Garmin G5000 Technical specifications

Textron Aviation Citation 560XL 190-02313-03 Rev. 8
ii
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All Rights Reserved
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GARMIN International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: [phone]
www.garmin.com

190-02313-03 Rev. 8 Textron Aviation Citation 560XL
iii
GARMIN International, Inc
FAA Approved Airplane Flight Manual Supplement for
G5000 Integrated Flight Deck
Textron Aviation Citation Model 560XL
Log Of Revisions
REV
NO.
PAGE
NO(S) DESCRIPTION DATE OF APPROVAL
FAA APPROVED
1 ALL Original Issue 06/07/2019 Robert G. Murray
2 Various
Changes for CPDLC
including removal of
CPDLC limitation, minor
clerical changes
06/19/2019 Robert G. Murray
3 Various
Added temperature
limitation for cold weather
operations. Updated
circuit breaker reset
procedures. Minor clerical
changes.
02/20/2020 Robert G. Murray
4 Various
Addition of TOLD,
Stabilized Approach,
Steep Approach,
Windshear
07/28/2020 Robert G. Murray
5 Various
Addition of FANS 1/A+,
ACARS, and rotary test
information.
03/02/2021 Robert G. Murray
6 2-17
Addition of TOLD
limitation 07/14/2021 Paul Mast
7 2-17
Addition of new TOLD
databases 10/27/2021 Robert G. Murray
8 Various
Addition of Scalable CDI
support for A-RNP
approaches. Addition of
secondary aural cue
description.
See Cover See Cover

Textron Aviation Citation 560XL 190-02313-03 Rev. 8
iv
Revision 8 – Change Summary
Section Page Description of Change
Section I -- General 1-11 Addition of manually scalable CDI support for A-RNP
approaches.
Appendix A – Systems
Description
A-20 Addition of CAS secondary aural cue description.

190-02313-03 Rev. 8 Textron Aviation Citation 560XL
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Table of Contents
Section I – General ....................................................................................................................................1-1
Section II – Limitations ...............................................................................................................................2-1
Section III – Operating Procedures............................................................................................................3-1
Section IV – Performance ..........................................................................................................................4-1
Section VI – Weight and Balance ..............................................................................................................6-1
Appendix A – Systems Description............................................................................................................A-1

Textron Aviation Citation 560XL 190-02313-03 Rev. 8
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Model 560XL Section I - General
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
1-1
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 G5000
Integrated Flight Deck including Digital Automatic Flight Guidance System in accordance with GARMIN
International, Inc. approved data, STC ST01918WI.
FAA approved sections of this supplement are labeled as “FAA APPROVED”. Sections not labeled “FAA
APPROVED” are provided for guidance information only.
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 this supplement for possible superseding information and
placarding applicable to operation of the airplane.
The GARMIN G5000 system installed in the Textron Aviation Citation 560XL provides a fully integrated
Display, Communications, Navigation and Flight Control system. Functions provided by the G5000
system include: Primary Flight Instrumentation, Powerplant Instrumentation, Navigation, Communication,
Traffic Surveillance, TAWS-A, Weather Avoidance, and a three-axis automatic flight control / flight director
system.
Use of this supplement requires the installation of the GARMIN G5000 hardware and system software
version 3343.02 or later in the aircraft. Pilots are advised to carefully review the contents of this manual
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
V
ersion
Pilot’s Guide
Part Numbe
r
Cockpit Reference Guide
Part Numbe
r
3343.02 or later 190-02537-02
Revision
A
or later
190-02538-02
Revision A or later
Table 1-1, Applicable Pilot's Guide and Cockpit Reference Guide
Use of This AFMS
The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the AFMS:
WARNING
Operating procedures or techniques that may result in personal injury or loss of life if not
carefully followed.
CAUTION
Operating procedures or techniques that may result in damage to equipment if not carefully
followed.
NOTE
Supplemental information or highlights considered of sufficient significance to require
emphasizing.

Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
1-2
G5000 GNSS (GPS/SBAS) Navigation System Equipment Approvals
The Garmin G5000 Integrated Avionics GNSS navigation system installed in this aircraft is a GPS system
with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145c Class 3 approved
Garmin GIA 64Es, two TSO-C146c Class 3 approved Garmin GTC 575 Touchscreen Control Units,
Garmin GA36 and GA37 antennas, and GPS software version 7.0 or later approved version. The G5000
GNSS navigation system in this aircraft is installed in accordance with AC 20-138D. When all the
equipment is operative, the Garmin G5000 system has two independent GNSS long-range navigation
systems. Failure of any of the above equipment indicates only one operational GNSS system.
The Garmin G5000 Integrated Avionics GNSS navigation system as installed in this aircraft 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 enroute,
terminal area, non-precision approach, and approach procedures with vertical guidance operations.
The Garmin G5000 Integrated Avionics GNSS navigation system as installed in this airplane complies
with the equipment, performance, and functional requirements to conduct RNAV and RNP operations in
accordance with 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.
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code Notes
Item 10a
Code
Item 18
PBN/
RNAV 10
RNP 10
Oceanic and
Remote
Areas of
Operation
(Class II
Navigation).
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is
34 minutes.1
Two GNSS systems
required to be
operational, (one
GNSS system for
those routes requiring
only one long range
navigation system).
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
FAA AC
91-70A,
EASA AMC
20-12
R A1 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
long-range navigation
systems, when used in
conjunction with an FDE
prediction tool that satisfies
the guidance of FAA AC
20-138D and AC 90-105A
(or later revision).1

Model 560XL Section I - General
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
1-3
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code Notes
Item 10a
Code
Item 18
PBN/
B-RNAV /
RNAV 5
(Europe)
This does not
constitute an
operational approval.
FAA AC
90-96A
CHG 1,
EASA AMC
20-4A
R B2
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
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).
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
FAA AC
91-70A
R L1 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
long-range navigation
systems, when used in
conjunction with an FDE
prediction tool that satisfies
the guidance of FAA AC
20-138D and AC 90-105A
(or later revision).1
Additional equipment may
be required to obtain
operational approval to
utilize RNP-4 performance.
RNAV 2 The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
In accordance with
AC 90-100A, CHG 2,
Part 91 operators
(except subpart K)
(
continued
)
FAA AC
20-138D
CHG 2,
FAA AC
90-100A
CHG 2
R C2 Includes RNAV Q and T
routes.

Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
1-4
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code Notes
Item 10a
Code
Item 18
PBN/
(continued)
following the aircraft
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.