Garmin | G1000 NXi: Cessna Citation Mustang | Garmin G1000 NXi: Cessna Citation Mustang Airplane Flight Manual Supplement, G1000 NXi and GFC700 in Textron Model 510 Mustang

Garmin G1000 NXi: Cessna Citation Mustang Airplane Flight Manual Supplement, G1000 NXi and GFC700 in Textron Model 510 Mustang
© Copyright 2019
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
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 2 of 44
190-02450-02 Rev. 1
FAA APPROVED
Garmin International, Inc.
Log of Revisions
FAA Approved Airplane Flight Manual Supplement for
G1000 NXi Integrated Avionics System and GFC 700 AFCS In Citation Mustang
MODEL 510
REV
NO.
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
1
ALL
Original Issue
See Cover
See Cover
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
Table of Contents
Section I – General ...................................................................................................................................... 7
Section II – Operating Limitations ............................................................................................................. 12
Section III – Operating Procedures ........................................................................................................... 29
Section IV – Performance ......................................................................................................................... 37
Section V – Supplements .......................................................................................................................... 39
Section VI – Weight and Balance .............................................................................................................. 41
Section VII – Advisory Information ............................................................................................................ 43
190-02450-02 Rev. 1
FAA APPROVED
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190-02450-02 Rev. 1
FAA APPROVED
Section I – GENERAL
The information in this supplement is FAA-approved material and must be attached to the FAA Approved
Airplane Flight Manual (AFM) when the airplane has been modified by installation of the Garmin G1000
NXi avionics upgrade in accordance with Garmin International, Inc. approved data, STC SA01896WI.
The information in this supplement supersedes or adds to the basic AFM 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 the Cessna Citation Mustang MODEL 510 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 three-axis automatic flight
control / flight director system.
Use of this supplement requires the installation of Garmin G1000 NXi hardware and system software
version 0413.41 or later in the aircraft. Pilots are advised to carefully review the contents of this revision
before operating the airplane.
The following table lists the Pilot’s Guide and Cockpit Reference Guide applicable to the respective system
software version.
System Software
Version
0413.41 or later
Pilot’s Guide
Part Number
190-02522-00
Revision A or later
Cockpit Reference Guide
Part Number
190-02523-00
Revision A or later
Table 1 - Applicable Pilot's Guide and Cockpit Reference Guide
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.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 7 of 44
ELECTRONIC FLIGHT BAG
Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC 12076D 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 (190-01999-00) can be
viewed at FlyGarmin.com.
REDUCED VERTICAL SEPARATION MINIMUMS (RVSM)
This airplane is equipped for operations in Reduced Vertical Separation Minimum (RVSM) airspace when
the required equipment is maintained in accordance with the Airplane Maintenance Manual. This does not
constitute operational approval. Operational approval must be obtained in accordance with applicable
operating rules.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 8 of 44
190-02450-02 Rev. 1
FAA APPROVED
ABBREVIATIONS AND TERMINOLOGY
The following glossary is applicable within the airplane flight manual supplement
AC
Advisory Circular
ADS-B
Automatic Dependent Surveillance - Broadcast
AFCS
Automatic Flight Control System
AFM
Airplane Flight Manual
AFMS
Airplane Flight Manual Supplement
AGL
Above Ground Level
AHRS
Attitude and Heading Reference System
AIRAC
Aeronautical Information Regulation And Control
ALT
Altitude, or AFCS altitude hold mode, or ALT button on the GMC 710 AFCS
Mode Controller
AMC
Acceptable Means of Compliance
AMMD
Airport Moving Map Display
APCH
Approach
Aux
Auxiliary
B-RNAV
Basic Area Navigation
BARO
Barometric Setting
BC
Back Course
CDI
Course Deviation Indicator
DEST
Destination
DUATS
Direct User Access Terminal Service
EASA
European Aviation Safety Agency
EFB
Electronic Flight Bag
ELEV
Elevation
ESA
Enroute Safe Altitude
FDE
Fault Detection/Exclusion
FIS-B
Flight Information Service-Broadcast
FMS
Flight Management System
FPL
Flight Plan
FPM
Feet Per Minute
FRT
Fixed Radius Transitions
GDU
Garmin Display Unit
GEO
Geographic
GFC
Garmin Flight Control
GIA
Garmin Integrated Avionics Unit
GMA
Garmin Audio Panel System
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 9 of 44
GMC
Garmin Mode Control Unit
GNSS
Global Navigation Satellite System
GP
GPS Glide Path
GPS
Global Positioning System
GRS
Garmin Reference System (AHRS)
GS
Glide Slope
GTX
Garmin Transponder
HSI
Horizontal Situation Indicator
ICAO
International Civil Aviation Organization
IFR
Instrument Flight Rules
ILS
Instrument Landing System
JAA
Joint Aviation Authorities
LDA
Localizer Type Directional Aid
LNAV
Lateral Navigation
LNAV/VNAV
Lateral Navigation / Vertical Navigation
LOA
Letter of Acceptance
LOC
Localizer
LP
Localizer Performance
LPV
Localizer Performance with Vertical Guidance
MDA
Barometric Minimum Descent Altitude
MFD
Multi Function Display
MLS
Microwave Landing System
MPS
Meters per Second
MSA
Minimum Safe Altitude
MSL
Mean Sea Level
MT
Meters
NAV
Navigation
ODA
Organization Designation Authorization
P-RNAV
Precision Area Navigation
PFD
Primary Flight Display
QFE
The altimeter setting which will cause the altimeter to read the height above
the airport or runway threshold elevation.
