Garmin | G1000 NXi: Beechcraft Baron G58 | Garmin G1000 NXi: Beechcraft Baron G58 FAA Approved Airplane Flight Manual Supplement, G1000 NXi System for Textron Aviation G36 Bonanza and G58 Baron Aircraft

Garmin G1000 NXi: Beechcraft Baron G58 FAA Approved Airplane Flight Manual Supplement, G1000 NXi System for Textron Aviation G36 Bonanza and G58 Baron Aircraft
© Copyright 2018
GARMIN Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be
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of GARMIN. GARMIN hereby grants permission to download a single copy
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and provided further that any unauthorized commercial distribution of this
manual or any revision hereto is strictly prohibited.
GARMIN International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
Textron G36, G58 G1000 NXi
Page 2 of 32
190-02128-03 Rev. 2
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 G36, G58
REV
NO.
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
r Robert G. Murray,
1
2
ALL
Original Issue
12/20/2016
ALL
Added Enhanced
AFCS, TAWS, ADSB and QFE
Procedures
See Cover
190-02128-03 Rev. 2
FAA APPROVED
ODA STC Unit
Administrator
GARMIN International, Inc.
ODA-240087-CE
See Cover
Textron G36, G58 G1000 NXi
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Textron G36, G58 G1000 NXi
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190-02128-03 Rev. 2
FAA APPROVED
Table of Contents
General ...................................................................................................... 7
Limitations .............................................................................................. 14
Introduction ............................................................................................. 14
Emergency Procedures .......................................................................... 17
Abnormal Procedures ............................................................................ 23
Normal Procedures ................................................................................. 27
Performance ............................................................................................ 28
Weight and Balance/Equipment List ..................................................... 28
Airplane and Systems Descriptions ...................................................... 28
Handling, Service, and Maintenance ..................................................... 28
Other Procedures ................................................................................... 29
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
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Textron G36, G58 G1000 NXi
Page 6 of 32
190-02128-03 Rev. 2
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 3185.00, 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.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 7 of 32
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 G36, G58 G1000 NXi
Page 8 of 32
190-02128-03 Rev. 2
FAA APPROVED
ELECTRONIC FLIGHT BAG
Electronic aeronautical charts displayed on this system have been shown to
meet the guidance in AC 120-76D as a Type B Electronic Flight Bag (EFB)
for FliteCharts and ChartView. Additional requirements may make a
secondary source of aeronautical charts necessary on the aircraft and
available to the pilot, such as traditional paper charts or an additional
portable electronic device. If the secondary source of aeronautical charts is
a Portable Electronic Device (PED), its use must be consistent with the
guidance in AC 120-76D.
For operations under 14 CFR Part 91, it is suggested that a secondary or
back up source of aeronautical information necessary for the flight be
available to the pilot in the airplane. If the source of aeronautical information
is in electronic format, operators must determine non-interference with the
G1000 NXi system and existing aircraft systems for all flight phases.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in
accordance with RTCA/DO-200A and AC 20-153B for database integrity,
quality, and database management processes for many of its aviation
databases. LOA status and RTCA/DO-200A List of Applicable Avionics (19001999-00) can be viewed at FlyGarmin.com.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 9 of 32
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
ESP
Electronic Stability and Protection
FD
Flight Director
Textron G36, G58 G1000 NXi
Page 10 of 32
190-02128-03 Rev. 2
FAA APPROVED
FIS-B
Flight Information Service-Broadcast
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
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 11 of 32
MFD
Multi Function Display
MPS
Meters per second
MSL
Mean Sea Level
MT
Meters
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
QFE
Atmospheric pressure at airport elevation (field
elevation equals zero feet)
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
USP
Autopilot Underspeed Protection
VAPP
AFCS VOR Approach Mode
Textron G36, G58 G1000 NXi
Page 12 of 32
190-02128-03 Rev. 2
FAA APPROVED
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
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
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 13 of 32
LIMITATIONS
INTRODUCTION
This AFMS is applicable to the System Software Version 3185.00. 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 Guides, GARMIN part number
190-02180-01 (G36) and 190-02182-01 (G58), for Textron G36 and G58
aircraft must be immediately available to the pilot during all phases of flight.
