Garmin G1000 Manual

							190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 627
APPENDIX A
GRS 77 MESSAGE ADVISORIES  (CONT.)
MessageComments
AHRS2 GPS – AHRS2 not receiving 
any GPS information.
The #2 AHRS is not receiving any or any useful GPS information.  Check AFMS 
limitations.  The G1000 system should be serviced.
AHRS1 GPS – AHRS1 not receiving 
backup GPS information.
The #1 AHRS is not receiving backup GPS information.  The G1000 system should be 
serviced.
AHRS2 GPS – AHRS2 not receiving 
backup GPS information.
The #2 AHRS is not receiving backup GPS information.  The G1000 system should be 
serviced.
AHRS1 GPS – AHRS1 operating 
exclusively in no-GPS mode.
The #1 AHRS is operating exclusively in no-GPS mode.  The G1000 system should be 
serviced.
AHRS2 GPS – AHRS2 operating 
exclusively in no-GPS mode.
The #2 AHRS is operating exclusively in no-GPS mode.  The G1000 system should be 
serviced.
AHRS MAG DB – AHRS magnetic 
model database version mismatch.The #1 AHRS and #2 AHRS magnetic model database versions do not match.
AHRS1 SRVC – AHRS1 Magnetic-field 
model needs update. 
The #1 AHRS earth magnetic field model is out of date.  Update magnetic field model 
when practical.
AHRS2 SRVC – AHRS2 Magnetic-field 
model needs update. 
The #2 AHRS earth magnetic field model is out of date.  Update magnetic field model 
when practical.
GEO LIMITS – AHRS1 too far North/
South, no magnetic compass.The aircraft is outside geographical limits for approved AHRS operation.  Heading is 
flagged as invalid.  GEO LIMITS – AHRS2 too far North/
South, no magnetic compass.
MANIFEST – GRS1 software 
mismatch, communication halted. The #1 AHRS has incorrect software installed.  The G1000 system should be serviced.
MANIFEST – GRS2 software 
mismatch, communication halted. The #2 AHRS has incorrect software installed.  The G1000 system should be serviced.
GMU 44 MESSAGE ADVISORIES
MessageComments
HDG FAULT – AHRS1 magnetometer 
fault has occurred.  
A fault has occurred in the #1 GMU 44.  Heading is flagged as invalid.  The AHRS uses 
GPS for backup mode operation.  The G1000 system should be serviced.
HDG FAULT – AHRS2 magnetometer 
fault has occurred.  
A fault has occurred in the #2 GMU 44.  Heading is flagged as invalid.  The AHRS uses 
GPS for backup mode operation.  The G1000 system should be serviced.
MANIFEST – GMU1 software 
mismatch, communication halted.The GMU 44 has incorrect software installed.  The G1000 system should be serviced.MANIFEST – GMU2 software 
mismatch, communication halted.
GSR 56 MESSAGE ADVISORIES
MessageComments
GSR1 FAIL – GSR1 has failed.A failure has been detected in the #1 GSR 56.  The system should be serviced.  
						

							Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A628
APPENDIX A
GDL 69A MESSAGE ADVISORIES
MessageComments
GDL69 CONFIG – GDL 69 config 
error.  Config service req’d. 
GDL 69 configuration settings do not match those of backup configuration memory.  
The G1000 system should be serviced.
GDL69 FAIL – GDL 69 has failed.A failure has been detected in the GDL 69.  The receiver is unavailable.  The G1000 
system should be serviced
MANIFEST – GDL software mismatch, 
communication halted.
The GDL 69 has incorrect software installed.  The G1000 system should be serviced.
GWX 68 MESSAGE ADVISORIES
MessageComments
GWX CONFIG – GWX config error.  
Config service req’d.
GWX 68 configuration settings do not match those of the GDU configuration.  The 
G1000 system should be serviced.
GWX FAIL – GWX is inoperative.The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting 
a fault.  The GWX 68 radar system should be serviced.
GWX SERVICE – GWX needs service.  
Return unit for repair.A failure has been detected in the GWX 68.  The GWX 68 may still be usable.
WX ALERT – Possible severe weather 
ahead.