RAIM
Receiver Autonomous Integrity Monitoring
REF
Reference
RF
Radius-to-Fix
RNAV
Area Navigation
RNP
Required Navigation Performance
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 10 of 44
190-02450-02 Rev. 1
FAA APPROVED
RVSM
Reduced Vertical Separation Minimums
SAPT
Service Availability Prediction Tool
SBAS
Satellite Based Augmentation System
SDF
Simplified Directional Facility
STC
Supplemental Type Certificate
STD
Standard
TAWS
Terrain Awareness and Warning System
TGL
Temporary Guidance Leaflet
TIS
Traffic Information System
TOAC
Time Of Arrival Control
TSO
Technical Standard Order
TWY
Taxiway
VFR
Visual Flight Rules
VNAV
Vertical Navigation
VNV
Vertical Navigation, or Vertical Navigation Button on the GMC 710 AFCS
Mode Controller
VOR
Very High Frequency Omni-directional Range
VS
Vertical Speed
VSD
Vertical Situation Display
WAAS
Wide Area Augmentation System
WFDE
WAAS Fault Detection/Exclusion
WGS-84
World Geodetic System – 1984
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 11 of 44
Section II – OPERATING LIMITATIONS
TABLE OF CONTENTS
EICAS and Instrument Markings ............................................................................................................... 13
GARMIN G1000 NXi Avionics System ...................................................................................................... 13
G1000 NXi GNSS (GPS/SBAS) Navigation System Operational Approvals ............................................ 15
G1000 NXi GNSS (GPS/SBAS) Navigation System Limitations .............................................................. 23
AHRS AREAS OF OPERATION ............................................................................................................... 26
Traffic Avoidance System Limits ............................................................................................................... 26
Data Link Weather (XM, CONNEXT, or FIS-B Weather) .......................................................................... 27
Kinds of Operations Equipment List .......................................................................................................... 27
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 12 of 44
190-02450-02 Rev. 1
FAA APPROVED
OPERATING LIMITATIONS
EICAS AND INSTRUMENT MARKINGS
No changes were made to the airplane’s power plant limitations and indicator markings. The power plant
limitations and indicator markings on the Multi Function Display (MFD) and the Primary Flight Displays
(PFDs) while in reversionary mode are marked in accordance with the airplane’s AFM.
No changes were made to the airplane’s airspeed limitations and indicator markings. The airspeed
indicators on the Primary Flight Displays (PFDs) and the standby airspeed indicator are marked in
accordance with the airplane’s AFM.
GARMIN G1000 NXI AVIONICS SYSTEM
1. The current Garmin G1000 Cockpit Reference Guide (CRG) Part Number and System Software
Version that must be available to the pilot during flight are displayed on the MFD Aux group, System
Status page.
2. Category II approaches are prohibited.
3. Takeoff is prohibited following a flight where either PFD/MFD COOLING or GIA1-2 COOLING
Garmin System Message was displayed, until the condition is identified and corrected.
4. Takeoff is prohibited with a PFD/MFD SERVICE, GIA 1-2 SERVICE, or GMA1-2 SERVICE Garmin
System Message displayed, until the condition is identified and corrected.
5. All display units must be installed and operational.
6. Takeoff with a display in reversionary mode is prohibited.
7. Autopilot:
a. One pilot must remain seated, with the seatbelt fastened, during all autopilot operations.
b. Autopilot operation is prohibited if either PFD is in AHRS reversion.
c. Autopilot Minimum-Use-Height:
1) Takeoff and Climb ............................................................................................ 700 feet AGL
2) Enroute and Descent ..................................................................................... 1000 feet AGL
3) Approach (GP or GPS Mode) .......................................................................... 200 feet AGL
4) Approach (FLC, VS, PIT, or ALT Mode) ............ Higher of 400 feet AGL or Approach MDA
8. [This limitation has been removed.]
9. Use of the NAVIGATION MAP page for pilotage navigation is prohibited unless required by AFM
procedure. The NAVIGATION MAP page is intended only to enhance situational awareness.
Navigation is to be conducted using only current charts, data, and authorized navigation facilities.
