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User Manual - Rev H California Instruments
Avionics Software 31
3.1.3.1 Specific Test Limitations and Discrepancies
While every effort has been made to provide comprehensive coverage of the RTCA/DO-160 tests,
some limitations apply, largely due to hardware limitations of the Lx power source such as available
programming resolution or rounding. The following table lists specific implementation issues by test
number. The deviation from the standard requirement is shown in the “Actual setting” column. The
reason for the deviation is shown in the last column.
DC tests are NOT supported by the Lx/Ls Series
Vnom
Test
Std requirement
Actual setting
Reason
115VAC
A(CF):16.5.1.2
115 +/- .18 Vrms
115 +/- .2 Vrms
Resolution
115VAC
A(NF):16.5.1.2
115 +/- .18 Vrms
115 +/- .2 Vrms
Resolution
115VAC
A(WF):16.5.1.2
115 +/- .18 Vrms
115 +/- .2 Vrms
Resolution
115VAC
A(CF):16.5.1.2
115 +/- 1.24 Vrms
115 +/- 1.2 Vrms
Resolution
115VAC
A(NF):16.5.1.2
115 +/- 1.24 Vrms
115 +/- 1.2 Vrms
Resolution
115VAC
A(WF):16.5.1.2
115 +/- 1.24 Vrms
115 +/- 1.2 Vrms
Resolution
230VAC
A(CF):16.5.1.2
230 +/- .36 Vrms
230 +/- .4 Vrms
Resolution
230VAC
A(CF):16.5.1.2
230 +/- 2.48 Vrms
230 +/- 2.5 Vrms
Resolution
115VAC
A(CF):16.5.1.3
400Hz mod by .75Hz
400Hz mod by .8Hz
Resolution
115VAC
A(NF):16.5.1.3
360Hz mod by .75Hz
360Hz mod by .8Hz
Resolution
115VAC
A(NF):16.5.1.3
650Hz mod by .75Hz
650Hz mod by .8Hz
Resolution
115VAC
A(WF):16.5.1.3
360Hz mod by .75Hz
360Hz mod by .8Hz
Resolution
115VAC
A(WF):16.5.1.3
800Hz mod by .75Hz
800Hz mod by .8Hz
Resolution
230VAC
A(CF):16.5.1.3
400Hz mod by .75Hz
400Hz mod by .8Hz
Resolution
230VAC
A(CF):16.5.1.5.1
320V Transient
No deviation but –HV
option required to run.
Max voltage 320Vrms requires
400V range.
230VAC
A(CF):16.5.2.3.1
360V Transient
No deviation but –HV
option required to run.
Max voltage 360Vrms requires
400V range.
- Avionics Software Manual 2
- 1 Introduction 6
- 1.3 Availability of tests 7
- 2 Basic Operation 9
- 2.2 Test Control Window 11
- 2.3 Test Selection 13
- 2.4 Test Control 14
- 16 Avionics Software 16
- 18 Avionics Software 18
- Avionics Software 19 19
- 3.1 Test Coverage 22
- Avionics Software 23 23
- 24 Avionics Software 24
- Revision F 24
- Avionics Software 25 25
- Avionics Software 27 27
- 3.2 –160 Power Groups 32
- 3.4 Test Tables 33
- 34 Avionics Software 34
- 3.4.1.1 Table A(CF)115: 34
- Avionics Software 35 35
- 3.4.1.2 Table A(NF)115: 35
- 36 Avionics Software 36
- Avionics Software 37 37
- 3.4.1.3 Table A(WF)115: 37
- 38 Avionics Software 38
- Avionics Software 39 39
- 3.4.1.4 Table ADC28: 39
- 40 Avionics Software 40
- 3.4.1.5 Table BDC28: 40
- Avionics Software 41 41
- 3.4.1.6 Table ZDC28: 41
- 42 Avionics Software 42
- 3.4.1.7 Table A(CF)230: 42
- Avionics Software 43 43
- 3.4.1.8 Table ADC14: 43
- 44 Avionics Software 44
- 3.4.1.9 Table BDC14: 44
- Avionics Software 45 45
- 3.4.1.10 Table ZDC14: 45
- 46 Avionics Software 46
- 3.4.2.1 Table A(CF)115: 46
- Avionics Software 47 47
- 3.4.2.2 Table A(CF)115: 47
- 48 Avionics Software 48
- 3.4.2.3 Table A(CF)115: 48
- 52 Avionics Software 52
- 3.4.2.8 Table A(CF)115: 52
- 4.1 Test Coverage 55
- 56 Avionics Software 56
- 4.2 –B787 Power Groups 62
- 4.4 Test Tables 64
- Avionics Software 65 65
- 4.4.1 Rev C: 65
- 4.4.1.1 115VAC: 65
- 66 Avionics Software 66
- Avionics Software 67 67
- 68 Avionics Software 68
- Avionics Software 69 69
- 4.4.1.3 235VAC: 69
- 70 Avionics Software 70
- Avionics Software 71 71
- 72 Avionics Software 72
- Avionics Software 73 73
- 4.4.1.5 Type I DC: 73
- 74 Avionics Software 74
- 4.4.1.6 Type II DC: 74
- Avionics Software 75 75
- 4.4.1.7 Type III DC: 75
- 76 Avionics Software 76
- 4.4.1.8 Type IV DC: 76
- Avionics Software 77 77
- 4.4.1.9 Type V DC: 77
- 78 Avionics Software 78
- 4.4.1.10 Type VI DC: 78
- Avionics Software 79 79
- 4.4.2 Rev B: 79
- 4.4.2.1 115VAC: 79
- 80 Avionics Software 80
- Avionics Software 81 81
- 82 Avionics Software 82
