
ENERAL 13
armin 400W Series PSiWAAS Nav Com 13
Operation 14
Class II O eani , Remote, and other Operations 14
FAA APPROVED
190-01226-06 Rev. I
Page 3 of 14 DATE:
SEP 7 010

ARMIN Ltd. or its subsidiaries
c/o armin International
200 E. 5 " Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGATION SYSTEM
Bell 206B
Section I. LIMITATIONS
1.1 Pilot's uide
The ARMIN 400W Series Pilot's uide, part number and revision listed below (or later
revisions), must be immediately available for the flight crew whenever navigation is
predicated on the use of the 400W Series unit.
400W Series Pilot's Guide Ref PIN 90-00356-00 Rev G
400W/500W Series Optional Displays PIN 90-00356-30 Rev H
This model helicopter when equipped with the G400W is limited to VFR ONLY
operations in accordance with 14 Code of Federal Regulations Part 91 and Part 135. The
placard listed below shall be located in close proximity to the 400W Series unit.
"APPROVED FOR DAYINIGIIT VFR".
1.2 System Software:
The system must utilize the Main and PS software versions listed below (or later FAA
approved versions for this STC). The software versions are displayed on the self-test
page immediately after turn.on for approximately 5 seconds or they can be accessed in
the AUX pages.
Subsequent software versions may support different functions. Check the 400W Series
Pilot's uide for further information.
Table 1 - Almroved Software Versions
Approved Software Version
Software Item or lacer FAA annroved versions or chis STCJ
SW version As disnlaved on unit
Main SW Version 4.0 4.0
PS SW Version 3.2 3.2
FAA APPROVED
SEP 27 2010
DATE:
-----
90-0 226-06 Rev. I
Page 4 of 4

ARMIN Ltd. or its subsidiaries
c/o annin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI ATION SYSTEM
Bell 206B
1.3 Navigation Database
The 400W Series unit database cards must he installed and current. The software
automatically precludes invalid databases for use y the 400W. Database cycle
information is displayed at power up on the screen, hut more detailed information is
available on the AUX - UTILITY page.
a) Installations with dua1400W/500W Series units will only crossfill between units
when they contain the same database cycle. Updating of each database must be
accomplished on the ground prior to flight.
1.4 Terrain Database
The 400W Series unit supports Terrain Proximity or HTAWS and requires a Terrain
database card to be installed in order for the feature to operate. Database cycle
information is displayed at power up on the screen, hut more detailed information is
available on the AUX - UTILITY page. Terrain database cards contain the following
data:
a) Due to the terrain resolution used in this system, the terrain database is divided into
six regions [Americas North; Americas South; Atlantic North; Atlantic South;
Pacific North; Pacific South]. Use of the proper database region must be verified.
b) The Obstacle Database has an area of coverage that includes the United States and
Europe, and is updated as frequently as every 56 days.
NOTE:
The area of coverage may be modified as additional terrain data sources become
available.
I.S Navigation
No navigation is authorized north of 89
0
(degrees) north latitude or south of 89
0
(degrees)
south latitude.
190-01226-06 Rev. I
Page 5 of 14
FAA APPROVED
DATE: __ SE_P_2 7 2010

ARMIN Ltd. or its subsidiaries
c/o armin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS.WAAS NA VI ATION SYSTEM
Bell 206B
1.6 Terrain Proximity Display IUnits without IITA \\'51
Terrain Proximity refers to the display of terrain information and comprises of a 2-D
picture of the surrounding terrain and obstacles relative to the position and altitude of the
rotorcraft. however it does not provide any alerts.
Navigation must not be predicated upon the use of the terrain display. The terrain display
is intended to serve as a situational awareness tool only. y itself, it may not provide
either the accuracy or the fidelity on which to base decisions and plan maneuvers to avoid
terrain or obstacles.
Terrain is not depicted on the terrain display within 10m of airports and heliports.
however terrain hazards may exist in these areas.
1,7 IITAWS Function IUnits with IITAWSI
HTA WS is an optional extension of Terrain Proximity. Pilots are authorized to deviate
from their current ATC clearance to the extent necessary to comply with HT AWS
warnings.
HT AWS shall NOT be used for navigation purposes.
HT AWS is an alerting system. The system does NOT guarantee successful recovery
from a conflict due to factors such as pilot response. aircraft performance. and database
limitations. No standardized recovery technique is defined as recovery maneuvers may
vary.
HTA WS functions perfonned by the armin 400W Series navigator are inhibited below
30 knots groundspeed.
Display of the terrain and obstacles is supplemental data only. Maneuvering solely by
reference to the terrain and obstacle display is not authorized.
NOTE:
The Terrain and Obstacle Display is intended to serve as a terrain and obstacle
awareness tool only. The Display and database may not provide the accuracy or
fidelity on which to base routine navigation decisions and plan routes to avoid
terrain or obstacles.
FAA APPROVED
190.0 1226.06 Rev. I
Page 6 of 14 DATE:
SEP 2 7 2010

