Garmin SR02080SE Owner's Manual
GARMIN Ltd. or its subsidiaries
c/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
FAA APPROVED
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGAnON SYSTEM
As Installed In
Bell 206B
Reg. No.
This document serves as a Rotorcraft Flight Manual Supplement when the rotorcraft is
equipped with the Garmin 400W Series unit. This document must be carried in the
rotorcraft at all times when the
STC SR02080SE.
The information contained herein supplements or supersedes the information made
available to the operatorbythe manufacturer in the form of clearly stated placards,
markings, or manuals or in the
in those areas listed herein. For limitations, procedures and performance
contained in this document, consult the basic placards, markings, or manuals or the basic
FAA approved Rotorcraft Flight Manual.
FAA APgOVED
Garmin
form of
SIN _
400W Series unit is installed in accordance with
an FAA approved Rotorcraft Flight Manual, only
information
not
~~~
J;<y Manager, Flight Test Branch
Federal Aviation Administration
Seattle Aircraft Certification Office
DATE:~
190-01226-06 Rev. 1
Page I of 14
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS.WAAS NAVIGATION SYSTEM
Page
Rev. No. No. Date
GARMIN Ltd. or its subsidiaries
c/o Garmin International
Bell 206B
LOG OF REVISIONS
Description
FAA Approved
1
Original
All
Complete
Supplement
~,,-r~
Mgr. Fit.TestBr.
Federal Aviation Administration
Seattle Aircraft Certification Office
'1/-.:,
Date
..
II")
190-01226-06 Rev. I
Page 2 of 14
GARMIN Ltd. or its subsidiaries
c/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGATION SYSTEM
Bell 206B
Table of Contents
Section I. LIMITATIONS 4
I. I Pilot's Guide 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. EMERGENCY PROCEDURES 8
2.1 Emergency Procedures 8
2.2 Abnormal Procedures 8
Section 3. NORMAL PROCEDURES 9
3.1 Approaches with Vertical Guidance 9
3.2 WFDE Prediction Program 9
3.3 HTAWS Controls 10
3.4 IITAWSAlerts II
3.5 G500H Interface 12
Section 4. PERFORMANCE 12
GENERAL 13
Garmin 400W Series GPSiWAAS Nav Com 13
Operation 14
Class II Oceanic, Remote, and other Operations 14
FAA APPROVED
190-01226-06 Rev. I
Page 3 of 14
DATE:
SEP 2 7 2010
GARMIN Ltd. or its subsidiaries
c/o Garmin International
1200 E. 151" 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 Guide
The GARMIN 400W Series Pilot's Guide, 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 190-00356-00 Rev G
400W/500W Series Optional Displays PIN 190-00356-30 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 GPS 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 Guide for further information.
Table 1 - Almroved Software Versions
Approved Software Version
Software Item
Main SW Version
GPS SW Version
(or lacer FAA annroved versions (or chis STCJ
SW version
4.01
3.2
As disnlaved on unit
4.01
3.2
190-01226-06 Rev. I
Page 4 of 14
FAA APPROVED
DATE:
-----
SEP 27 2010
GARMIN Ltd. or its subsidiaries
c/o Gannin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGATION 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 by 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 890(degrees) north latitude or south of 890(degrees)
south latitude.
190-01226-06 Rev. I
Page 5 of 14
FAA APPROVED
DATE: __
SE_P_2 7
2010
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