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GPS sensor. However, either display will automatically revert to the cross-side sensor
if the on-side sensor fails or if the cross-side sensor is determined to be more
accurate. A BOTH ON GPS1 or BOTH ON GPS2 message does not necessarily
mean that one GPS has failed. Refer to the MFD AUX-GPS STATUS page to
determine the status of the unused GPS.
b. North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS)
Airspace per AC 91-49 and AC 120-33. Both GPS receivers are required to be
operating and receiving usable signals except for routes requiring only one Long
Range Navigation sensor.
c. Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) - In accordance
with JAA TGL-10, ACJ 20X4, AC 90-96A, and AC 90-100A, provided the FMS is
receiving usable navigation information from one or more GPS receivers.
LIMITATIONS
1. GPS-based IFR enroute, oceanic, and terminal navigation is prohibited unless the pilot
verifies the currency of the database or verifies each selected waypoint for accuracy by
reference to current approved data.
2. RNAV/GPS instrument approaches must be accomplished in accordance with approved
instrument approach procedures that are retrieved from the G1000 navigation database.
The G1000 database must incorporate the current update cycle.
NOTE
Not all published approaches are in the navigation database. The flight crew must
make sure that the planned approach is in the database.
(Continued Next Page)
2-30 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
GARMIN G1000 AVIONICS SYSTEM
1. The Garmin G1000 Cockpit Reference Guide for the Cessna Citation MUSTANG,
190-00600-01, Rev B, dated April 2007, or later applicable revision, must be immediately
available to the flight crew.
2. These limitations apply to Garmin system software versions 0435.09 or 0435.10, which
include GPS software version 2.4, and GPS Antenna Model’s GA36/37 or GA56A/57.
3. Category II approaches are prohibited.
4. Dispatch is prohibited following a flight where either a PFD/MFD COOLING or GIA 1-2
COOLING Garmin System Message was displayed, until the condition is identified and
corrected.
5. Dispatch is prohibited with a PFD/MFD SERVICE, GIA 1-2 SERVICE, or GMA 1-2
SERVICE Garmin System Message displayed, until the condition is identified and
corrected.
6. All display units must be installed and operational.
7. Dispatch with a display in reversionary mode is prohibited.
8. Autopilot:
a. One pilot must remain seated, with the seatbelt fastened, during all autopilot
operations.
b. Autopilot operation is prohibited if either PFD is in AHRS reversion.
c. Autopilot Minimum-Use-Height:
(5) Takeoff and Climb ............................................................................700 feet AGL
(6) Enroute and Descent .....................................................................1000 feet AGL
(7) Approach (GP or GS Mode).............................................................200 feet AGL
(8) Approach (FLC, VS, PIT or ALT Mode)............................ Higher of 400 feet AGL
or Approach MDA
9. Use of VNAV is prohibited during an approach with a teardrop course reversal. VNAV will
fail at the beginning of the teardrop.
10. Use of the NAVIGATION MAP page for pilotage navigation is prohibited unless required by
AFM procedure. The NAVIGATION MAP is intended only to enhance situational awareness.
Navigation is to be conducted using only current charts, data, and authorized navigation
facilities.
11. Use of the TRAFFIC MAP to maneuver the airplane to avoid traffic is prohibited. The
TRAFFIC INFORMATION SYSTEM (TIS) is intended for advisory use only. TIS is intended
only to help the pilot to visually locate traffic. It is the responsibility of the pilot to see and
maneuver to avoid traffic.
12. Use of the TERRAIN information for primary terrain avoidance is prohibited. The TERRAIN
information is intended only to enhance situational awareness. It is the pilots responsibility
to provide terrain clearance at all times.
13. Use of the WEATHER MAP (XM Weather) for hazardous weather (thunderstorm)
penetration is prohibited. LTNG information on the NAVIGATION MAP or WEATHER MAP
is approved only as an aid to hazardous weather avoidance, not penetration.
14. The fuel quantity, fuel required, fuel remaining, and gross weight estimate functions of the
G1000 are supplemental information only and must be verified by the flight crew.
510FM-07 AK 2-29.1
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
GARMIN G1000 GPS NAVIGATION SYSTEM
OPERATIONAL APPROVALS
　
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