ARMIN Ltd. or its subsidiaries
/o armin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGATION SYSTEM
Bell 206B
The Obstacle Database does not contain the location of power line poles or wires. Also
the Obstacle Database contains only KNOWN obstacles and docs not contain ALL
existing obstacles.
When alerting is inhibited, all Forward Looking Terrain Alerting aural and visual alerting
is suppressed. HTA WS should be only inhibited when in visual contact with terrain and
when the pilot can be assured of maintaining clearance from terrain and obstacles.
1.8 IITAWS Annun iations on the PFD IUnits with IITAWSj
HTA WS (Terrain Awareness and Warning System) visual annunciations from the NS
400W series unit are displayed on the 500H PFD. The required HTAWS annunciations
appear in the upper right of the PFD. These annun iations in lude TERRAIN (red),
TERRAIN (yellow), OBSTACLE (red), OBSTACLE (yellow), HTAWS /A (yellow),
HTA WS INHB (white). These annunciations are not relative to the terrain elevation
information displayed on the G500H MFD.
FAA APPROVED
190-01226-06 Rev. 1
Page 7 of 14 DATE:
SEP 2 7 2010

ARMIN Ltd. or its subsidiaries
Ia armin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NA VI ATION SYSTEM
Bell 206B
Section 2, EMER ENCY PROCEDURES
2.1 Emergency Procedures
No change.
2.2 Abnormal Procedures
a) If the armin 400W Series unit PS navigation information is not available, or is
invalid, utilize other remaining operational navigation equipment installed in the
aircraft as appropriate. If the 00W Series unit loses PS position and reverts to Dead
Reckoning mode (indicated by the annunciation of"OR
n
in the lower left of the
display), the moving map will continue to be displayed. Rotorcraft position will be
based upon the last valid PS position and estimated by Dead Reckoning methods.
Changes in airspeed or winds aloft can affect the estimated position substantially.
Dead Reckoning is only available in Enroute and Oceanic mode; Terminal and
Approach modes do not support DR.
b) If a "Loss of Integrity" (INTE ) message is displayed during:
Enrouterrerminal: continue to navigate using PS equipment and periodically
cross-check the PS guidance to other approved means of navigation.
c) When a Terrain or Obstacle Awareness CAUTION occurs, verifY the aircraft flight
path and correct it, ifrequired.
d) When a Terrain or Obstacle Awareness WARNIN occurs, immediately initiate a
maneuver that will provide maximum terrain or obstacle clearance, until all alerts
cease.
FAA APPROVED
190-01226-06 Rev. I
Page 8 of 14 DATE: __
~S~EP272010

ARMIN Ltd. or its subsidiaries
c/o armin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI ATION SYSTEM
Bell 206B
Section 3. NORMAL PROCEDURES
Refer to the 400W Series unit Pilot's uide defined in paragraph 1.1 of this document for
nonnal operating procedures. This includes all PS operations, VHF COM and NAY,
and Multi-Function Display information.
Although intuitive and user friendly the 400W Series unit requires a reasonable degree of
familiarity to enable unit operations without becoming too engrossed at the expense of
basic see-and-avoid. Pilot workload will be higher for pilots with limited familiarity in
using the unit. annin provides training tools with the Pilot's uide and PC based
simulator. Pilots should take full advantage of these training tools to enhance system
familiarization.
3.1 Approaches with Vertical uidance
The 400W Series unit supports three types of PS approaches with vertical guidance:
LPV approaches, LNAVNNAV (annunciated as LNNAV) approaches, and LNA V
approaches with advisory vertical guidance (annunciated as LNA V+V). For LNA V
approaches with advisory vertical guidance, the 400W Series will annunciate LNA V+V
indicating vertical guidance is available. LNA V minimums will be controlling in this
case.
3.2 "'FDE Prediction Program
The annin WAAS Fault Detection and Exclusion (WFDE) Prediction Program is
required for Remote/Oceanic operations. The Prediction Program should be used in
conjunction with the annin 400W/500W Simulator. After entering the intended route
of flight in the Simulator flight plan the pilot selects the FDE Prediction Program under
the Options menu of the Simulator program.
For detailed infonnation refer to the WFDE prediction program instructions
(190-00643-01). The availability of FOE is only required for Oceanic or Remote
operations.
FAA APPROVED
190-01226-06 Rev. I
Page 9 of 14 DATE:
SEP 27 2010
------

