Ametek Compact i/iX Series Software Manual Manual do Utilizador descarregar pdf (Página 63)

User Manual - Rev H California Instruments

Avionics Software 63

The voltage of the two output terminals of this system with respect to the current return network will be

+130 and -130 respectively. All +/-130 volt equipment shall be connected between the +130 and -130

volt terminals.

Type VI DC power is provided exclusively for the landing gear electric braking system.

1 2 ... 58 59 60 61 62 63 64 65 66 67 68 ... 202 203

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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