Garmin SA01456Wi_D Manual Page 171
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G1000/GFC700 System Maintenance Manual – C90A/C90GT/C90GTi King Air Page 5-47
190-00682-01 Revision F
5.8 GDU 104X Troubleshooting
5.8.1 GDU 104X Common Problems
Symptom Recommended Action
Display is blank
• Ensure that a cell phone or a device using cell phone technology is not
turned on (even in a monitoring state) in the cabin.
• Cycle power.
9 If GDU recovers, observe display for yellow text containing error
information at the top of the screen. If message indicates software
need to be re-loaded, then re-load software. Otherwise, replace
the GDU.
• Use a bright light to verify LCD is active.
9 Adjust avionics dimmer control full clockwise.
9 Manually turn up backlight on the PFD and load configuration files
to the GDU.
• Ensure slide lock is fully engaged with the locking tabs on the back of
the unit.
9 If slide lock is not fully engaged, remove connector and verify the
locking tabs on the GDU are perpendicular to the connector. If
necessary, straighten them before reseating connector.
• Ensure GDU is receiving power. If a circuit breaker is tripped,
determine source of short before resetting breaker.
• Ensure circuit breakers have not failed and power wire connections are
secure.
• Swap PFD1 and PFD2.
9 If problem follows unit, replace the display. Please note the
position it failed in (PFD1/2).
9 If problem does not follow unit, troubleshoot aircraft wiring for fault.
Display resets
Display flickers
SD card is stuck in GDU
• DO NOT insert a screwdriver of any length into the card slot.
• DO NOT pry against the overlay.
• DO NOT force the SD Card out.
• Use a small screwdriver in the groove on the side of the exposed end of
the card to help pull out the card.
• Push the card in further to release the card locking mechanism.
• Check SD Card for having more than one label. Two or more labels on
the card will cause sticking.
9 Remove all but one label.
• Ensure the SD card is from Cactus or SanDisk. Use of other SD Cards
is not recommended.
• If card was inserted with the label facing to the right, do not attempt to
remove. Return the unit to Garmin for repair.
A button/knob/joystick does not
appear to function
• Go to the GDU TEST page in configuration mode and verify button,
knob, or joystick operates correctly by observing a change in color from
red to green in the button/knob/joystick icon when the
button/knob/joystick is pressed. If a button is stuck, the button icon will
be green without pressing the button as soon as you turn to the GDU
TEST page.
9 If problem is verified, replace GDU.
- G1000 / GFC 700 1
- System Maintenance Manual 1
- Hawker Beechcraft 1
- FIGURE PAGE 8
- TABLE PAGE 9
- 1 INTRODUCTION 11
- 1.2 Organization 13
- 1.3.1 Units of Measure 14
- 1.4 Publications 15
- Hawker Beechcraft Document 16
- 2 SYSTEM DESCRIPTION 17
- 2.1.9 OAT Probe (2) 21
- 2.1.12 GDL 69A Datalink 22
- 2.1.13 GWX 68 Weather Radar 22
- 2.4 Shield Block Grounds 28
- 3.1.1 Softkeys 32
- 3.1.2 FMS Knob 32
- 3.3 GMC 710 - AFCS Controls 33
- 3.4 GMA 1347D Audio Panel 34
- 3.5 G1000 Normal Mode 36
- 3.6 Reversionary Mode 37
- SET Column ACTIVE Column 39
- 3.7.2 Configuration Prompts 40
- 3.8.1 G1000 Software Image 43
- 3.8.2 Loader Card Creation 44
- 3.8.3 Software Files 47
- G1000 System Upload Selection 55
- 3.9.3 Software Check 59
- 3.9.4.3 TIS Configuration 66
- 7. Deactivate cursor 72
- 3.9.7 TAWS B Enable 76
- 3.9.11 SVS/Pathways Enable 80
- 3.9.12 ESP Enable 81
- 3.11 Splash Screen Loading 82