ARMIN Ltd. or its subsidiaries
/o Gannin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI AnON SYSTEM
Bell 206B
3,3 T AWS Controls
The HTAWS function has control options on the HTAWS Page using the MENU key.
The options are activated by highlighting the desired option and pressing ENTER.
The "Inhibit HTAWS?" menu selection is used to inhibit HTAWS alerts. When alerting
is inhibited, all HTAWS aural and visual alerting is suppressed. HTAWS should be only
inhibited when in visual onta t with terrain and when the pilot an be assured of
maintaining learan e from terrain and obsta les. Use the "Enable HTA WS?" to un-
inhibit the unit.
The "Mute A tive Caution?" menu sele tion is used to mute an HTA WS aution that is
presently active. When the aution is resolved, the next aution will be heard. It does not
mute warnings, only autions. The "Unrnute A tive Caution?" is used to an el the
mute. An optional "MUTE" external swit h installation on the y li sti k is allowed to
mute the aution that is presently a tive in the same manner as using the Page Menu
sele tion.
The "Redu e Prote tion?" menu sele tion is used to a tivate the Redu e Prote tion (RP)
fun tionality. RP Mode redu es alerting thresholds and suppresses aural and visual
autions to allow operation in loser proximity to terrain and obsta les while ontinuing
to provide prote tion from terrain and obsta les. The "Enable Full Prote tion?" menu
sele tion is used to sele t full prote tion fun tionality again. An optional "RP MODE"
external swit h installation on the y li sti k is allowed to toggle Redu e Prote tion and
Enable Full Prote tion in the same manner as using the Page Menu sele tion.
The "Test HTA WS?" menu sele tion is used to a tivate a manual test whi h verifies
proper operation of the aural and visual annun iations of the system. The aural message
"HTAWS System Test, OK" is played if the system passes the test, if the system fails the
test "HTA WS System Failure" is played. HTAWS test is only available while on the
ground.
Yoi e allouts (yeas) provide voi e annun iation of the air raft height above terrain
when that threshold is crossed. VCOs may be enabled by the pilot in 100ft increments
from 500 feet above ground level to the surfa e. Enabling yeas is a omplished using
Voi e Callout sele tion in the AUX pages.
FAA APPROVED
190-01226-06 Rev. I
Page 10 of 14 DATE:
£,...EP272010

ARMIN Ltd. or its subsidiaries
c/o armin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NA VI ATION SYSTEM
Bell 206B
3.4 liTAWS Alerts
HTA WS visual and aural alerts provided by the armin 400W Series Psrw AAS
Navigator are shown in the table
below.
HTAWS Pop-Up Alert ural Message
Description
nnunciation
It Rs FAIL I
None "HT WS System Failure' HT WS has failed
ttliJA tSfII!
None
None HT WS has been inhibited by the
crew, or the aircraft groundspeed has
fallen below 30 knots (automatic inhi-
bitlng).
I T HS NIA! Non'
"HT WS Not vailable"
HT WS not available.
!tmINI
CAlIIICll - TBIlAIN
'Caution- T,maln, Terrain" Forward Looking Terrain voidance
Caution for Terrain
":I,.• p,l:.
"Warning. Terrain. Terrain" Forward Looking Terrain voidance
Warning 101'Terrain
IIINeU!
CJiJlI(JI.1llST1IC1I
.Caution. Obstacle, Obstade. Forward Looking Terrain voidance
Caution or Obstacle
'I
:fi'!3
il
"WamlOg' Obstacle, Obstacle" Forward Looking Terrain voidance
Warning for Obstacle
l p HOtEl
None
Non.
lerting thresholds are reduced. Visual
and aural annunciation of caution
alerts are suppressed.
",,,
No~e
"Five Hundred" HT WS provides optionalSOO ft
"Four Hundred' through 100 ft (in 100 ft increments)
"Three Hundred' altitude can out alerts.
"Two Hundred"
"One Hundred"
FAA APPROVED
190-01226-06 Rev. I
Page II of14 DATE:
SEP 2 7 2010

ARMIN Ltd. or its subsidiaries
/o Garmin International
1200 E. lSI" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NAVI ATION SYSTEM
Bell 206B
3.5 G500H Interface
The NS 400W series unit is interfaced to the SOOH display system for the purpose of
displaying HTA WS annun iations in the pilot's primary field of view. Terrain and
obstacle alerts are provided by the NS 400W series unit. The alerting mode for SOOH
Terrain Helicopter Synthetic Vision Technology (HSVT) will be driven by the HTA WS
mode sele ted on the GNS 400W series unit. In the event of a failure of the GNS unit
providing HTA WS functionality. the HSVT Terrain alerting may be available and the
alerting mode can be selected by the pilot on the SOOH terrain page.
Section 4. PERFORMANCE
No hange.
FAA APPROVED
190-01226-06 Rev. I
Page 120fl4 DATE: __ ~S~F~P272010

