Garmin G5000 - Cessna Citation 560XL/XLS Owner's manual

Type
Owner's manual
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
ii FAA Approved
© Copyright 2020
GARMIN Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express prior
written consent of GARMIN. GARMIN hereby grants permission to download a single copy of this manual
and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and
to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of
this manual or revision must contain the complete text of this copyright notice and provided further that
any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
GARMIN International, Inc.
1200 E. 151
st
Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 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
See Cover
See Cover
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
iv FAA Approved
This page intentionally left blank.
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved v
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. 4
vi FAA Approved
This page intentionally left blank.
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 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.
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 3343.01 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
Version
Pilot’s Guide
Part Number
3343.01 or later
190-02537-01
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. 4
1-2 FAA Approved
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. 4 Textron Aviation Citation 560XL
FAA Approved 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. 4
1-4 FAA Approved
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.
RNAV 1
The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
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.
FAA AC
20-138D
CHG 2,
FAA AC
90-100A
CHG 2
R
D2
Includes RNAV terminal
departure and arrival
procedures.
P-RNAV
(Europe)
This does not
constitute an
operational approval.
FAA AC
90-96A
CHG 1,
JAA TGL
10 Rev 1
R
D2
ICAO flight plan code for
P-RNAV no longer exists.
P-RNAV utilizes RNAV 1
flight plan codes.
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 1-5
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP 1
When flying an RNP
procedure containing
an RF leg, the AFCS
must be operational.
At a minimum, the
flight director must be
displayed and utilized
when conducting
procedures containing
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 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A
R
O2
Includes RNP terminal
departure and arrival
procedures, including
procedures with
radius-to-fix (RF) legs.
Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
1-6 FAA Approved
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP-2
(Oceanic /
Remote)
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is 5
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
CHG2,
FAA AC
90-105A
R
TBD
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote navigation 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-2 performance.
Item 18 PBN flight plan
code is still
to-be-determined at time of
publication of this AFMS.
RNP-2
(Domestic /
Offshore
Enroute)
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.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A
R
TBD
Includes RNP-2 domestic
and offshore routes.
Item 18 PBN flight plan
code is still
to-be-determined at time of
publication of this AFMS.
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 1-7
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP APCH
LNAV minima
When flying an 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.
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.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
EASA AMC
20-27
R
S1
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.
Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
1-8 FAA Approved
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP APCH
LNAV/VNAV
minima
When flying an 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.
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.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
EASA AMC
20-27 with
CM-AS-002
R
S2
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’.
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.
RNP APCH
LP minima
When flying an 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
In accordance with
AC 90-107, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-107 are
(continued)
FAA AC
20-138D
CHG 2,
FAA AC
90-107
N/A
N/A
Includes area navigation
approaches titled
“RNAV (GPS)” and
RNAV (GNSS)” including
procedures with
radius-to-fix (RF) legs.
LP minima are available
only when within SBAS
coverage.
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 1-9
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
(continued)
authorized to fly RNP
APCH LP minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNP APCH
LPV minima
When flying an 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.
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.
FAA AC
20-138D
CHG 2,
FAA AC
90-107,
EASA
AMC 20-28
B
N/A
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS)”, including
procedures with
radius-to-fix (RF) legs.
LPV minima are available
only when within SBAS
coverage.
Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
1-10 FAA Approved
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
Advanced
RNP
See Notes for
specific
Advanced
RNP
functions.
This does not
constitute an
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A
N/A
N/A
RNAV Holding:
Supported.
RF Legs:
Supported.
Parallel Offsets: RNP-4
parallel offsets as
defined by AC 20-138D
Chapter 10 are
supported.
Advanced RNP parallel
offsets as defined by
AC20-138D Appendix 3
are supported.
Higher Continuity:
Supported when both
GIA 64E GPS/SBAS
receivers are operating
and providing GPS
navigation guidance to
their respective PFD.
Scalable RNP:
Not supported.
Fixed Radius
Transitions (FRT):
Supported
Time of Arrival Control
(TOAC):
Not supported.
_________________________________
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 or
later approved version with GPS SW >= 3.0 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.