- 4.2 Servicing Information 87
- 4.2.2 Required Tools 88
- 4.3 Maintenance Intervals 89
- G1000/GFC700 Equipment 89
- G1000 Accessories 91
- 4.4 Visual Inspection 94
- 4.5 Electrical Bonding Test 99
- 4.5.1 Requirements 99
- 4.5.2 Test Equipment 99
- Procedure in Section 4.9.3 105
- MFD circuit breaker: 113
- 4.11 Engine Data Check 115
- 4.12 Trim Annunciator Check 117
- 4.16.1 Charge Check 120
- 4.16.2 Capacity Test 122
- 4.16.3 Cell Isolation Test 123
- 4.16.4 Charging Procedure 123
- 5 TROUBLESHOOTING 125
- 5.1 G1000 Alerting System 126
- 190-00682-01 Revision F 127
- Aural & Audio Alerts 127
- 5.2 System Annunciations 128
- 5.2.1 Failed Path Messages 128
- (applies only 136
- 0636.03 and 136
- Revision F 190-00682-01 146
- 5.2.4 ADF/DME Failure 150
- Message Advisory Solution 151
- 5.4 TAWS Troubleshooting 152
- Condition Resolution 156
- 5.6.3 GFC Status Page 157
- DRIVE SERVO 158
- SERVO DATA 158
- SLIP CLUTCH TEST RESULTS 158
- PFT Faults 165
- Normal Mode Faults 165
- 5.7.1 Overview 170
- 5.7.2 Data Path Failures 170
- 5.8 GDU 104X Troubleshooting 171
- 5.9 GDU 104X Alerts 173
- 5.9.2 Database Alerts 175
- 5.9.3 Cooling Alerts 176
- 5.9.4 Key Alerts 177
- 5.9.5 Miscellaneous Alerts 177
- 5.9.6 GMA Common Problems 179
- 5.9.7 GMA Alerts 180
- 5.10 GIA 63 Troubleshooting 181
- 5.10.1 COM 181
- 5.10.2 NAV 181
- 5.10.3 G/S 181
- 5.10.4 GPS 182
- 5.11 GIA Alert Messages 183
- 5.11.1 COM Alerts 183
- 5.11.2 NAV Alerts 185
- 5.11.3 Glideslope Alerts 186
- 5.11.4 GPS Alerts 186
- 5.11.5 GIA Cooling Alerts 188
- GIA Configuration Alerts 189
- 5.12 GEA Troubleshooting 190
- 5.12.1 GEA Alerts 190
- 5.13 GTX Troubleshooting 191
- 5.13.1 GTX Alerts 191
- GDL 69A Common Problems 192
- 5.14.2 GDL 69A Alerts 193
- 5.15.1 AHRS Common Problems 194
- 5.15.2 GRS Alerts 195
- 5.15.3 GMU Alerts 197
- 5.16.2 GDC 74B Alerts 200
- 5.17 GWX 68 Troubleshooting 201
- 5.18 GMC 710 Troubleshooting 202
- GCU 475 Alerts and Problems 203
- 5.21 Backshell Connectors 206
- Symptom Recommended Action 211
- 6.1 GDU 1040A/1500 214
- 6.2 GMA 1347D Audio Panel 214
- 6.5 GTX 33 Transponder 216
- 6.7 GTP 59 OAT Probe 216
- 6.8 GRS 77 AHRS 217
- 6.9 GMU 44 Magnetometer 217
- 6.10 GDL 69A 217
- 6.11 GSA 80/81 Servos 218
- 6.13 GCU 475 219
- 6.14 GMC 710 219
- 6.15 GWX 68 220
- 3 Screw 1 211-60234-08 223
- 6.18 GPS/WAAS Antennas 224
- 6.24 Standby Altimeter 227
- 6.26 Avionics Cooling Fans 228
- 6.27 GDU Cooling Fans 229
- CAUTION 231
- 7.1.1 PFD/MFD Test 232
- 7.2 GMA 1347D Audio Panel 233
- 7.2.1 GMA 1347D Test 233
- 7.2.1.6 Marker Beacon Test 236
- • GEAR 237
- • STALL 237
- 7.3.1 GIA 63W Test 240
- 7.4.1 GEA 71 Test 243
- 7.4.2.2 ITT Functional Test 245
- 129 +/- 10 100 247
- 40.6 +/- .35 58 247
- 71.4 +/- .35 102 247
- 140 100 +/- 10 249
- 7.5 GTX 33 Transponder 250
- 7.5.2 GTX 33 Test 251
- 7.6.3 OAT Probe Check 255
- Procedure B: 257
- 7.7.6 GRS/GMU Test 264
- 7.8 GDL 69A XM Data Link 266
- 7.8.1 GDL 69A Test 266
- 7.9 GSA 80/81 Servos 266
- 7.10 GCU 475 FMS Controller 267
- 7.10.1 GCU 475 Test 267
- 7.11.1 GMC 710 Test 268
- 7.12 GWX 68 Weather Radar 269
- 7.12.1 GWX 68 Test 269
- 7.15 TAWS Functional Check 273
- 7.19 DME Functional Check 277
- 7.20 ADF Functional Check 278
- 7.23 ESP Functional Check 284
- 8.1.1 GPS Failure Test 288
- 8.1.2 GIA Failure Test 289
- 8.1.3 Display Failure Test 290
- 8.2 GFC 700 Ground Checkout 296
- 8.2.1 Pre-Flight Test 296
- 8.2.2 AFCS Switch Checks 297
- 8.2.6 VOR/LOC/GS Test 299
- 8.3 Maintenance Records 300
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