Garmin | G1000 NXi: Cessna 206H/T206H Nav III | Garmin G1000 NXi: Cessna 206H/T206H Nav III FAA Approved Airplane Flight Manual Supplement, G1000 NXi System for Textron Nav III Series Aircraft

Garmin G1000 NXi: Cessna 206H/T206H Nav III FAA Approved Airplane Flight Manual Supplement, G1000 NXi System for Textron Nav III Series Aircraft
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GARMIN Ltd. or its subsidiaries
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GARMIN International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
Textron NAV III G1000 NXi
Page 2 of 23
190-02128-02 Rev. 1
FAA APPROVED
GARMIN International, Inc.
Log of Revisions
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual
Supplement for
G1000 NXi Integrated Avionics System and GFC 700 AFCS for Textron NAV III
REV
NO.
PAGE
NO(S)
1
ALL
190-02128-02 Rev. 1
FAA APPROVED
DESCRIPTION
Original Issue
DATE OF
APPROVAL
FAA APPROVED
See Cover
See Cover
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190-02128-02 Rev. 1
FAA APPROVED
Table of Contents
GENERAL ................................................................................................... 7
LIMITATIONS ............................................................................................ 13
EMERGENCY PROCEDURES.................................................................. 14
ABNORMAL PROCEDURES .................................................................... 18
NORMAL PROCEDURES ......................................................................... 22
PERFORMANCE ....................................................................................... 22
WEIGHT AND BALANCE/EQUIPMENT LIST .......................................... 22
AIRPLANE AND SYSTEMS DESCRIPTIONS .......................................... 22
HANDLING, SERVICE, AND MAINTENANCE ......................................... 22
190-02128-02 Rev. 1
FAA APPROVED
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190-02128-02 Rev. 1
FAA APPROVED
GENERAL
The information in this supplement is FAA-approved material and must be
attached to the Pilot’s Operating Handbook and FAA Approved Airplane
Flight Manual (POH/AFM) when the airplane has been modified by
installation of the GARMIN G1000 NXi Integrated Avionics System and GFC
700 Digital Automatic Flight Guidance System in accordance with GARMIN
International, Inc. approved data, STC SA01830WI
The information in this supplement supersedes or adds to the basic Pilot’s
Operating Handbook and FAA Approved Airplane Flight Manual only as set
forth below. Users of the manual are advised to always refer to the
supplement for possibly superseding information and placarding applicable
to operation of the airplane.
The GARMIN G1000 NXi system installed in this aircraft provides a fully
integrated Display, Communications, Navigation and Flight Control System.
Functions provided by the G1000 NXi system include: Primary Flight
Information, Powerplant Monitoring, Navigation, Communication, Traffic
Surveillance, TAWS Class B, Weather Avoidance, and a two-axis automatic
flight control / flight director system.
Use of this supplement requires the installation of Garmin G1000 NXi
hardware and system software version 2501.00, or later, in the aircraft.
Pilots are advised to carefully review the contents of this revision before
operating the airplane.
The installed ADS-B OUT system has been shown to meet the equipment
performance requirements of 14 CFR 91.227.
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 7 of 23
USE OF THE AFMS
The following definitions apply to WARNINGS, CAUTIONS and NOTES
found throughout the AFMS:
WARNING
OPERATING PROCEDURES, TECHNIQUES, ETC.,
WHICH COULD RESULT IN PERSONAL INJURY OR
LOSS OF LIFE IF NOT CAREFULLY FOLLOWED.
CAUTION
OPERATING PROCEDURES, TECHNIQUES, ETC.,
WHICH COULD RESULT IN DAMAGE TO
EQUIPMENT IF NOT CAREFULLY FOLLOWED.
NOTE
Operating procedures, techniques, etc., which is considered
essential to emphasize.
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
SYMBOLS, ABBREVIATIONS AND TERMINOLOGY
The following glossary is applicable within the airplane flight manual
supplement
AC
Advisory Circular
ADC
Air Data Computer
ADF
Automatic Direction Finder
ADS-B
Automatic Dependent Surveillance - Broadcast
AFCS
Automatic Flight Control System
AFM
Airplane Flight Manual
AFMS
Airplane Flight Manual Supplement
AHRS
Attitude and Heading Reference System
ALT
Altitude, or AFCS altitude hold mode, or ALT button on
the GDU.
AMMD
Airport Moving Map Display
AP
Autopilot
ATC
Air Traffic Control
AUX
Auxiliary
BARO
Barometric Setting
BC
Back Course
CDI
Course Deviation Indicator
COM
Communication radio
CWS
Control Wheel Steering
DME
Distance Measuring Equipment
DR
Dead Reckoning
EIS
Engine Indication System
FD
Flight Director
FIS-B
Flight Information Service-Broadcast
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
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FLC
AFCS Flight Level Change mode, or FLC button on the
GDU.