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 1-11
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
Fly-Garmin website on the internet (fly.garmin.com/fly-garmin/support/). 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 AC 20-153A for
database integrity, quality, and database management practices for the Navigation database. Flight
crews and operators can view the LOA status at FlyGarmin.com then select “Aviation Database
Declarations”.
Navigation information is referenced to the WGS-84 reference system.
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.
The own-ship aircraft position displayed on any G5000 electronic charts should not be used as the
primary source of navigation.
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 G5000 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 Minimum (RVSM)
This aircraft has been determined to be capable of meeting the Reduced Vertical Separation Minimum
(RVSM) performance requirements of 14 CFR part 91 appendix G, when required equipment is
maintained in accordance with the Garmin G5000 System Maintenance Manual for the Textron Aviation
Citation 560XL.
This does not constitute operational approval. Operational approval must be obtained in accordance with
applicable operating rules.
Transponder
The ADS-B Out system has been shown to meet the equipment requirements of 14 CFR 91.227.
Airplanes Certified For Steep Approach
The G5000 Integrated Flight Deck autopilot installed in the Textron Aviation Citation 560XL has been
demonstrated to be capable of conducting coupled approaches up to glideslope angles of 5.5°. More
information is included in the Limitations and Normal Procedures sections of this AFMS.
For limitations, procedures, and performance information not contained in the G5000 Integrated Flight
Deck AFMS, see the Textron AFMS “Airplanes Certified For Steep Approaches” and the basic airplane
flight manual.
Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
1-12 FAA Approved
ATC Data Link System (CPDLC) (Optional)
The FAA has approved the optional aircraft data link system meeting the criteria in AC 20-140C for the
following datalink capabilities:
Interoperability Designators
FANS 1/A CPDLC (with automation)
ATN B1
Subnetworks
VDL M2
Aircraft-Allocated Performance
CPDLC: RCP 130
This design approval does not constitute operational authorization. Note, the system does not support
full FANS 1/A + capabilities since it does not include ADS-C capabilities.
When filing ICAO flight plans, use the table below to determine what equipment codes should be filed in
reference to the installed data link system.
Optionally Installed Capability (Enablements)
Flight Plan Filing
FAA Data Comm only
Field 10a: J4Z
Field 18: DAT/1FANSE
FAA Data Comm AND Link2000+
Field 10a: J1J4Z
Field 18: DAT/1FANSE
Link2000+ only
Field 10a: J1
To determine what ATC data link options have been enabled on the aircraft:
On either GTC homepage, the presence of a button labeled “ATC Datalink” indicates that an ATC data
link option has been enabled. To determine which option is enabled, on the GTC select Utilities
Setup Avionics Status select the Data Link tab. The presence of a “Router” button on this page
indicates that Link2000+ is enabled. The presence of an “ACARS” button on this page indicates that
FAA Data Comm is enabled.
Abbreviations and Terminology
The following glossary is applicable within the airplane flight manual supplement:
AC Advisory Circular or Alternating Current
ADC Air Data Computer
ADF Automatic Direction Finder
ADS-C Automatic Dependent Surveillance -
Contract
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 7200 AFCS
Mode Controller
ALTS AFCS altitude capture using the altitude
in the altitude preselect window
ALTV AFCS altitude capture using the altitude
from the VNAV profile vertical constraint
AMMD Airport Moving Map Display
AP Autopilot
APR Approach
APPR Approach mode, or APPR button of
GMC 7200 AFCS mode controller
Model 560XL Section I - General
190-02313-03 Rev. 4 Textron Aviation Citation 560XL
FAA Approved 1-13
APV Approach with Vertical Guidance
ATC Air Traffic Control