Use the G1000 NXi Cockpit Reference Guide, GARMIN part number 19002180-01, Revision A (G36) or later revision and 190-02182-01, Revision B
(G58) or later revision when system software 3185.00, 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.
Textron G36, G58 G1000 NXi
Page 14 of 32
190-02128-03 Rev. 2
FAA APPROVED
TRAFFIC AVOIDANCE SYSTEM LIMITS
Use of the MAP - TRAFFIC MAP, Inset Map traffic display, or the SVT display
to maneuver the airplane for traffic avoidance without outside visual
reference is prohibited. The Traffic Information System (TIS) or optional
Skywatch TAS, Skywatch HP, Honeywell KTA-870, and Garmin GTS
820/850/8000 Traffic Systems are intended as an aid for the pilot to visually
locate traffic. It is the responsibility of the pilot to see and manually maneuver
the airplane to avoid other traffic.
Maneuvers based solely on a traffic advisory (TA) or on information
displayed on a traffic display are not authorized. Pilots are authorized to
deviate from their current ATC clearance to comply with a TCAS II resolution
advisory (RA). When responding to a TCAS RA warning, the autopilot must
be immediately disconnected and the evasive maneuver hand flown by the
pilot.
DATA LINK WEATHER (XM, CONNEXT, OR FIS-B WEATHER)
Datalink weather information displayed by the G1000 NXi system is limited
to supplemental use only. XM, Garmin Connext, or FIS-B weather data is
not a source of official weather information. Use of the NEXRAD, PRECIP,
XM LTNG and DL LTNG (Datalink Lightning) data on the MAP –
NAVIGATION MAP, MAP – WEATHER DATA LINK (XM), MAP –
WEATHER DATA LINK (CNXT), and MAP – WEATHER DATA LINK (FISB) pages for hazardous weather, e.g., thunderstorm penetration, is
prohibited.
NEXRAD, PRECIP, XM LTNG and DL LTNG information on the MAP –
NAVIGATION MAP, MAP – WEATHER DATA LINK (XM), MAP –
WEATHER DATA LINK (CNXT), and MAP – WEATHER DATA LINK (FISB) pages is intended only as an aid to enhance situational awareness of
hazardous weather, not penetration. It is the pilot’s responsibility to avoid
hazardous weather using official weather data sources and the airplane’s inflight weather radar.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 15 of 32
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 G36, G58 G1000 NXi
Page 16 of 32
190-02128-03 Rev. 2
FAA APPROVED
EMERGENCY PROCEDURES
UNDERSPEED PROTECTION ACTIVATION AND RECOVERY
(IF EQUIPPED)
(Red
equipped aircraft)
Warning Annunciator on the PFD on ESP-
May also be accompanied by an amber
annunciator above the
airspeed tape display and aural “AIRSPEED” alert)
1. Throttle Control.................. INCREASE POWER AS REQUIRED TO
CORRECT UNDERSPEED CONDITION
2. Aircraft Attitude and Altitude ........................................... MONITOR
After underspeed condition is corrected:
3. Autopilot .............. RESELECT VERTICAL AND LATERAL MODES (if
necessary)
4. Throttle Control .......................................... ADJUST AS NECESSARY
NOTE
Autopilot Underspeed Protection mode provides a pitch
down command to maintain sufficient airspeed. When
power is applied to correct the underspeed condition the
resulting nose up attitude may be high to climb back to the
programmed vertical path. Underspeed Protection Mode
recovery is not available below 200 feet AGL (61 meters),
except in go-around (GA) mode.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 17 of 32
ESP ACTIVATION (IF EQUIPPED)
1. Power......................................................................... AS REQUIRED
2. Aircraft Attitude .............................. MAINTAIN/REGAIN CONTROL
NOTE
If ESP is active for at least 50% of the last 20 seconds, the
autopilot will automatically engage in LVL mode, an aural
‘ENGAGING AUTOPILOT’ alert will be played, and the
autopilot will roll the wings level and fly at zero-vertical speed.