The GWX 68 indicates severe weather within ±10º of the aircraft heading at a range 
of 80 to 320 nm.
MANIFEST – GWX software 
mismatch, communication halted.The GWX 68 has incorrect software installed.  The G1000 system should be serviced.
GDC 74B MESSAGE ADVISORIES
MessageComments
ADC1 ALT  EC – ADC1 altitude error 
correction is unavailable.GDC1 or GDC2 is reporting that the altitude error correction is unavailable.ADC2 ALT  EC – ADC2 altitude error 
correction is unavailable.
ADC1 AS  EC – ADC1 airspeed error 
correction is unavailable.GDC1 or GDC2 is reporting that the airspeed error correction is unavailable.ADC2 AS  EC – ADC2 airspeed error 
correction is unavailable.
MANIFEST – GDC1 software 
mismatch, communication halted.The GDC 74B has incorrect software installed.  The G1000 system should be serviced.MANIFEST – GDC2 software 
mismatch, communication halted.
GTS 820 MESSAGE ADVISORIES
MessageComments
GTS CONFIG – GTS config error.  
Config service req’d.
The GTS and GDU have incompatible configurations.  This alert is also set when the GTS 
has an invalid mode S addres sconfigured or the mode S address does not match bo\
th 
XPDR mode S addresses.
MANIFEST – GTS software 
mismatch, communication halted.The GTS has incorrect software installed.  The G1000 system should be serviced.  
						

							190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 629
APPENDIX A
GCU 475 MESSAGE ADVISORIES
MessageComments
GCU CNFG – GCU Config error.  
Config service req’d.
GCU 475 configuration settings do not match those of backup configuration memory.  
The G1000 system should be serviced.
GCU FAIL – GCU is inoperative.A failure has been detected in the GCU 475.  The GCU 475 is unavailable.
MANIFEST – GCU software mismatch, 
communication halted.The GCU 475 has incorrect software installed.  The G1000 system should be serviced.
GCU KEYSTK – GCU [key name] Key 
is stuck.
A key is stuck on the GCU 475 bezel.  Attempt to free the stuck key by pressing it 
several times.  The G1000 system should be serviced if the problem persists.
GMC 710 MESSAGE ADVISORIES
MessageComments
GMC CONFIG – GMC Config error.  
Config service req’d.Error in the configuration of the GMC 710.
GMC FAIL – GMC is inoperative.A failure has been detected in the GMC 710.  The GMC 710 is unavailable.
MANIFEST – GMC software 
mismatch.  Communication halted.The GMC 710 has incorrect software installed.  The G1000 system should be serviced.
GMC KEYSTK – GMC [key name] Key 
is stuck.
A key is stuck on the GMC 710 bezel.  Attempt to free the stuck key by pressing it 
several times.  The G1000 system should be serviced if the problem persists.
MISCELLANEOUS MESSAGE ADVISORIES
MessageComments
FPL WPT  LOCK – Flight plan waypoint 
is locked. 
Upon power-up, the G1000 system detects that a stored flight plan waypoint is 
locked.  This occurs when an navigation database update eliminates an obsolete 
waypoint.  The flight plan cannot find the specified waypoint and flags this message.  
This can also occur with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no longer exists in any database, 
Or 
update the waypoint name/identifier to reflect the new information. 
FPL WPT  MOVE – Flight plan 
waypoint moved.
The system has detected that a waypoint coordinate has changed due to a new 
navigation database update.  Verify that stored flight plans contain correct waypoint 
locations.
TIMER EXPIRD – Timer has expired.The system notifies the pilot that the timer has expired.
MISCELLANEOUS MESSAGE ADVISORIES  (CONT.)
MessageComments
DB CHANGE – Database changed.  
Verify user modified procedures.
This occurs when a stored flight plan contains procedures that have bee\
n manually 
edited.   This alert is issued only after an navigation database update.  Verify that the 
user-modified procedures in stored flight plans are correct and up to da\
te.
DB CHANGE – Database changed.  
Verify stored airways.
This occurs when a stored flight plan contains an airway that is no longer consistent 
with the navigation database.  This alert is issued only after an navigation database 
update.  Verify use of airways in stored flight plans and reload airways as needed.  
