Garmin G5000 Technische Daten

Textron Aviation Citation 560XL 190-02313-03 Rev. 8

GARMIN Ltd. or its subsidiaries

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. 151st Street

Olathe, KS 66062 USA

Telephone: 913-397-8200

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

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

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

This page intentionally left blank.

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

ersion

Pilot’s Guide

Part Numbe

Cockpit Reference Guide

Part Numbe

3343.02 or later 190-02537-02

Revision

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

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

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

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

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.

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