ATN Aeronautical Telecommunication
Network
AUX Auxiliary
BANK Low-bank mode of the AFCS
BARO Barometric Setting
BC Back Course
BRNAV Basic Area Navigation
CDI Course Deviation Indicator
CFR Code of Federal Regulations
COM Communication radio
CPDLC Controller Pilot Datalink
Communications
CRS Course
CWS Control Wheel Steering
DC Direct Current
DME Distance Measuring Equipment
DN Down
DR Dead Reckoning
EFB Electronic Flight Bag
EIS Engine Indication System
FAF Final Approach Fix
FANS Future Air Navigation System
FD Flight Director
FDE Fault Detection and Exclusion
FLC AFCS Flight Level Change mode, or
FLC button on the GMC 7200 AFCS
mode controller
FMS Flight Management System
FPM Flight Path Marker or Feet Per Minute
FT Feet
FT/MIN Feet/Minute
GA Go-around
GCU Garmin Control Unit
GDC Garmin Air Data Computer
GDL Garmin Data Link Radio
GEA Garmin Engine/Airframe Unit
GEN Generator
GEO Geographic
GIA Garmin Integrated Avionics Unit
GMA Garmin Audio Processor System
GMC Garmin Mode Control Unit
GP GPS Glide Path
GPS Global Positioning System
GPWS Ground Proximity Warning System
GRS Garmin Reference System (AHRS)
GS Glide Slope
GTC Garmin Touchscreen Controller
HDG AFCS heading mode or the HDG button
on the GMC 7200 AFCS Mode
Controller
HSI Horizontal Situation Indicator
IAF Initial Approach Fix
IAS Indicated Airspeed
ICAO International Civil Aviation Organization
IFR Instrument Flight Rules
ILS Instrument Landing System
INH Inhibit
ITT Inter-Turbine Temperature
KIAS Knots Indicated Air Speed
LCD Liquid Crystal Display
LDA Localizer Type Directional Aid
LNAV Lateral Navigation
LNAV + V Lateral Navigation with Advisory Vertical
Guidance
LNAV/VNAV Lateral Navigation / Vertical Navigation
LOC Localizer
LOI Loss of Integrity (GPS)
LPV Localizer Performance with Vertical
Guidance
LRU Line Replaceable Unit
M Mach
MAN Manual thrust mode of the Target N
1
Computer. Manual speed select mode
of FLC
MAP Missed Approach Point
MAXSPD Maximum Speed, AFCS Overspeed
Protection mode
MCT Maximum Continuous Thrust
MCR Maximum Cruise Thrust
MDA Barometric minimum descent altitude
MFD Multi Function Display
Model 560XL Section I - General
Textron Aviation Citation 560XL 190-02313-03 Rev. 4
1-14 FAA Approved
MLS Microwave Landing System
MSL Mean Sea Level
NAV Navigation, or AFCS navigation mode,
or NAV button on the GMC 7200 AFCS
Mode Controller
NEXRAD Next Generation Radar (XM Weather
Product)
NM Nautical Mile
NPA Non-precision Approaches
OAT Outside Air Temperature
OBS Omni Bearing Selector
OVR Override
P/N Part Number
PDA Premature Descent Alert
PFD Primary Flight Display
PFT Pre-Flight Test
PIT AFCS pitch mode
PRNAV Precision Area Navigation
PROC Procedure button on the GDUs or GCU
475
PSI Pounds per Square Inch
PWR Power
RA Resolution Advisory (TCAS II)
RAIM Receiver Autonomous Integrity
Monitoring
RAT Ram Air Temperature
RCP Required Communication Performance
RNAV Area Navigation
RNP Required Navigation Performance
ROL AFCS roll mode
RPM Revolutions per Minute
RVSM Reduced Vertical Separation Minimums
SBAS Satellite Based Augmentation System
SDF Simplified Directional Facility
SPD Speed knob on the GMC 7200 AFCS
Mode Controller. Adjusts the manual
airspeed reference. Pushing toggles the
FLC airspeed reference between Mach
and IAS references.
STBY Standby
STC Supplemental Type Certificate
SUSP Suspend
SVT Synthetic Vision Technology
TAWS Terrain Awareness and Warning System
TEMP Temperature
TO Takeoff
TOLD Takeoff and Landing Data
TSO Technical Standard Order
USP Underspeed Protection
VAPP AFCS VOR Approach Mode
Vdc Volts DC
VDL VHF Datalink
VFR Visual Flight Rules
VHF Very High Frequency
VNAV Vertical Navigation, or Vertical
Navigation button on the GMC 7200
AFCS Mode Controller
VOR VHF Omni-directional Range
VS Vertical Speed
WAAS Wide Area Augmentation System
WFDE WAAS Fault Detection and Exclusion
WGS-84 World Geodetic System 1984
XM XM satellite system
YD Yaw Damper
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Garmin G5000 - Cessna Citation 560XL/XLS Owner's manual

Type
Owner's manual

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