Garmin SA01456Wi_D Manual Page 122
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Page 4-38 G1000/GFC700 System Maintenance Manual – C90A/C90GT/C90GTi King Air
Revision F 190-00682-01
4.16.2 Capacity Test
NOTE
The PS-835 Emergency Power Supply must have completed a full charge prior to any
discharge testing. This test is performed with the battery removed from the aircraft.
A. Press and hold TEST SWITCH (Figure 4-7, Item 4) and observe the OUTPUT VOLTAGE
MONITOR LED's.
1) If the 24VDC OUTPUT VOLTAGE MONITOR LED comes on, proceed with Discharge Test
procedure.
2) If OUTPUT VOLTAGE MONITOR LED's do not come on, check fuses at bracket next to
battery and replace if blown. Perform Cell Isolation Test if no fuses are blown.
B. Discharge Test (Load Resistor)
1) Prepare for test by first constructing an X-Y graph similar to the one shown below. If possible,
use pre-printed graph paper to create a record of the discharge period along the X-axis and
voltage readings along the Y-axis.
2) Position all INDIVIDUAL CELL DIP SWITCHES (Figure 4-7, Item 5) to the ON position.
If the INDIVIDUAL CELL MONITOR LED DS12 is the only LED not illuminated, proceed to
the Cell Isolation Test.
3) Connect Digital Voltmeter leads to J1 connector pins 11 (+) and 7 (-).
- 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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