10. Use of the TRAFFIC MAP to maneuver the airplane to avoid traffic is prohibited. The TRAFFIC
INFORMATION SYSTEM (TIS) and the optional GTX 345 ADS-B Traffic system are for advisory
use only. TIS and ADS-B are intended only to help the pilot to visually locate traffic. It is the
responsibility of the pilot to see and maneuver to avoid traffic.
11. Use of the TERRAIN information for primary terrain avoidance is prohibited. The TERRAIN
information is intended only to enhance situational awareness. It is the pilot’s responsibility to
provide terrain clearance at all times.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 13 of 44
NOTE
For terrain database cycle 08T2 and earlier cycles, TERRAIN information is not available in locations
north of 75° North latitude or south of 60° South latitude due to the absence of terrain data in these
geographical areas.
12. Do not use data link weather information shown on any display for maneuvering in or near areas
of hazardous weather. The data link weather information is intended to assist in avoiding
hazardous weather. The actual age of the weather phenomena may be older than the indicated
age of the data link weather product.
13. The fuel quantity, fuel required, fuel remaining, and gross weight estimate functions of the G1000
are supplemental information only and must be verified by the flight crew.
14. Takeoff with a noticeably drifting heading indicator (1/2 degree per second or greater when the
airplane is stationary) is prohibited. AHRS failure may occur when the heading is drifting in this
manner. A constant heading offset is not an indication of a drifting heading.
15. [This limitation has been removed.]
16. 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.
17. The use of the colors red and amber within the checklist function has not been evaluated or
approved by this STC. Use of the colors red and/or amber within user created checklists may
require separate evaluation and approval by the FAA.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 14 of 44
190-02450-02 Rev. 1
FAA APPROVED
G1000 NXI GNSS (GPS/SBAS) NAVIGATION SYSTEM OPERATIONAL
APPROVALS
The Garmin G1000 NXi Integrated Avionics GNSS navigation system installed in this aircraft is a GPS
system with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145a Class 3
approved Garmin GIAs, TSO-C146d Class 3 approved Garmin GDU 1050A and GDU 1550 Display Units,
Garmin GA36 and GA37 antennas, and GPS software version 5.1 or later approved version. The G1000
GNSS navigation system in this airplane is installed in accordance with AC 20-138D. When all the
equipment is operative, the Garmin G1000 NXi system has two independent GNSS long-range navigation
systems. Failure of any of the above equipment or the posting of ‘BOTH ON GPS1’ or ‘BOTH ON GPS2’
annunciators indicates only one operational GNSS system.
The Garmin G1000 NXi Integrated Avionics GNSS navigation system as installed in this airplane complies
with the requirements of AC 20-138D and is approved for navigation using GPS and GPS/SBAS (within the
coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR en-route,
terminal area, non-precision approach, and approach procedures with vertical guidance operations.
The Garmin G1000 NXi Integrated Avionics GNSS navigation system as installed in this aircraft complies
with the equipment, performance, and functional requirements to conduct RNAV and RNP operations in
accordance with the applicable requirements of the reference documents listed in the following table. This
table is accurate at the time it was published. However, changes to operational rules, FAA advisory
circulars, flight plan formats, etc., are possible. The pilot is responsible to ensure compliance with current
operational requirements.
Operational
Requirements/
Authorization
Navigation
Specification
RNAV 10
RNP 10
Oceanic and
Remote
Areas of
Operation
(Class II
Navigation)
Reference
Documents
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is
34 minutes1.
FAA AC
20-138D
CHG 2
Two GNSS systems
required to be
operational, (one
GNSS system for
those routes requiring
only one long range
navigation system).
FAA AC
91-70A
FAA AC
90-105A
EASA AMC
20-12
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
R
A1
Notes
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote airspace without
reliance on other longrange navigation systems,
when used in conjunction
with an FDE prediction
tool that satisfies the
guidance of FAA AC 20138D and AC 90-105A (or
later revision).1
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 15 of 44
Navigation
Specification
B-RNAV /
RNAV 5
(Europe)
Operational
Requirements/
Authorization
This does not
constitute an
operational approval.
Reference
Documents
FAA AC
90-96A
CHG 1
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
R
B2
R
L1
Notes
EASA AMC
20-4A
RNP 4
Oceanic and
Remote
Areas of
Operation
(Class II
Navigation)
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is
25 minutes.1
FAA AC
20-138D
CHG 2
Two operational
long-range nav
systems required, (or
one navigation
system and one
GNSS sensor for
those routes requiring
only one long-range
navigation sensor).
FAA AC
91-70A
FAA AC
90-105A
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote airspace without
reliance on other longrange navigation systems,
when used in conjunction
with an FDE prediction
tool that satisfies the
guidance of FAA AC 20138D and AC 90-105A (or
later revision).1
Additional equipment may
be required to obtain
operational approval to
utilize RNP-4
performance.