FLTA
Forward Looking Terrain Awareness
FMS
Flight Management System
FPL
Flight Plan
GA
Go-around or Garmin Antenna
GDU
Garmin Display Unit
GEA
Garmin Engine/Airframe Unit
GFC
Garmin Flight Control
GNSS
Global Navigation Satellite System
GP
GPS Glide Path
GPS
Global Positioning System
GPWS
Ground Proximity Warning System
GS
Glide Slope
HDG
AFCS heading mode or the HDG button on the GDU.
HSI
Horizontal Situation Indicator
IFR
Instrument Flight Rules
ILS
Instrument Landing System
INH
Inhibit
LNAV
Lateral Navigation
LNAV + V
Lateral Navigation with Advisory Vertical Guidance
LNAV/VNAV
Lateral Navigation / Vertical Navigation
LOC
Localizer
LOI
Loss of Integrity (GPS)
LP
Localizer Performance
LPV
Localizer Performance with Vertical Guidance
MAXSPD
Maximum Speed, AFCS Overspeed Protection mode
MFD
Multi Function Display
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
MSL
Mean Sea Level
NAV
Navigation, or AFCS navigation mode, or NAV button
on the GDU.
NEXRAD
Next Generation Radar (XM/FIS-B Weather Product)
NM
Nautical Mile
OAT
Outside Air Temperature
ODA
Organization Designation Authorization
OPT
Option
PDA
Premature Descent Alert
PFD
Primary Flight Display
PFT
Pre-Flight Test
PIT
AFCS Pitch Mode
POH
Pilot’s Operating Handbook
PROC
Procedure Button on the GDU
PTCH
Pitch
ROL
AFCS roll mode
SBAS
Satellite Based Augmentation System
STC
Supplemental Type Certificate
SVT
Synthetic Vision Technology
TAWS
Terrain Awareness and Warning System
TWY
Taxiway
VAPP
AFCS VOR Approach Mode
VFR
Visual Flight Rules
VMC
Visual Meteorological Conditions
VNAV
Vertical Navigation
VNV
Vertical Navigation Button on the GDU
VOR
VHF Omni-directional Range
VPTH
Vertical Path
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 11 of 23
VS
Vertical Speed
WAAS
Wide Area Augmentation System
WFDE
WAAS Fault Detection/Exclusion
WGS-84
World Geodetic System – 1984
XM LTNG
XM Satellite System Lighting
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
LIMITATIONS
INTRODUCTION
This AFMS is applicable to the System Software Version 2501.00. The
System Software Version number is displayed at the top right side of the
MFD Power-up page.
COCKPIT REFERENCE GUIDE
The G1000 NXi Cockpit Reference Guide, GARMIN part number
190-02178-00, for Textron NAVIII series aircraft must be immediately
available to the pilot during all phases of flight. Use the G1000 NXi Cockpit
Reference Guide, GARMIN part number 190-02178-00, Revision A or later
revision when system software 2501.00, or later, is installed.
G1000 NXI LIMITATIONS
GROUND MANEUVERING
Do not use SafeTaxi, FliteCharts, ChartView, or SurfaceWatch functions as
the basis for ground maneuvering. These functions do not comply with the
requirements of AC 20-159 and are not qualified to be used as an airport
moving map display (AMMD). These functions are to be used by the flight
crew to orient themselves on the airport surface to improve pilot situational
awareness during ground operations
IFR/VFR CHARTS
Do not use the IFR/VFR CHARTS page for pilotage navigation. The
IFR/VFR CHARTS are intended only to improve pilot situational
awareness.
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 13 of 23
DATA LINK WEATHER (XM, OR FIS-B WEATHER)
Use of the NEXRAD, XM LTNG data on the MAP – NAVIGATION MAP,
MAP – WEATHER DATA LINK (XM) and MAP – WEATHER DATA LINK
(FIS-B) pages for hazardous weather, e.g., thunderstorm penetration, is
prohibited. Datalink weather information displayed by the G1000 NXi
system is limited to supplemental use only. XM, or FIS-B weather data is
not a source of official weather information and is intended only as an aid to
enhance situational awareness of hazardous weather.
FMS FLIGHT PLAN
Do not delete the arrival airport or runway waypoint within a loaded arrival
procedure. Arrival procedures loaded into the G1000 NXi FMS must be
associated with the destination airport.