						

							Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A630
APPENDIX A
MISCELLANEOUS MESSAGE ADVISORIES  (CONT.)
MessageComments
FPL TRUNC – Flight plan has been 
truncated.
This occurs when a newly installed navigation database eliminates an obso\
lete 
approach or arrival used by a stored flight plan.  The obsolete procedure is removed 
from the flight plan.  Update flight plan with current arrival or approach.
LOCKED FPL – Cannot navigate 
locked flight plan.
This occurs when the pilot attempts to activate a stored flight plan that contains 
locked waypoint.  Remove locked waypoint from flight plan.  Update flight plan with 
current waypoint.  
WPT ARRIVAL – Arriving at waypoint 
-[xxxx]Arriving at waypoint [xxxx], where [xxxx] is the waypoint name.
STEEP TURN – Steep turn ahead.A steep turn is 15 seconds ahead.  Prepare to turn.
INSIDE ARSPC – Inside airspace.The aircraft is inside the special use airspace.
ARSPC AHEAD – Airspace ahead less 
than 10 minutes.
Special use airspace is ahead of aircraft.  The aircraft will penetrate the airspace within 
10 minutes.
ARSPC NEAR – Airspace near and 
ahead.Special use airspace is near and ahead of the aircraft position.
ARSPC NEAR – Airspace near – less 
than 2 nm.Special use airspace is within 2 nm of the aircraft position.
APR INACTV – Approach is not active.The system notifies the pilot that the loaded approach is not active.  Activate 
approach when required.
SLCT FREQ – Select appropriate 
frequency for approach.
The system notifies the pilot to load the approach frequency for the ap\
propriate NAV 
receiver.  Select the correct frequency for the approach.
SLCT NAV – Select NAV on CDI for 
approach.
The system notifies the pilot to set the CDI to the correct NAV receiver.  Set the CDI to 
the correct NAV receiver.
PTK FAIL – Parallel track unavailable: 
bad geometry.Bad parallel track geometry.
PTK FAIL – Parallel track unavailable: 
invalid leg type.Invalid leg type for parallel offset.
PTK FAIL – Parallel track unavailable: 
past IAF.IAF waypoint for parallel offset has been passed.
UNABLE V WPT – Can’t reach current 
vertical waypoint.
The current vertical waypoint can not be reached within the maximum flight path 
angle and vertical speed constraints.  The system automatically transitions to the next 
vertical waypoint.
VNV – Unavailable.  Unsupported leg 
type in flight plan.
The lateral flight plan contains a procedure turn, vector, or other unsupported leg 
type prior to the active vertical waypoint.  This prevents vertical guidance to the active 
vertical waypoint.
VNV – Unavailable.  Excessive track 
angle error.
The current track angle error exceeds the limit, causing the vertical deviation to go 
invalid.
VNV – Unavailable.  Excessive 
crosstrack error.The current crosstrack exceeds the limit, causing vertical deviation to go invalid.
VNV – Unavailable.  Parallel course 
selected.A parallel course has been selected, causing the vertical deviation to go invalid.
TRAFFIC FAIL – Traffic device has 
failed.
The G1000 is no longer receiving data from the traffic system.  The traffic device 
should be serviced.  
						

							190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 631
APPENDIX A
MISCELLANEOUS MESSAGE ADVISORIES  (CONT.)
MessageComments
NON WGS84 WPT – Do not use GPS 
for navigation to [xxxx]
The position of the selected waypoint [xxxx] is not calculated based on the WGS84 
map reference datum and may be positioned in error as displayed.  Do not use GPS to 
navigate to the selected non-WGS84 waypoint.
STRMSCP FAIL – Stormscope has 
failed.Stormscope has failed.  The G1000 system should be serviced.
FAILED PATH – A data path has failed.A data path connected to the GDU or the GIA 63/W has failed.
MAG VAR WARN – Large magnetic 
variance.  Verify all course angles. 
The GDU’s internal model cannot determine the exact magnetic variance for 
geographic locations near the magnetic poles.  Displayed magnetic course angles may 
differ from the actual magnetic heading by more than 2°.