ARMIN Ltd. or its subsidiaries
c/o annin International
1200 E. \5\" Street, Olathe, KS 66062 USA
ROTORCRAFT FLI HT MANUAL SUPPLEMENT
ARMIN 400W SERIES PS-WAAS NA VI ATION SYSTEM
Bell 206B
ENERAL
ormin 400W Series PS/WAAS Nov Com
The armin 400W Series PSIW AAS Navigator is a panel-mounted product that
contains a PS/W AAS receiver for PS approved primary navigation under TSO C 146a,
(plus optional VHF Com, VHF Nav radios and HTAWS) in an integrated unit with a
moving map and color display. The 400W Series unit features a graphical display.
The navigation functions arc operated by dedicated keys and graphical menus which are
controlled by the buttons and the dual concentric rotary knob along the bottom and right
side of the display.
Optional VHF Com and VHF Nav radio functions arc controlled via dedicated buttons
and knobs on the left side of the display and adjacent to frequencies they are controlling.
r'pllle Mo••.•.•g
Map Oospilly and
Na""llllloQl'llofO
NIV RadIO __ ---
"".~
t>llv RadIO ._--.- - -
F1~p
l...-ge KnOb _
Com'VLOC ~
Freq (1,11-11) ........--Terr.in FIiQIl1 I \
Sma. Knob Ph'5e .fl<l
Col'ni"'AOC ~~o~~~~::? MOUo"OlQ I COl 06S
Freq (~Hl) Sere.... I Key Key
NaVlllDhOO
Source PS,
\/LOC, Or
PS-F'T)(
DMeel.To Key
RaOlQeKeys / Meou Key
/ . ~c.,,'"
, "'.---- EOTer Key
FuncloQl'l and
Pa.ge Nurnl>oe<
__ laf1;leKilob
Figure I - 400\V Series Control and Display Layout
Optional HTA WS functions are controlled by soft keys located on the dedicated TA WS
page. An installation option allows some of the controls to be installed on the cyclic grip.
FAA APPROVED
\90-0\226-06 Rev. I
Page \3 of 14 DATE: __
~S£~P272010

ARMIN Ltd. or its subsidiaries
/o armin International
200 E. 5 " Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NA VIGATION SYSTEM
Bell 206B
Operation
GPS/WAAS TSO-CI46a Class 3 Operation: The Garmin 400W Series unit uses GPS
and WAAS (within the coverage of a Space-Based Augmentation System complying
with ICAO Annex 10) for emoute, terminal area, non-precision approach operations
(including "GPS", "or GPS", and "RNA V" approaches), and approach procedures
with vertical guidance (including "LNAVIVNA V" and "LPV").
Navigation is accomplished using the W S-84 (NAD-83) coordinate reference datum.
GPS navigation data is based upon use of only the Global Positioning System (GPS)
operated by the United States of America.
Class II Oceanic, Remote, and other Operations
The armin 400W Series, as installed, has been found to comply with the requirements
for PS primary means of Class II navigation in oceanic and remote airspace, when used
in conjunction with WAAS Garmin Prediction Program part number 006-AO 54-03.
Oceanic operations are supported when the 400W Series unit annunciates OCN. This
provides an alarm limit of four NMI and a mask angle oftive degrees. The 400W series
unit also has the ability to predict RAIM availability at any waypoint in the database or if
WAAS corrections are expected to be absent or disabled. This RFMS does not constitute
an operational approval for Oceanic or Remote area operations. Additional equipment
installations or operational approvals may be required.
a) Oceanic navigation requires an additional approved long range oceanic and/or
remote area navigation system with independent display, sensors, antenna, and
power source. (It may be a second 400W/500W Series unit.)
b) Redundant VHF Com and VHF Nav systems may be required for other than
U.S. 14 CFR Part 91 operations. Check foreign regulation requirements as
applicable. (It may be a second 400W/500W Series unit.)
c) Operations approval ay be granted for the use of the 400W Series unit RAIM
prediction function in lieu of the Prediction Program for operators requiring
this capability. Refer to your appropriate civil aviation authorities for these
authorizations.
FAA APPROVED
90-0 226-06 Rev. I
Page 4 of 4 DATE: __
~SE.-f?2720 0