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displayed. Refer to the Abnormal Procedures for these messages as time
allows.
PROCEDURE COMPLETED
• IF MFD
1. Either DISPLAY BACKUP Button . . . . PRESS (EICAS info will be displayed on PFDs)
PROCEDURE COMPLETED
510FM-07 AA 3-99
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
DUAL GPS FAILURE (AMBER “DR" OR “LOI" ON HSI)
When both GPS receivers are inoperative, the G1000 system will enter one of two modes: Dead
Reckoning mode (DR) or Loss Of Integrity mode (LOI). The mode is indicated on the HSI by an
amber “DR" or “LOI". Which mode is active depends on the distance from the destination airport
in the active flight plan.
• IF ALTERNATE NAVIGATION SOURCES (ILS, LOC, VOR, DME, ADF)
ARE AVAILABLE
1. Navigation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE ALTERNATE SOURCES
PROCEDURE COMPLETED
• IF NO ALTERNATE NAVIGATION SOURCES ARE AVAILABLE
DEAD RECKONING (DR) MODE - ACTIVE WHEN THE AIRPLANE
IS GREATER THAN 30 NM FROM THE DESTINATION AIRPORT
1. Navigation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Use the airplane symbol and
magenta course line on the map display
WARNING
• All information normally derived from GPS turns amber. All of this
information will become more inaccurate over time.
• TAWS is inoperative.
NOTE
• DR mode uses heading, airspeed, and the last known GPS position to estimate
the airplane’s current position.
• All maps with an airplane symbol show a ghosted airplane and a “DR" label.
• Traffic Information System (TIS) is not dependent on GPS information. The
position of displayed traffic relative to the airplane symbol on the map is still
accurate.
LOSS OF INTEGRITY (LOI) MODE - ACTIVE WHEN THE
AIRPLANE IS WITHIN 30NM OF THE DESTINATION AIRPORT (AS
CALCULATED FROM THE PREVIOUS GPS OR DR POSITION)
1. Navigation - Fly towards known visual conditions or available terminal navigation
sources. Use ATC or other information sources as possible.
NOTE
• All information derived from GPS or DR is removed from the displays.
• The airplane symbol is removed from all maps. The map will remain centered at
the last known position. “NO GPS POSITION" is shown in the center of the map.
• TAWS and TIS are inoperative.
PROCEDURE COMPLETED.
3-100 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
AUDIO PANEL FAILURE
Audio panel failure may be indicated by a GMA 1/2 FAIL Garmin System Message or the inability
to communicate using the affected audio panel. This failure may also be accompanied by the
loss of some aural warnings such as Altitude Alert, Autopilot Disconnect, TAWS, and Traffic
alerts.
1. AUDIO1 or AUDIO2 Circuit Breaker (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
2. SPKR Button (operating audio panel). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. COM Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE ON-SIDE RADIO for communication
(Pilot-COM1, Copilot-COM2)
NOTE
• In the event of an audio panel failure, a fail-safe circuit connects the affected side
headset directly to the on-side com radio. The speaker on the affected side will be
inoperative.
• The operating audio panel will not be able to listen to COM or NAV audio from the
side with the inoperative audio panel.
PROCEDURE COMPLETED
LOSS OF RADIO TUNING FUNCTIONS
1. COM Frequency Toggle Button (affected PFD) . . . PRESS AND HOLD FOR 2 SECONDS
NOTE
This procedure will tune the active COM field to the emergency frequency 121.5.
Certain failures of the tuning system will automatically tune 121.5 without pilot action.
PROCEDURE COMPLETED
TRANSPONDER FAILURE
Transponder failure may be indicated by a red “X" across the transponder display or failure of the
transponder to accept codes or mode changes from the PFD.
1. TRANSPONDER . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT OPPOSITE TRANSPONDER
a. PFD XPDR Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
b. XPDR1 or XPDR2 Softkey . . . . . . . . . . . . . . . PRESS to select opposite transponder
2. XPDR1 or XPDR2 Circuit Breaker (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
PROCEDURE COMPLETED
510FM-07 AA 3-101
SECTION III - OPERATING PROCEDURES MODEL 510
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Citation Mustang airplane flight manual 1(73)
