Garmin G5000 Airplane Flight Manual Supplement page 18

Model 560XL
• 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.
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.
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.
(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
Textron Aviation Citation 560XL
1-12
LOA status and RTCA/DO-200A List of Applicable Avionics
Section I - General
Additional
190-02313-03 Rev. 8