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
RNP-2
(Oceanic/
Remote)
GNSS FDE
availability must be
verified prior to
oceanic or remote
continental flight.
Maximum predicted
FDE unavailability is
5 minutes.1
FAA AC
20-138D
CHG 2
R
TBD
FAA AC
90-105A
Two operational
long-range nav
(continued)
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 16 of 44
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote airspace without
reliance on other longrange navigation systems,
when used in conjunction
with an FDE prediction
tool that satisfies the
(continued)
190-02450-02 Rev. 1
FAA APPROVED
Operational
Requirements/
Authorization
Navigation
Specification
Reference
Documents
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
guidance of FAA AC 20138D and AC 90-105A (or
later revision).1
systems required, (or
one navigation
system and one
GNSS sensor for
those routes requiring
only one long-range
navigation sensor).
Additional equipment may
be required to obtain
operational approval to
utilize RNP-2
performance.
No time limit using
GNSS as the primary
navigation sensor.
Item 18 PBN flight plan
code is still to-bedetermined at time of
publication of this AFMS.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
RNP -2
(Domestic /
Offshore
En route)
In accordance with
AC 90-105A, Part 91
operators (except
subpart K) following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly
RNP-2 domestic and
offshore routes.
Notes
FAA AC
20-138D
CHG 2
R
TBD
Includes RNP-2 domestic
and offshore routes.
Item 18 PBN flight plan
code is still to-bedetermined at time of
publication of this AFMS.
FAA AC
90-105A
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNAV 2
The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
FAA AC
20-138D
CHG 2
R
C2
Includes RNAV Q and T
routes.
FAA AC
90-100A
CHG 2
In accordance with
AC 90-100A, CHG 2,
Part 91 operators
(except subpart K)
(continued)
following the aircraft
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 17 of 44
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
R
D2
Includes RNAV terminal
departure and arrival
procedures.
R
D2
ICAO flight plan code for
P-RNAV no longer exist.
P-RNAV utilizes RNAV 1
flight plan codes.
R
O2
Includes RNP terminal
departure and arrival
procedures. This includes
procedures with radius-tofix (RF) legs.
and training guidance
in AC 90-100A are
authorized to fly
RNAV 2 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNAV 1
The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
FAA AC
20-138D
CHG 2
FAA AC
90-100A
CHG 2
In accordance with
AC 90-100A, Part 91
operators (except
subpart K) following
the aircraft and
training guidance in
AC 90-100A are
authorized to fly
RNAV 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
P-RNAV
(Europe)
This does not
constitute an
operational approval.
FAA AC
90-96A
CHG 1
JAA TGL
10 Rev 1
RNP 1
When flying a RNP
procedure containing
a radius-to-fix (RF)
leg, the AFCS must
be operational.
(continued)
FAA AC
20-138D
CHG 2
FAA AC
90-105A
At a minimum, the
flight director must be
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 18 of 44
190-02450-02 Rev. 1
FAA APPROVED
Operational
Requirements/
Authorization
Navigation
Specification
Reference
Documents
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
R
S1
Notes
displayed and utilized
when conducting
procedures
containing RF legs.
In accordance with
AC 90-105, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly
RNP 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNP APCH
LNAV minima
When flying a RNP
procedure with a
radius-to-fix (RF) leg,
the AFCS must be
operational. At a
minimum, the flight
director must be
displayed and utilized
when conducting
procedures
containing RF legs.
FAA AC
20-138D
CHG 2
FAA AC
90-105A
EASA AMC
20-27
Includes non-precision
approaches based on
conventional navigation
aids with “or GPS” in the
title and area navigation
approaches titled “GPS”,
“RNAV (GPS)”, and
“RNAV (GNSS)”. This
includes procedures with
radius-to-fix (RF) legs.
In accordance with
AC 90-105A, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly RNP
APCH LNAV minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 19 of 44
Navigation
Specification
RNP APCH
LNAV/VNAV
minima
Operational
Requirements/
Authorization
When flying a RNP
procedure with a
radius-to-fix (RF) leg,
the AFCS must be
operational.
At a minimum, the
flight director must be
displayed and utilized
when conducting
procedures
containing RF legs.
Reference
Documents
FAA AC
20-138D
CHG 2
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
R
S2
FAA AC
90-105A
The aircraft complies with
the criteria of AMC 20-27
for RNP approaches to
LNAV/VNAV minima, with
the exception that VNAV
is based on SBAS/GNSS
geometric altitude when
SBAS/GNSS is available
and authorized.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
When flying a RNP
procedure with a
radius-to-fix (RF) leg,
the AFCS must be
operational. At a
minimum, the flight
director must be
displayed and utilized
when conducting
procedures
containing RF legs.
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS).” This
includes procedures with
radius-to-fix (RF) legs.