SVS – SVS DISABLED: Out of available 
terrain region.
Synthetic Vision is disabled because the aircraft is not within the boundaries of the 
installed terrain database.
SVS – SVS DISABLED: Terrain DB 
resolution too low.
Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arc-
second or better) is not currently installed.
SCHEDULER [#] – .Message criteria entered by the user.
CHECK CRS – Database course for 
LOC1 / [LOC ID] is [CRS]°.
Selected course for LOC1 differs from published localizer course by more\
 than 10 
degrees.
CHECK CRS – Database course for 
LOC2 / [LOC ID] is [CRS]°.
Selected course for LOC2 differs from published localizer course by more\
 than 10 
degrees.
[PFD1, PFD2, or MFD1] CARD 1 REM 
– Card 1 was removed.  Reinsert card.
The SD card was removed from the top card slot of the PFD or MFD.  The SD card 
needs to be reinserted.
[PFD1, PFD2, or MFD1] CARD 2 REM 
– Card 2 was removed.  Reinsert card.
The SD card was removed from the bottom card slot of the PFD or MFD.  The SD card 
needs to be reinserted.
[PFD1, PFD2, or MFD1] CARD 1 ERR 
– Card 1 is invalid.The SD card in the top card slot of the PFD or MFD contains invalid data.
[PFD1, PFD2, or MFD1] CARD 2 ERR 
– Card 2 is invalid.The SD card in the bottom card slot of the PFD or MFD contains invalid data.
ECS – Service required.The Environmental Control System has failed.
EPS – Service required.The EPS option has been installed on an aircraft without the EPS system.  Software 
baseline and appropriate options shall be reloaded.
EPS – S/G speed sensor failed.The EPS option has been installed on an aircraft without the EPS system.  Software 
baseline and appropriate options shall be reloaded.
CRUISE I – Cruise I conditions met.Cruise I engine trend data log has been captured.
CRUISE II – Cruise II conditions met.Cruise II engine trend data log has been captured.
EXCEEDANCE – Engine exceedance 
data is being logged.An engine exceedance log has been captured.
REGISTER GFDS – Data services are 
inoperative, register w/GFDS.
The system is not registered with Garmin Flight Data Services, or its current 
registration data has failed authentication.
TRN AUD  FAIL  – Trn Awareness  audio 
source unavailable.The audio source for terrain awareness is offline.  Check GIA1 or GIA 2.
TERRAIN AUD  CFG  – Trn Awareness 
audio config error. Service req’d.Terrain audio alerts are not configured properly.  The system should be serviced  
						

							Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A632
APPENDIX A
AFCS ALERTS
Figure A-5   AFCS  Status AnnunciationAFCS Status 
Annunciation
The	following	alert	annunciations	appear	in	the	AFCS	System	Status	field	on	the	PFD.
Alert ConditionAnnunciation Description
Rudder Mistrim RightYaw servo providing sustained force in the indicated direction.  Aircraft rudder retrim 
after substantial pitch and power changes required.Rudder Mistrim Left
Aileron Mistrim Right
Roll servo providing sustained force in the indicated direction
Aileron Mistrim Left
Elevator Mistrim 
DownPitch servo providing sustained force in the indicated direction.  May indicate a 
failure of the pitch trim servo or trim system.Elevator Mistrim Up
Pitch Trim  Failure
(or stuck MEPT 
Switch)
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move MEPT switches separately to unstick
Yaw Trim  Failure
(or stuck MEYT 
Switch)
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move the MEYT switch to check if a stuck switch is causing the 
annunciation
Yaw Damper FailureYD control failure; AP also inoperative
Roll FailureRoll axis control failure; AP inoperative
Pitch FailurePitch axis control failure; AP inoperative
System FailureAP and MEPT are unavailable; FD may still be available
Preflight Test
Performing preflight system test; aural alert sounds at completion
Do not press the AP DISC Switch during servo power-up and preflight system tests 
as this may cause the preflight system test to fail or never to start (if servos fail their 
power-up tests).  Power must be cycled to the servos to remedy the situation.
