Garmin G5000 Airplane Flight Manual Supplement page 8

Model 560XL
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.
Operational
Navigation
Requirements/
Specification
Authorization
RNAV 10 GNSS FDE
availability must be
RNP 10 verified prior to flight.
Maximum predicted
Oceanic and FDE unavailability is
Remote 34 minutes.
Areas of
Two GNSS systems
Operation
required to be
(Class II
operational, (one
Navigation).
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.
Textron Aviation Citation 560XL
1-2
Reference
Documents
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
1
FAA AC
91-70A,
EASA AMC
20-12
ICAO Flight
Plan Code
Item 10a Item 18
Code PBN/
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).
Section I - General
Notes
1
190-02313-03 Rev. 8