Vertical guidance is based
on GPS/SBAS when
within SBAS coverage and
on baro VNAV when
outside SBAS coverage,
when SBAS has been
disabled by pilot selection,
or for approaches with
‘WAAS VNAV NA’.
EASA AMC
20-27 with
CM-AS-002
In accordance with
AC 90-105A, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly RNP
APCH LNAV/VNAV
minima procedures.
RNP APCH
LP minima
Notes
FAA AC
20-138D
CHG 2
N/A
N/A
FAA AC
90-107
This includes area
navigation approaches
titled “RNAV (GPS)” and
“RNAV (GNSS)” including
procedures with radius-tofix (RF) legs.
LP minima are available
only when within SBAS
coverage.
In accordance with
AC 90-107, Part 91
operators (except
subpart K) following
the operational
(continued)
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
Operational
Requirements/
Authorization
Navigation
Specification
Reference
Documents
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
B
N/A
Notes
considerations and
training guidance in
AC 90-107 are
authorized to fly RNP
APCH LP minima
procedures.
Part 91 subpart K,
121, 125, 133, 135,
and 137 operators
require operational
approval.
RNP APCH
LPV minima
When flying a RNP
procedure containing
a radius-to-fix (RF)
leg, the AFCS must
be operational. At a
minimum, the flight
director must be
displayed and utilized
when conducting
procedures
containing RF
segments.
FAA AC
20-138D
CHG 2
FAA AC
90-107
EASA
AMC 20-28
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS).” This
includes procedures with
radius-to-fix (RF) legs.
LPV minima are available
only when within SBAS
coverage.
In accordance with
AC 90-107, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-107 are
authorized to fly RNP
APCH LPV minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 21 of 44
Navigation
Specification
Advanced
RNP
Operational
Requirements/
Authorization
This does not
constitute an
operational approval.
Reference
Documents
FAA AC
20-138D
CHG 2
ICAO Flight
Plan Code
Item 10a
Code
Item 18
PBN/
N/A
N/A
See Notes for
specific
Advanced
RNP
functions.
Notes

RNAV Holding:
Supported.

Radius-to-Fix (RF)
Legs:
Supported.

Parallel Offsets:
RNP-4 parallel offsets
as defined by AC 20138D Chapter 10 are
supported. However,
Advanced RNP
parallel offsets as
defined by AC 20138D Appendix 3 are
not supported.

Higher Continuity:
Supported when both
GIA GPS/SBAS
receivers are
operating and
providing GPS
navigation guidance to
their respective PFD.

Scalable RNP:
Not supported.

Fixed Radius
Transitions (FRT):
Not supported.

Time of Arrival Control
(TOAC):
Not supported.
Table 2 -G1000 NXi GNSS Operational Requirements
1. FDE/RAIM availability worldwide can be determined via the following:
An FDE prediction tool that satisfies the guidance of FAA AC 20-138D and AC 90-105A (or later revision),
such as the Garmin WFDE Prediction program, part number 006-A0154-01 (010-G1000-00) or later
approved version with Garmin GA36 and GA37 antennas selected.
Also, within the United States:
Via the FAA’s RAIM Service Availability Prediction Tool (SAPT) website: http://sapt.faa.gov.
Contacting a Flight Service Station (not DUATS) to obtain non-precision approach RAIM.
Also, within Europe:
Via Europe’s AUGER GPS RAIM Prediction Tool at http://augur.ecacnav.com/augur/app/home.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of
flight. The route planning and WFDE prediction program may be downloaded from the Garmin website
on the internet. For information on using the WFDE Prediction Program, refer to Garmin WAAS FDE
Prediction Program, part number 190-00643-01, ‘WFDE Prediction Program Instructions’.
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 (190-01999-00) can be
viewed at FlyGarmin.com.
Navigation information is referenced to the WGS-84 reference system.
G1000 NXI GNSS (GPS/SBAS) NAVIGATION SYSTEM LIMITATIONS
If the navigation database AIRAC cycle will change during flight, the pilot must ensure the accuracy of
navigation data, including suitability of navigation facilities used to define the routes and procedures for
flight. If an amended chart affecting navigation data is published for the procedure, the database must not
be used to conduct the procedure.
GPS/SBAS based IFR enroute, oceanic, and terminal navigation is prohibited unless the flight crew verifies
and uses a valid, compatible, and current Navigation database or verifies each waypoint for accuracy by
reference to current approved data.
Discrepancies that invalidate a procedure must be reported to Garmin International. The affected
procedure is prohibited from being flown using data from the Navigation database until a new Navigation
database is installed in the aircraft and verified that the discrepancy has been corrected.
For flight planning purposes:

In areas where SBAS coverage is not available, the pilot must check RAIM availability.

Operations within the U.S. National Airspace System on RNP and RNAV procedures when SBAS
signals are not available, the availability of GPS integrity RAIM must be confirmed for the intended
route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for
any part of the intended route of flight, the flight should be delayed, canceled, or re-routed on a
track where RAIM requirements can be met.