- Avionics Software 83 83
- 4.4.2.3 235VAC: 83
- 84 Avionics Software 84
- Avionics Software 85 85
- 86 Avionics Software 86
- Avionics Software 87 87
- 4.4.2.5 Type I DC: 87
- 88 Avionics Software 88
- 4.4.2.6 Type II DC: 88
- Avionics Software 89 89
- 4.4.2.7 Type III DC: 89
- 90 Avionics Software 90
- 4.4.2.8 Type IV DC: 90
- Avionics Software 91 91
- 4.4.2.9 Type V DC: 91
- 92 Avionics Software 92
- 4.4.2.10 Type VI DC: 92
- Avionics Software 93 93
- 4.4.3 Rev A: 93
- 4.4.3.1 115VAC: 93
- 94 Avionics Software 94
- 4.4.3.2 230VAC: 94
- Avionics Software 95 95
- 96 Avionics Software 96
- 4.4.3.3 Type I DC: 96
- Avionics Software 97 97
- 4.4.3.4 Type II DC: 97
- 98 Avionics Software 98
- 4.4.3.5 Type III DC: 98
- Avionics Software 99 99
- 4.4.3.6 Type IV DC: 99
- 100 Avionics Software 100
- 4.4.3.7 Type V DC: 100
- 5.1 Test Coverage 101
- 102 Avionics Software 102
- 104 Avionics Software 104
- 5.2 –704 Power Groups 106
- 5.3 Test Tables 106
- 5.3.1.1 Table SAC: 107
- Avionics Software 107 107
- 5.3.1 Rev F: 107
- 108 Avionics Software 108
- 5.3.1.2 Table TAC: 108
- Avionics Software 109 109
- 5.3.1.3 Table SVF: 109
- 110 Avionics Software 110
- Avionics Software 111 111
- 5.3.1.4 Table TVF: 111
- 112 Avionics Software 112
- Avionics Software 113 113
- 5.3.1.5 Table SXF: 113
- 114 Avionics Software 114
- 5.3.1.6 Table LDC: 114
- 116 Avionics Software 116
- 5.3.4 Rev C: 116
- 5.3.4.1 Table SAC: 116
- Avionics Software 117 117
- 5.3.4.2 Table TAC: 117
- 118 Avionics Software 118
- 5.3.4.3 Table LDC: 118
- 5.3.4.4 Table HDC: 118
- Avionics Software 119 119
- 120 Avionics Software 120
- 5.3.5 Rev B: 120
- 5.3.5.1 Table SAC: 120
- Avionics Software 121 121
- 5.3.5.2 Table TAC: 121
- 122 Avionics Software 122
- 5.3.5.3 Table LDC: 122
- 5.3.5.4 Table HDC: 122
- Avionics Software 123 123
- 124 Avionics Software 124
- 5.3.6 Rev A: 124
- 5.3.6.1 Table SAC: 124
- Avionics Software 125 125
- 5.3.6.2 Table TAC: 125
- 126 Avionics Software 126
- 5.3.6.3 Table LDC: 126
- 6.1 Test Coverage 127
- Avionics Software 129 129
- 130 Avionics Software 130
- Avionics Software 133 133
- Avionics Software 135 135
- 138 Avionics Software 138
- 6.2 –A350 Power Groups 140
- 6.3 Test Tables 140
- Avionics Software 141 141
- 6.3.1.1 SCF: 141
- 142 Avionics Software 142
- Avionics Software 143 143
- 6.3.1.2 TCF: 143
- 144 Avionics Software 144
- Avionics Software 145 145
- 6.3.1.3 SVF: 145
- 146 Avionics Software 146
- Avionics Software 147 147
- 6.3.1.4 TVF: 147
- 148 Avionics Software 148
- Avionics Software 149 149
- 6.3.1.5 SCFH: 149
- 150 Avionics Software 150
- Avionics Software 151 151
- 6.3.1.6 TCFH: 151
- 152 Avionics Software 152
- Avionics Software 153 153
- 6.3.1.7 SVFH: 153
- 154 Avionics Software 154
- Avionics Software 155 155
- 6.3.1.8 TVFH: 155
- 156 Avionics Software 156
- Avionics Software 157 157
- 6.3.1.9 LDC: 157
- 158 Avionics Software 158
- 7.1 Test Coverage 159
- 7.2 –ABD Power Groups 162
- 7.3 –ABD Special Features 163
- Avionics Software 165 165
- 7.4 Test Tables 167
- Avionics Software 168
- 7.4.1 Revision E 168
- 7.4.1.1 Table A: 168
- Avionics Software 169 169
- 7.4.1.2 Table B: 169
- Avionics Software 171 171
- 7.4.1.3 Table C: 171
- 7.4.1.4 Table D: 173
- Avionics Software 173 173
- Avionics Software 175 175
- 7.4.1.5 Table E: 175
- Avionics Software 177 177
- 7.4.2 Revision D 177
- 7.4.2.1 Table A: 177
- Avionics Software 179 179
- 7.4.2.2 Table B: 179
- 7.4.2.3 Table C: 180
- Avionics Software 181 181
- Avionics Software 183 183
- 7.4.2.4 Table D: 183
- Avionics Software 185 185
- 7.4.2.5 Table E: 185
- 8.1 Test Coverage 186
- Avionics Software 189 189
- 8.2 –AMD Power Groups 193
- 8.4 Test Tables 194
- Avionics Software 195 195
- 8.4.1 Rev C: 195
- 8.4.1.1 Table SVF: 195
- 8.4.1.2 Table TVF: 196
- Avionics Software 197 197
- 8.4.1.3 Table SCF: 198
- Avionics Software 199 199
- 8.4.1.4 Table TCF: 199
- 8.4.1.5 Table LDC: 200
- Avionics Software 201 201
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