3. Autopilot Modes........................................................... AS DESIRED
Textron G36, G58 G1000 NXi
Page 18 of 32
190-02128-03 Rev. 2
FAA APPROVED
WIRE OBSTACLE
(Red WIRE AHEAD – PULL UP annunciator Is displayed and aural “WIRE
AHEAD PULL UP” Message)
1. AP DISC / TRIM INTER Button ............ PRESS and RELEASE
(To disconnect the autopilot)
2. Aircraft Attitude ............. PULL BACK ON CONTROL WHEEL
3. Power................................................ MAXIMUM ALLOWABLE
4. Airspeed .............................. BEST ANGLE OF CLIMB SPEED
After Warning Ceases:
1. Power ............................................... MAXIMUM CONTINUOUS
2. Altitude ..................... CLIMB AND MAINTAIN SAFE ALTITUDE
3. Advise ATC of Altitude Deviation, if appropriate.
NOTE
Only vertical maneuvers are recommended, unless either
operating in visual meteorological conditions (VMC), or the pilot
determines, based on all available information, that turning in
addition to the escape maneuver is the safest course of action,
or both.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 19 of 32
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:
1. 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.
Textron G36, G58 G1000 NXi
Page 20 of 32
190-02128-03 Rev. 2
FAA APPROVED
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:
1. 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)
1.
2.
3.
4.
5.
annunciator Is Displayed and Aural “Runway Too
Takeoff ................................................................................... ABORT
Throttle Control.......................................................................... IDLE
Brakes .................................................................................... APPLY
Aircraft Position and Runway Assignment ...............................Confirm
Ensure correct origin, runway, and required takeoff distance have
been entered into the G1000 system from the FPL – SurfaceWatch
Setup page.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 21 of 32
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.
Textron G36, G58 G1000 NXi
Page 22 of 32
190-02128-03 Rev. 2
FAA APPROVED
ABNORMAL PROCEDURES
TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) OR
WIRE OBSTACLE CAUTION
(Amber TERRAIN or CAUTION - WIRE annunciator Is displayed with aural
message)
1. When a TAWS or WIRE OBSTACLE CAUTION occurs, take positive
corrective action until the alert ceases. Stop descending or initiate either
a climb or a turn, or both, as necessary, based on analysis of all available
instruments and information.
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:
1. Takeoff ....................................................... CONTINUE AS DESIRED
If Aircraft Position and Runway Assignment are Not Correct or Cannot
be Determined:
1. Takeoff...................................................................................... ABORT
2. Throttle Control … ................................................ …IDLE (pull full out)
3. Brakes …………………… ......................................... …………. APPLY
4. Enter correct origin, runway, and required takeoff distance into the
G1000 NXi system from the FPL – SurfaceWatch Setup Page on the
MFD.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 23 of 32
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.
Textron G36, G58 G1000 NXi
Page 24 of 32
190-02128-03 Rev. 2
FAA APPROVED
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 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.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 25 of 32
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.
Textron G36, G58 G1000 NXi
Page 26 of 32
190-02128-03 Rev. 2
FAA APPROVED
NORMAL PROCEDURES
DISABLING ESP (IF EQUIPPED)
(ESP OFF message on PFD)
ESP may be disabled in the Aux – System Setup 2 page on the MFD. In the
Stability & Protection group, highlight Enabled. Change Enabled to Disabled.