For operations within European B-RNAV and P-RNAV airspace, if more than one satellite is
scheduled to be out of service, then the availability of GPS integrity RAIM must be confirmed for
the intended flight (route and time). In the event of a predicted continuous loss of RAIM of more
than five minutes for any part of the intended flight, the flight should be delayed, canceled, or rerouted on a track where RAIM requirements can be met.

For operations where the route requires Class II navigation, the aircraft’s operator or flight crew
must use an FDE Prediction program that satisfies the guidance of AC 20-138D and AC 90-105A
(or later revision) to demonstrate that there are no outages on the specified route that would prevent
the G1000 NXi from providing primary means of Class II navigation in oceanic and remote areas
of operation that requires RNP-2 oceanic/remote, RNP-4, or RNP-10 capability. In accordance
with FAA AC 90-105A requirements, if the Garmin WFDE Prediction program indicates fault
exclusion (FDE) will be unavailable for more than 5 minutes for RNP-2 oceanic/remote, 25 minutes
for RNP-4, or 34 minutes for RNP-10, then the operation must be rescheduled when FDE is
available.
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 23 of 44
Both GIA GPS navigation receivers must be operating and providing GPS navigation guidance to their
respective PFD for operations requiring RNP-2 oceanic/remote, RNP-4, and RNP-10 performance.
NOTE
An amber “BOTH ON GPS1” or “BOTH ON GPS2” message does not necessarily
mean that one GPS has failed. Refer to the MFD – GPS STATUS page to determine
the state of the unused GPS.
Manual entry of waypoints using latitude/longitude or place/bearing is prohibited for published RNP and
RNAV routes.
“GPS”, “or GPS”, “RNAV (GPS)”, and “RNAV (GNSS)” instrument approaches using the G1000 NXi System
are prohibited unless the pilot verifies and uses the current Navigation database. GPS based instrument
approaches must be flown in accordance with an approved instrument approach procedure that is loaded
from the Navigation database.
When conducting instrument approaches referenced to true North, the NAV Angle on the Display Units
(Aux – System Status page) must be set to True (To).
Pilots planning to fly an RNAV instrument approach must ensure that the Navigation database contains the
planned RNAV Instrument Approach Procedure and that approach procedure must be loaded from the
Navigation database into the FMS flight plan by its name.
IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches within
the U.S. National Airspace System. Approaches to airports in other airspace are not approved unless
authorized by the appropriate governing authority.
It is prohibited to flight plan to an alternate airport based on minima for which SBAS is required (RNAV(GPS)
LP/LPV).
Use of the Garmin G1000 NXi GPS/SBAS receivers to provide navigation guidance during the final
approach segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved
for “or GPS” navigation is prohibited. When using the G1000 NXi VOR/LOC/GS receivers to fly the final
approach segment, VOR/LOC/GS navigation data must be selected and presented on the CDI of the pilot
flying.
Navigation information is referenced to WGS-84 reference system, and should only be used where the
Aeronautical Information Publication (including electronic data and aeronautical charts) conform to WGS84 or equivalent.
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.
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190-02450-02 Rev. 1
FAA APPROVED
The installed Garmin GTX 33D Mode-S transponder system, or the optional Garmin GTX 345R transponder
system, satisfies the data requirements of EASA document CS-ACNS (initial issue), Subpart D, Section 3
– Mode S Enhanced Surveillance. The capability of the GTX 33D and GTX 345R to transmit specific
Mode-S, Level 2 data parameters is shown in column 2 of the following table:
PARAMETER
AVAILABLE / NOT AVAILABLE
Magnetic Heading
Available
Indicated Airspeed
Available
Mach Number
Available
Vertical Rate
Available
Roll Angle
Available
Track Angle Rate
Not Available
True Track Angle
Available
Ground Speed
Available
Selected Altitude
Available
True Airspeed
Available
Barometric Pressure Setting
Available
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FAA APPROVED
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Page 25 of 44
AHRS AREAS OF OPERATION
For airplanes that have GRS 77 AHRS installed.
Flight operations are prohibited in the following regions due to unsuitability of the magnetic fields near the
Earth’s poles:
1. North of 72° North latitude at all longitudes
2. South of 70° South latitude at all longitudes
3. North of 65° North latitude between longitude 75° W and 120° W (Northern Canada)
4. North of 70° North latitude between longitude 70° W and 128° W (Northern Canada)
5. North of 70° North latitude between longitude 85° E and 114° E (Northern Russia)
6. South of 55° South latitude between longitude 120° E and 165° E (Region south of Australia and
New Zealand)
NOTE
The Garmin G1000 NXi installation in this aircraft is not designed for use as a polar
navigator. Operation outside the approved operating area is prohibited. The GRS 77
AHRS internally monitor the magnetic field and will display a GEO LIMITS system
message when the magnetic field becomes unsuitable for AHRS operation. When
the AHRS can no longer reliably compute heading, heading information will be
removed from the HSI.