Preflight system test failed; aural alert sounds at failure
 NOTE: Do not press the AP DISC switch during servo power-up and preflight system tests as this may cause 
the preflight system test to fail or never to start (if servos fail t\
heir power-up tests).  Power must be cycled 
to the servos to remedy the situation.  
						

							190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 633
APPENDIX A
TERRAIN-SVS ALERTS
Alert Type
PFD/MFD TERRAIN-
SVS Page
Annunciation
MFD
Pop-Up AlertAural Message
Reduced  Required Terrain  Clearance Warning 
(RTC)
“Warning; Terrain, Terrain”
Imminent Terrain  Impact Warning  (ITI)“Warning; Terrain, Terrain”
Reduced Required Obstacle Clearance Warning 
(ROC)
“Warning; Obstacle, 
Obstacle”
Imminent Obstacle Impact Warning (IOI)“Warning; Obstacle, 
Obstacle”
Reduced Required Terrain Clearance Caution 
(RTC)
“Caution; Terrain, Terrain”
Imminent Terrain Impact Caution (ITI)“Caution; Terrain, Terrain”
Reduced Required Obstacle Clearance Caution 
(ROC)
“Caution; Obstacle, 
Obstacle”
Imminent Obstacle Impact Caution (IOI)“Caution; Obstacle, 
Obstacle”
TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS
Alert TypePFD/MFD Alert 
Annunciation
TERRAIN-SVS Page 
AnnunciationAural Message
System Test in ProgressTERRAIN TESTNone
System Test  PassNoneNone“Terrain System Test OK”
Terrain Alerting is disabledNoneNone
MFD Terrain or Obstacle database 
unavailable or invalid.  Terrain-SVS 
operating with PFD Terrain or Obstacle 
databases
NoneTERRAIN DATABASE FAILURENone
Terrain System Test FailTERRAIN FAIL“Terrain System Failure”
Terrain or Obstacle database unavailable 
or invalid, invalid software configuration, 
system audio fault
TERRAIN FAIL“Terrain System Failure”
No GPS positionNO GPS POSITION“Terrain System Not 
Available”
Excessively degraded GPS signal, Out of 
database coverage areaNone“Terrain System Not 
Available”
Sufficient GPS signal received after lossNoneNone“Terrain  System Available”  
						

							Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A634
APPENDIX A
TAWS-B ALERTS
Annunciations	appear	on	the	PFD	and	MFD.		Pop-up	alerts	appear	only	on	the	MFD.
Alert Type
PFD/MFD TAWS 
Page
Annunciation
MFD Map Page
Pop-Up AlertAural Message
Excessive Descent Rate Warning (EDR)“Pull Up”
Reduced Required Terrain  Clearance Warning 
(RTC)or
“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
Imminent Terrain Impact Warning (ITI)
or
Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”
Reduced Required Obstacle Clearance Warning 
(ROC)or
“Obstacle, Obstacle; Pull Up, Pull Up”
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
Imminent Obstacle Impact Warning (IOI)
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”
Reduced Required Terrain Clearance Caution 
(RTC)or
“Caution, Terrain; Caution, Terrain”
or
“Terrain Ahead; Terrain Ahead”
Imminent Terrain Impact Caution (ITI)
or
“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution, Terrain”
Reduced Required Obstacle Clearance Caution 
(ROC)or
“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead;  Obstacle Ahead”
Imminent Obstacle Impact Caution (IOI)
or
“Obstacle Ahead;  Obstacle Ahead”
or
“Caution, Obstacle; Caution, Obstacle”
Premature Descent Alert Caution (PDA)“Too Low, Terrain”
Altitude Callout “500”NoneNone“Five-Hundred”
Excessive Descent Rate Caution (EDR)“Sink Rate”
Negative Climb Rate Caution (NCR)
or
“Don’t Sink”
or
“Too Low, Terrain”  
						

							190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 635
APPENDIX A
TAWS-B SYSTEM STATUS ANNUNCIATIONS
Alert TypePFD/MFD Alert 
AnnunciationTAWS-B  Page AnnunciationAural Message
System Test in ProgressTAWS TESTNone
System Test  PassNoneNone“TAWS System Test OK”
TAWS Alerting is disabledNoneNone
MFD Terrain or Obstacle database 
unavailable or invalid.  TAWS operating 
with PFD Terrain or Obstacle databases
NoneTERRAIN DATABASE FAILURENone
TAWS-B System Test FailTAWS FAIL“TAWS System Failure”
Terrain or Obstacle database unavailable 
or invalid, invalid software configuration, 
system audio fault
TAWS FAIL“TAWS System Failure”
No GPS positionNO GPS POSITION“TAWS  Not Available”
Excessively degraded GPS signal, Out of 
database coverage areaNone“TAWS  Not Available”
Sufficient GPS signal received after lossNoneNone“TAWS Available”
OTHER G1000 AURAL ALERTS
Voice AlertDescription
“Minimums, minimums”The aircraft has descended below the preset barometric minimum descent altitude.
