Garmin SA01456Wi_D Manual Page 156
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- Table of contents
- TROUBLESHOOTING
- BOOKMARKS
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Page 5-32 G1000/GFC700 System Maintenance Manual – C90A/C90GT/C90GTi King Air
Revision F 190-00682-01
Annunciation Condition Resolution
Aileron Mistrim
Right
• Check for possible fuel imbalance.
• Check aileron control adjustments.
• If mistrim condition still exists remove and replace the roll
servo.
Aileron Mistrim
Left
Rudder Mistrim
Right
• Check rudder control adjustments.
• If mistrim condition still exists remove and replace the yaw
servo.
Rudder Mistrim
Left
Pre-Flight Test
Fails
• Allow the system to complete pre-flight tests.
• The preflight test should finish within 2 minutes. If it does
not pass, the red ‘PFT’ annunciation is shown. In case of
PFT failure, see Section 5.6.5 for additional PFT diagnostics.
Table 5-4. AFCS General Troubleshooting
Condition Resolution
Poor AP Performance
(Limited AP Authority)
• Check each servo mount slip clutch per Section 4.9. Verify
the clutches are not excessively loose and are within
torque limits.
• Check aircraft controls for proper adjustment per the King
Air Model 90 Series Maintenance Manual.
• Check aircraft control cables for proper tension per the
King Air Model 90 Series Maintenance Manual.
AP DISC Problems
• For intermittent nuisance disconnects with no AFCS of PFT
alert, check A/P disconnect switch and wiring for
intermittent faults.
• If an AFCS or PFT alert is displayed at the time of the
disconnect, troubleshoot per Section 5.5.
• Check the GIA AFCS Fault Logs according to Section
5.6.4. If a Mon Prmtr Invalid message is received, check
for valid true airspeed. A faulty GTP 59 OAT probe may
cause TAS to become invalid, which will flag the
Mon Prmtr Invalid message.
• Contact Garmin Product Support for assistance
Loss of Manual Electric Trim
• Check pitch trim servo status.
• Check MET switch discrete inputs to both GIAs by going to
the GIA I/O Configuration page and selecting DISCRETE
IN inputs.
AutoTrim Inoperative
• Check flap-in-motion discrete inputs to both GIAs for proper
operation by going to the GIA I/O Configuration page and
selected DISCRETE IN inputs. See Section 4.8.
• If DATA indicator fails to illuminate or illuminates
incorrectly, troubleshoot flap motor & discrete input wiring
(refer to G1000/GFC 700 Wiring Diagram, listed in Table
1-2).
- 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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