TRAFFIC AVOIDANCE SYSTEM LIMITS
Use of the TRAFFIC MAP to maneuver the airplane to avoid traffic is prohibited. The TRAFFIC
INFORMATION SYSTEM (TIS) and the option GTX 345 ADS-B Traffic systems are for advisory use only.
TIS and ADS-B are intended only to help the pilot to visually locate traffic. It is the responsibility of the pilot
to see and maneuver to avoid traffic.
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FAA APPROVED
DATA LINK WEATHER (XM, CONNEXT, OR FIS-B WEATHER)
Use of the WEATHER MAP (XM Weather and FIS-B) for hazardous weather (thunderstorm) penetration is
prohibited. LTNG information on the NAVIGATION MAP or WEATHER MAP is approved only as an aid to
hazardous weather avoidance, not penetration.
KINDS OF OPERATIONS EQUIPMENT LIST
This airplane may be operated in day or night VFR, day or night IFR, and icing conditions when the required
systems and equipment are installed and operable.
The following systems are added to the operations equipment list in the original AFM:
VFR
Day
VFR
Night
IFR
Day
IFR
Night
Icing
System and/or Component
Comments
MISCELLANEOUS EQUIPMENT
FAA Approved Flight Manual
Supplement
1
1
1
1
1
Accessible to pilot in flight
Garmin G1000 NXi Cockpit
Reference Guide
1
1
1
1
1
Accessible to pilot in flight
Flight Stream 510
0
0
0
0
0
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
Section III – OPERATING PROCEDURES
TABLE OF CONTENTS
EMERGENCY PROCEDURES ................................................................................................................. 30
Taxiway Takeoff ..................................................................................................................................... 30
Taxiway Landing .................................................................................................................................... 30
Runway Too Short During Takeoff ......................................................................................................... 31
Runway Too Short During Landing ........................................................................................................ 31
ABNORMAL PROCEDURES .................................................................................................................... 32
Check Runway During Takeoff .............................................................................................................. 32
Check Runway During Landing ............................................................................................................. 32
SurfaceWatch Inhibit .............................................................................................................................. 33
SurfaceWatch Failed .............................................................................................................................. 33
No SurfaceWatch Runway Position Data .............................................................................................. 33
NORMAL PROCEDURES ......................................................................................................................... 34
QFE ........................................................................................................................................................ 34
Metric ALT/VS Units ............................................................................................................................... 35
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FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 29 of 44
EMERGENCY PROCEDURES
Some emergency situations require immediate memorized corrective action. These numbered steps are
printed in boxes within the emergency procedures and should be accomplished without the aid of the
checklist.
For airplanes equipped with SurfaceWatch:
 TAXIWAY TAKEOFF
(Red
Annunciator Is Displayed and Aural “Taxiway” Message)
1. Takeoff .................................................................................................................................. ABORT
a. Brakes ...................................................................................... MAXIMUM PILOT EFFORT
b. Throttles ........................................................................................................................ IDLE
c. Speed Brakes......................................................................................................... EXTEND
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 1 page
a. Set SurfaceWatch Alerts: ............................................................................................... OFF
NOTE
SurfaceWatch Alerts should be turned ON as soon as practical after
takeoff to restore functionality for remainder of flight.
PROCEDURE COMPLETED
 TAXIWAY LANDING
(Red
Annunciator Is Displayed and Aural “Taxiway” Message)
1. ALL ENGINES GO-AROUND 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 1 page
a. Set SurfaceWatch Alerts: ............................................................................................... OFF
NOTE
SurfaceWatch Alerts should be turned ON as soon as practical after
landing to restore functionality for ground operations.
PROCEDURE COMPLETED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
 RUNWAY TOO SHORT DURING TAKEOFF
(Red
Annunciator Is Displayed and Aural “Runway Too Short” Message)
1. Takeoff .................................................................................................................................. ABORT
a. Brakes ...................................................................................... MAXIMUM PILOT EFFORT
b. Throttles ........................................................................................................................ IDLE
c. Speed Brakes......................................................................................................... EXTEND
2. Aircraft Position and Runway Assignment ........................................................................ CONFIRM
3. Ensure correct origin, runway, and required takeoff distance have been entered into the G1000
system, on the FPL – SurfaceWatch Setup page.
PROCEDURE COMPLETED
 RUNWAY TOO SHORT DURING LANDING
(Red
Annunciator Is Displayed and Aural “Runway Too Short” Message)
1. ALL ENGINES GO-AROUND 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, on the FPL – SurfaceWatch Setup page.
PROCEDURE COMPLETED
190-02450-02 Rev. 1
FAA APPROVED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
Page 31 of 44
ABNORMAL PROCEDURES
For airplanes equipped with SurfaceWatch:
 CHECK RUNWAY DURING TAKEOFF
(Amber
annunciator displayed on PFD and aural “CHECK RUNWAY”)
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. The alert will be issued when N2 is above 85% and the
groundspeed is greater than 40 knots.