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
EMERGENCY PROCEDURES
AUTOMATIC FLIGHT CONTROL SYSTEM (IF
EQUIPPED)
SURFACEWATCH WARNING (IF EQUIPPED)
TAXIWAY TAKEOFF
(Red
Message)
1.
2.
3.
4.
Annunciator Is Displayed and Aural “Taxiway”
Takeoff .................................................................................... ABORT
Throttle Control ........................................................................... IDLE
Brakes ...................................................................................... APPLY
Aircraft Position and Runway Assignment ........................... CONFIRM
If Aircraft Position and Runway Assignment are Correct:
5. SurfaceWatch Alerts ...................................................................... OFF
•
From the MFD AUX – System Setup page
•
Set SurfaceWatch Alerts: OFF
NOTE
SurfaceWatch Alerts should be turned ON as soon as
practical after takeoff to restore functionality for remainder
of flight.
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 15 of 23
TAXIWAY LANDING
(Red
Message)
Annunciator Is Displayed and Aural “Taxiway”
1. BALKED LANDING Procedure .......................................... EXECUTE
2. Aircraft Position and Runway Assignment ........................... CONFIRM
If Aircraft Position and Runway Assignment are Correct:
3. SurfaceWatch Alerts ...................................................................... OFF
•
From the MFD AUX – System Setup page
•
Set SurfaceWatch Alerts: OFF
NOTE
SurfaceWatch Alerts should be turned ON as soon as
practical after landing to restore functionality for ground
operations.
RUNWAY TOO SHORT DURING TAKEOFF
(Red
Short” Message)
Annunciator Is Displayed and Aural “Runway Too
1. Takeoff .................................................................................... ABORT
2. Throttle Control ........................................................................... IDLE
3. Brakes ..................................................................................................
APPLY
4. Aircraft Position and Runway Assignment ............................... Confirm
5. Ensure correct origin, runway, and required takeoff distance have
been entered into the G1000 system.
• From the FPL – SurfaceWatch Setup page
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
RUNWAY TOO SHORT DURING LANDING
(Red
Short” Message)
Annunciator Is Displayed and Aural “Runway Too
1. BALKED LANDING Procedure .......................................... EXECUTE
2. Aircraft Position and Runway Assignment ........................... CONFIRM
3. Ensure correct destination, runway, and required landing distance
have been entered into the G1000 NXi system:
• From the FPL – SurfaceWatch Setup page
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 17 of 23
ABNORMAL PROCEDURES
SURFACEWATCH CAUTION MESSAGES (IF
EQUIPPED)
CHECK RUNWAY DURING TAKEOFF
(Amber
RUNWAY”)
annunciator displayed on PFD and aural “CHECK
This caution alert is issued when the aircraft is taking off from a runway
different than that entered in the FPL – SurfaceWatch Setup Page on the
MFD.
1. Aircraft Position/Runway Assignment .................................. CONFIRM
If Aircraft Position and Runway Assignment are Correct:
2. Takeoff ........................................................ CONTINUE AS DESIRED
If Aircraft Position and Runway Assignment are Not Correct or Cannot
be Determined:
3. Takeoff ......................................................................................ABORT
4. Throttle Control … ................................................ …IDLE (pull full out)
5. Brakes …………………… .......................................... ………….APPLY
6. Enter correct origin, runway, and required takeoff distance into the
G1000 NXi system:
• From the FPL – SurfaceWatch Setup Page on the MFD.
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190-02128-02 Rev. 1
FAA APPROVED
CHECK RUNWAY DURING LANDING
(Amber
RUNWAY”)
annunciator displayed on PFD and aural “CHECK
This caution alert is issued when the aircraft is landing on a runway
different than that entered on the MFD FPL – SurfaceWatch Setup Page.
1. Aircraft Position/Runway Assignment .................................. CONFIRM
If Aircraft Position and Runway Assignment are Correct:
2. Approach and Landing ................................ CONTINUE AS DESIRED
If Aircraft Position and Runway Assignment are Not Correct or
Cannot be Determined:
3. BALKED LANDING Procedure ............................................ EXECUTE
4. Enter correct destination, runway, and required landing distance into
the G1000 NXi system:
•
From the FPL – SurfaceWatch Setup Page on the MFD.
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 19 of 23
SURFACEWATCH SYSTEM MESSAGES (IF
EQUIPPED)
SURFACEWATCH INHIBITED
During certain flight operations, there may be a desire by the crew to inhibit
the SurfaceWatch system, although it is considered abnormal to do so. Use
the following procedures to inhibit the SurfaceWatch system:
1. MFD AUX – System Setup Page ................................................. VIEW
2. SurfaceWatch Alerts ............................................................... SELECT
3. SurfaceWatch Alerts ....................................................... SELECT OFF
NOTE
After inhibiting SurfaceWatch, the following will post as an
alert on the PFD, in the Alerts window:
“SURFACEWATCH INHIBITED SurfaceWatch Inhibited.”