COUPLED GO-AROUND (IF EQUIPPED)
1. GO AROUND button .................... PRESS - Verify GA/GA in AP mode
selection window on PFD
autopilot will not disengage
2. Power .......................................................... APPLY Go Around power
3. MFD Bezel ........ PRESS NAV to couple to selected navigation source
OR;
PRESS HDG to Fly ATC Assigned Missed Approach Heading
4. Altitude Preselect ........................... VERIFY Set to appropriate altitude
5. Aircraft Attitude ................................................................... MONITOR
NOTE
The pilot is responsible for initial missed approach guidance
in accordance with published procedure. When the GA
button is pressed the Flight Director command bars will
command go-around pitch attitude and wings-level. The
pilot must select the CDI to the appropriate navigation
source and select the desired lateral and vertical flight
director modes.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 27 of 32
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 G36, G58 G1000 NXi
Page 28 of 32
190-02128-03 Rev. 2
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
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 29 of 32
QFE
On ground, if QFE operations are required:
1. BARO setting ............................ Set to appropriate QFE BARO setting
2. View the MFD Aux – System Setup 1 page.
3. BARO QFE REF ....................................... Set (Manual or FMS ORIG)
4. BARO QFE ELEV ............Set if Manual REF, verify if FMS ORIG REF
5. BARO QFE Off/On.................................................................... Set On
This will make QFE mode active, as indicated by black QFE text on
green box in upper right corner of both PFD attitude display.
In Flight, before QFE operations are required:
1. BARO setting .................................. STD BARO or QFE BARO setting
2. View the MFD Aux – System Setup 1 page.
3. BARO QFE REF ....................................... Set (Manual or FMS DEST)
4. BARO QFE ELEV ........... Set if Manual REF, verify if FMS DEST REF
5. BARO QFE Off/On.................................................................... Set On
If STD BARO is set then this will Arm QFE, as indicated by black
QFE text on white box in upper right corner of the PFD attitude
display. QFE mode will not yet be active if baro setting is STD
BARO. Changing the baro setting to a numerical value will activate
QFE. If STD BARO is not set, this will activate QFE as indicated by
black QFE text on a green box in upper right corner of the PFD
attitude display.
NOTE
Changing the baro setting to STD BARO while QFE is active disables
QFE. Selecting QFE On while the baro setting is STD BARO arms
QFE which is indicated by black QFE text on a white box. When QFE
is armed, changing the baro setting to a number activates QFE,
which is indicated by green QFE text on a green box.
Textron G36, G58 G1000 NXi
Page 30 of 32
190-02128-03 Rev. 2
FAA APPROVED
NOTE
Changing the BARO setting while in Autopilot ALT mode will result in
the AFCS slowly climbing or descending to eventually recover to the
original indicated altitude.
Indicated Altitude on Aux – Trip Planning page will always display
MSL altitude, which may not match indicated altitude if QFE is
enabled.
When QFE is toggled on or off, the following altitude displays will be
converted by the system: Flight Plan altitude constraints, active VNV
Profile altitude, ESA and MSA, BARO Transition Alert Altitude,
and VSD altitude constraints. These will be displayed with
parentheses to indicate QFE altitudes, and without parentheses to
indicate MSL altitudes. Flight Levels will NOT be converted.
The following will not be converted by the system, and will not be
displayed with parentheses: PFD indicated altitude, PFD selected
altitude, and approach minimums altitude.
190-02128-03 Rev. 2
FAA APPROVED
Textron G36, G58 G1000 NXi
Page 31 of 32
METRIC ALT / VS UNITS
If operation with Metric Altitude and Vertical Speed units is desired or
required:
1. View the MFD Aux – System Setup 1 page.
2. Display Units – ALT, VS.................................. Set to Meters (MT, MPS)
If Metric Altitude and Vertical Speed units are displayed and English units
display is desired or required:
1. View the MFD Aux – System Setup 1 page.
2. Display Units – ALT,VS....................................... Set to Feet (FT, FPM)
Textron G36, G58 G1000 NXi
Page 32 of 32
190-02128-03 Rev. 2
FAA APPROVED
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