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.
4.
5.
6.
Brakes............................................................................................. MAXIMUM PILOT EFFORT
Throttles ............................................................................................................................... IDLE
Speed Brakes ............................................................................................................... EXTEND
Enter correct origin, runway, and required takeoff distance into the G1000 NXi system on the
FPL – SurfaceWatch Setup page on the MFD.
PROCEDURE COMPLETED
 CHECK RUNWAY DURING LANDING
(Amber
annunciator displayed on PFD and aural “CHECK RUNWAY”)
This caution alert is issued when the aircraft is landing on a runway different than that entered on the MFD
FPL – SurfaceWatch Setup page. The alert will be issued when the aircraft is below 250’ (76 m) AGL and
within one nautical mile of the airport.
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. ALL ENGINES GO-AROUND Procedure ......................................................................... EXECUTE
4. Enter correct destination, runway, and required landing distance into the G1000 NXi system, on
the FPL – SurfaceWatch Setup page on the MFD.
PROCEDURE COMPLETED
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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190-02450-02 Rev. 1
FAA APPROVED
 SURFACEWATCH INHIBIT
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 1 Page ............................................................................................ VIEW
2. SurfaceWatch Alerts ................................................................................................................... OFF
PROCEDURE COMPLETED
NOTE
After inhibiting SurfaceWatch, the following will post as an alert on both PFDs in
the Alerts window:
“SURFACEWATCH INHIBITED SurfaceWatch Inhibited.”
SurfaceWatch Alerts will remain inhibited until manually un-inhibited by the crew,
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.
 SURFACEWATCH FAILED
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 both PFDs 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 both PFDs in the
alerts window:
“NO RUNWAY POSITION DATA Inhibit SurfaceWatch. No runway position data.”
SurfaceWatch should then be inhibited according to the SURFACEWATCH INHIBIT procedure 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 un-inhibited as
soon as practical so that functionality will be restored for the remainder of the flight.
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FAA APPROVED
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Page 33 of 44
NORMAL PROCEDURES
QFE
ON GROUND, IF QFE OPERATIONS ARE REQUIRED
1.
BARO setting ................................................... SET to appropriate QFE BARO setting (both PFDs)
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 ........................................................................................................................ ON
This will make QFE mode active, as indicated by black QFE text on green box in upper right corner
of both PFD attitude displays.
TO DISABLE QFE MODE:
6.
BARO setting ................................................... SET STD BARO (both PFDs), then SET as desired
Changing the baro setting on both PFDs to STD BARO will automatically disable QFE mode,
removing any QFE indications.
IN FLIGHT, BEFORE QFE OPERATIONS ARE REQUIRED:
1.
BARO setting ...................................................................................... SET STD BARO (both PFDs)
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 ........................................................................................................................ ON
If STD BARO is set on both PFDs, this step will Arm QFE mode, as indicated by black QFE text in
a white box in the upper right corner of both PFD attitude displays.
TO ACTIVATE QFE MODE:
6.
BARO setting ................................................... SET to appropriate QFE BARO setting (both PFDs)
Changing the baro setting on both PFDs to a numerical value (not STD BARO) will automatically
activate QFE mode, as indicated by black QFE text in a green box in the upper right corner of both
PFD attitude displays.
TO DISABLE QFE MODE:
7.
BARO setting ................................................... SET STD BARO (both PFDs), then SET as desired
Changing the baro setting on both PFDs to STD BARO will automatically disable QFE mode,
removing any QFE indications.
NOTE
Changing the BARO setting with the autopilot engaged in ALT mode will result in
the aircraft slowly climbing or descending to return to the original indicated altitude.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
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FAA APPROVED
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.
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 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 Feet(FT,FPM)
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FAA APPROVED
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190-02450-02 Rev. 1
FAA APPROVED
Section IV – PERFORMANCE
No Change. Refer to basic Aircraft Flight Manual or appropriate supplement.
190-02450-02 Rev. 1
FAA APPROVED
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190-02450-02 Rev. 1
FAA APPROVED
Section V – SUPPLEMENTS
This section is not applicable to this AFMS.
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FAA APPROVED
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190-02450-02 Rev. 1
FAA APPROVED
Section VI – WEIGHT AND BALANCE
No Change. Refer to basic Aircraft Flight Manual or appropriate supplement.
190-02450-02 Rev. 1
FAA APPROVED
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FAA APPROVED
Section VII – ADVISORY INFORMATION
No Change. Refer to basic Aircraft Flight Manual or appropriate supplement.
190-02450-02 Rev. 1
FAA APPROVED
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