SurfaceWatch Alerts will remain inhibited until manually uninhibited by the pilot, or a power-cycle of the system. After
a shutdown of the G1000 NXi system, SurfaceWatch will
return to its normal state of operation and will not be
inhibited.
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190-02128-02 Rev. 1
FAA APPROVED
SURFACEWATCH FAIL
If any of the required inputs for SurfaceWatch operation are failed, invalid, or
unavailable (such as GPS position), SurfaceWatch will be inoperative until
the required parameters are restored. If SurfaceWatch has failed, the
following will post as a message on the PFD, in the Alerts window:
“SURFACEWATCH FAIL One or more inputs invalid.”
SurfaceWatch will automatically return to its normal state of operation
without crew action once the required inputs are restored.
NO SURFACEWATCH RUNWAY POSITION DATA
There are certain runways at various worldwide airports that do not have
valid position data for the SurfaceWatch system to use. If such a runway is
entered into the system for either takeoff or landing via the FPL –
SurfaceWatch Setup Page on the MFD, the following will post as a message
on the PFD, in the alerts window:
“NO RUNWAY POSITION DATA Inhibit SurfaceWatch. No
runway position data.”
SurfaceWatch should then be inhibited according to the SURFACEWATCH
INHIBIT procedures outlined above. Failure to do so will result in nuisance
TWY TAKEOFF or TWY LANDING warnings as applicable. After performing
the takeoff or landing with SurfaceWatch inhibited, the system should be uninhibited as soon as practical so that functionality will be restored for the
remainder of the flight.
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
Page 21 of 23
NORMAL PROCEDURES
No Change. Refer to Pilot’s Operating Handbook and FAA Approved
Airplane Flight Manual or appropriate supplement.
PERFORMANCE
No Change. Refer to Pilot’s Operating Handbook and FAA Approved
Airplane Flight Manual or appropriate supplement.
WEIGHT AND BALANCE/EQUIPMENT LIST
No Change. Refer to Pilot’s Operating Handbook and FAA Approved
Airplane Flight Manual or appropriate supplement.
AIRPLANE AND SYSTEMS DESCRIPTIONS
STANDARD AVIONICS
GSU 75 AIRDATA, ATTITUDE AND HEADING REFERENCE
SYSTEM (ADAHRS) AND MAGNETOMETER (GMU)
If installed, the optional GSU 75 ADAHRS combines information from the
airplane’s pitot/static system, as well as the aircraft’s attitude, to provide the
following indications on the G1000 NXi displays: attitude, altitude, airspeed,
true airspeed, vertical speed, OAT, and heading information. The ADAHRS
is located in the tailcone of the airplane, and contains both an Air Data
Computer (ADC), as well as an Attitude and Heading Reference System
(AHRS). The magnetometer, located in the left wing panel, provides
heading information to the ADAHRS unit.
HANDLING, SERVICE, AND MAINTENANCE
No Change. Refer to Pilot’s Operating Handbook and FAA Approved
Airplane Flight Manual or appropriate supplement.
Textron NAV III G1000 NXi
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190-02128-02 Rev. 1
FAA APPROVED
OTHER PROCEDURES
ADS-B OUT
The installed ADS-B OUT system has been shown to meet the equipment
performance requirements of 14 CFR 91.227.
The ADS-B OUT system should be operational during all phases of flight,
including airport surface movement operations.
The ADS-B OUT system is operational when the transponder is in the ON or
ALT mode. This will be indicated in the transponder window in the lower right
corner of the PFD.
If the G1000 NXi system is unable to transmit ADS-B OUT messages, the
following message will post on the PFD in the alerts window:
XPDR1 ADS-B NO POS – Transponder: ADS-B is not transmitting position.
If the above message is received, verify valid GPS position is available.
1. MFD AUX – GPS Status Page........................... VERIFY GPS Position
PRESSURE ALTITUDE BROADCAST INHIBIT
While conducting operations within airspace that requires ADS-B Out
transmissions, operate the transponder in ALT mode unless requested
otherwise by ATC. If ATC requests the inhibit of pressure altitude
transmissions, select the transponder to ON mode:
1. XPDR Softkey on PFD .............................................................. PRESS
2. ON Softkey ............................................................................... PRESS
190-02128-02 Rev. 1
FAA APPROVED
Textron NAV III G1000 NXi
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