Model 560XL Section II – Limitations
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 2-15
the Navigation database into the FMS flight plan by its name.
IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches
within the U.S. National Airspace System. Approaches to airports in other airspace are not approved
unless authorized by the appropriate governing authority.
It is prohibited to flight plan to an alternate airport based on minima for which SBAS is required
(RNAV(GPS) LP/LPV).
Use of the Garmin G5000 GPS/SBAS receivers to provide navigation guidance during the final approach
segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for “or
GPS” navigation is prohibited. When using the G5000 VOR/LOC/GS receivers to fly the final approach
segment, VOR/LOC/GS navigation data must be selected and presented on the HSI of the pilot flying.
Navigation information is referenced to WGS-84 reference system and should only be used where the
Aeronautical Information Publication (including electronic data and aeronautical charts) conform to
WGS-84 or equivalent.
Autopilot Operation Limits
Approved for Category I ILS approaches only.
Autopilot and yaw damper must be disengaged during takeoff and landing.
Do not manually override the autopilot in flight.
No intentional stalls permitted above 25,000 FT (FL250).
WARNING
THE OPTIONAL UNDERSPEED PROTECTION SYSTEM RELIES ON STICK
SHAKER ACTIVATION, AND MAY NOT ACTIVATE AT SUFFICIENT AIRSPEED
TO PREVENT AERODYNAMIC STALL WHEN ABOVE 18,000 FT.
One pilot must remain seated with the seatbelt fastened during all autopilot operations.
Autopilot preflight check (located in the Normal Procedures – Cockpit Preparation section of this AFMS)
must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.
The AFCS automatic preflight test must complete successfully prior to use of the autopilot, yaw damper,
or flight director (failure will be indicated by a white AP FAIL or AP-YD FAIL CAS message, or lack of the
aural disconnect alert at preflight test completion).
Do not use autopilot below the following altitudes:
Climb ............................................................................................................................. 500 feet AGL
Enroute and Descent .................................................................................................. 1000 feet AGL
Non-precision Approach ................................................................................................ 200 feet AGL
Precision Approach (ILS, LPV) ..................................................................................... 120 feet AGL
Steep Approach (GP or GS Mode) ............................................................................... 300 feet AGL
Autopilot coupled ILS approaches with flight path angles greater than 4.5 degrees are prohibited if the
G5000 system has not acquired a valid GPS position.
Synthetic Vision Limits
Use of the Synthetic Vision system display elements alone for aircraft control without reference to the
G5000 primary flight instruments or the aircraft standby instruments is prohibited.
Use of the Synthetic Vision system alone for navigation, obstacle, or terrain avoidance is prohibited.
Use of the Synthetic Vision system traffic display alone to avoid other aircraft is prohibited.
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