“Vertical track”The aircraft is one minute from Top of Descent.  Issued only when vertical navigation is 
enabled.
“Airspeed, Airspeed”Played when the indicated airspeed is below a given threshold for a give\
n aircraft 
configuration.  Note this alert may be heard under normal conditions during the landin\
g flare.
“Traffic”Played when a Traffic Advisory  (TA) is issued with the TIS system.
“Traffic  Not Available”The aircraft is outside the Traffic Information Service (TIS) coverage area.
“Traffic, Traffic”Played when a Traffic Advisory  (TA) is issued with a TAS system.
“TAS System Test OK”Played when the TAS system passes a pilot-initiated self test.
“TAS System Test Failed”Played when the TAS system fails a pilot-initiated self test.
“One o’clock” through 
“Twelve o’clock”
or “No Bearing”
Played to indicate bearing of traffic from own aircraft (GTS 820 only).
“High”, “Low”, “Same Altitude” (if 
within 200 feet of own altitude), or 
“Altitude not available”
Played to indicate altitude of traffic relative to own aircraft (GTS 820 only).
“Less than one mile”,
 “One Mile” through “Ten Miles”, or 
“More than ten miles”
Played to indicate distance of traffic from own aircraft (GTS 820 only).  
						

							Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A636
APPENDIX A
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export ResultsDescription
‘Flight plan successfully imported.’A flight plan file stored on the SD card was successfully imported as a stored flight 
plan.
‘File contained user waypoints only.  User 
waypoints imported successfully.  No stored 
flight plan data was modified.’
The file stored on the SD card did not contain a flight plan, only user waypoints.  These 
waypoints have been saved to the system user waypoints.  No flight plans stored in 
the system have been modified.
‘No flight plan files found to import.’The SD card contains no flight plan data.
‘Flight plan import failed.’Flight plan data was not successfully imported from the SD card.
‘Flight plan partially imported.’Some flight plan waypoints were successfully imported from the SD card, however 
others had errors and were not imported.  A partial stored flight plan now exists in the 
system.
‘File contained user waypoints only.’The file stored on the SD card did not contain a flight plan, only user waypoints.  One 
or more of these waypoints did not import successfully.
‘Too many points.  Flight plan truncated.’The flight plan on the SD card contains more waypoints than the system can support.  
The flight plan was imported with as many waypoints as possible.
‘Some waypoints not loaded.  Waypoints 
locked.’
The flight plan on the SD card contains one or more waypoints that the system cannot 
find in the navigation database.  The flight plan has been imported, but must be 
edited within the system before it can be activated for use.
‘User waypoint database full.  Not all loaded.’The flight plan file on the SD card contains user waypoints.  The quantity of stored 
user waypoints has exceeded system capacity, therefore not all the user waypoints 
on the SD card have been imported.  Any flight plan user waypoints that were not 
imported are locked in the flight plan.  The flight plan must be edited within the 
system before it can be activated for use.
‘One or more user waypoints renamed.’One or more imported user waypoints were renamed when imported due to naming 
conflicts with waypoints already existing in the system.
‘Flight plan successfully exported.’The stored flight plan was successfully exported to the SD card.
‘Flight plan export failed.’The stored flight plan was not successfully exported to the SD card.  The SD card may 
not have sufficient available memory or the card may have been removed prematurely.