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by a green circle on the pilot and copilot airspeed indicators.
The low speed awareness system may be used as a reference, but does not replace the airspeed
display in the Primary Flight Display (PFD) as a primary instrument.
2-28 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 version 0435.13 or 0435.14, 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:
(1) Takeoff and Climb ............................................................................700 feet AGL
(2) Enroute and Descent .....................................................................1000 feet AGL
(3) Approach (GP or GS Mode).............................................................200 feet AGL
(4) 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 pilot’s 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 AJ 2-29
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
GARMIN G1000 GPS NAVIGATION SYSTEM
OPERATIONAL APPROVALS
The Garmin G1000 GPS receivers are approved under TSO C145a Class 3. The Garmin G1000
system has been demonstrated capable of, and has been shown to meet the accuracy requirements
for, the following operations provided it is receiving usable navigation data. These do not constitute
operational approvals.
1. Enroute, terminal, non-precision instrument approach operations using GPS and WAAS
(including "GPS", or GPS", and "RNAV" approaches), and approach procedures with
vertical guidance (including "LNAV/VNAV", "LNAV + V", and "LPV") within the U.S. National
Airspace System in accordance with AC 20-138A.
2. As a required Long Range Navigation (LRN) system for use in the following types of
airspace when used in conjunction with Garmin WAAS Fault Detection/Exclusion Prediction
Program, part number 006-A0154-01 or later approved version:
a. Oceanic/Remote - RNP-10 (per FAA AC 20-138A, FAA Notice 8110-60, FAA Order
8400-12A, and FAA Order 8700-1). Both GPS receivers are required to be operating
and receiving usable signals except for routes requiring only one Long Range
Navigation (LRN) sensor.
NOTE
Each display computes an independent navigation solution based on the on-side
　
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