W DOC AIRBUS | MMEL OPS PROC

Brakes Temperature Indication on the WHEEL SD page

32-07-01ABrakes Temperature Indication on the WHEEL SD page
Applicable to: -
- Flight Preparation/Limitations
The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :
  • Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS).
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
  • Enter with the aircraft landing weight, and
  • Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
  • Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases.
    NOTE:
    In the case of a dispatch with one brake inoperative ( Refer to item 01 Main Wheel Brake or Refer to item 02 Green System Brake), the brake energy accumulated is increased by 34 %.
Brake Energy with Thrust Reverser Use
MMEL ILLUSTRATION
Brake Energy without Thrust Reverser Use
MMEL ILLUSTRATION
Brake Cooling Time Table
Determination of the brake cooling time:
EXAMPLE:
25
99
49
90
45
94
46
97
48
100
50
====> TIME (min) WITHOUT BRAKE COOLING FAN
====> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row.
For Example, with Energy = 25 MJ, and OAT = 15 °C, entering the next adjacent column/row (Energy = 25 MJ, OAT = 20 °C) gives the following results:
  • Without brake cooling fan: 112 min
  • With brake cooling fan: 55 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY
(MJ)
OAT (°C)
-50 -40 -30 -20 -10 0 10 20 30 40 50 55
0 28 14 17 20 23 26 29 34 39 45 52 56
14 7 9 10 11 13 15 17 20 23 26 28
5 52 41 44 48 50 54 57 62 67 73 80 84
26 20 22 24 25 27 28 31 33 36 40 42
10 69 58 62 65 68 72 75 80 85 91 98 102
34 29 31 32 34 36 37 39 42 45 49 51
15 81 71 75 78 81 85 88 93 98 105 112 116
40 35 37 39 40 42 44 46 49 52 55 57
20 91 82 85 89 92 95 99 103 109 115 122 126
45 40 42 44 45 47 49 51 54 57 60 62
25 99 90 94 97 100 104 108 112 118 124 131 135
49 45 46 48 50 51 53 55 58 61 65 67
30 106 98 101 105 108 111 115 119 125 131 138 142
53 48 50 52 53 55 57 59 62 65 68 70
35 113 104 108 111 114 118 121 126 131 138 145 149
56 51 53 55 56 58 60 62 65 68 71 73
40 118 110 113 117 120 124 127 132 137 143 150 154
58 54 56 58 59 61 63 65 68 71 74 76
45 123 115 118 122 125 129 132 137 142 149 156 160
61 57 58 60 62 64 65 68 70 73 77 79
50 128 120 123 127 130 133 137 141 147 153 160 164
63 59 61 62 64 66 68 70 73 76 79 81
55 132 124 127 131 134 138 141 146 151 158 165 169
65 61 63 65 66 68 70 72 75 78 81 83
60 136 128 131 135 138 142 145 150 155 161 169 173
67 63 65 67 68 70 72 74 77 80 83 85
65 139 131 135 138 142 145 149 153 159 165 172 176
69 65 67 68 70 72 73 76 78 81 85 87
70 143 135 138 142 145 149 152 157 162 169 176 180
70 67 68 70 72 73 75 77 80 83 87 89
75 146 138 141 145 148 152 156 160 166 172 179 183
72 68 70 72 73 75 77 79 82 85 88 90
80 149 141 144 148 151 155 159 163 169 175 182 186
73 70 71 73 75 76 78 80 83 86 90 92
- After Engine Start
In the case of a false BRAKES HOT alert displayed on the EWD:
  • EMER CANC pbPress
NOTE:
In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION:
The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
32-07-01ABrakes Temperature Indication on the WHEEL SD page
Applicable to: -
- Flight Preparation/Limitations
The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :
  • Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
  • Enter with the aircraft landing weight, and
  • Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
  • Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases.
    NOTE:
    In the case of a dispatch with one brake inoperative ( Refer to item 01 Main Wheel Brake or Refer to item 02 Green System Brake), the brake energy accumulated is increased by 34 %.
Brake Energy with Thrust Reverser Use
MMEL ILLUSTRATION
Brake Energy without Thrust Reverser Use
MMEL ILLUSTRATION
Brake Cooling Time Table
Determination of the brake cooling time:
EXAMPLE:
25
73
27
69
26
72
27
75
28
79
30
====> TIME (min) WITHOUT BRAKE COOLING FAN
====> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row.
For Example, with Energy = 25 MJ, and OAT = 15 °C, entering the next adjacent column/row (Energy = 25 MJ, OAT = 20 °C) gives the following results:
  • Without brake cooling fan: 88 min
  • With brake cooling fan: 33 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY
(MJ)
OAT (°C)
-50 -40 -30 -20 -10 0 10 20 30 40 50 55
0 0 0 0 0 0 0 0 0 0 0 0 2
0 0 0 0 0 0 0 0 0 0 0 1
5 11 5 8 11 13 16 19 23 27 32 37 39
4 2 3 4 5 6 8 9 10 12 14 15
10 33 28 31 34 37 40 43 46 51 55 60 63
12 11 12 13 14 15 16 18 19 21 23 24
15 49 45 48 51 54 57 60 63 68 72 77 80
19 17 18 19 20 21 23 24 26 27 29 30
20 62 58 61 64 67 70 74 77 81 86 91 93
23 22 23 24 25 26 28 29 31 32 34 35
25 73 69 72 75 79 82 85 88 93 97 102 105
27 26 27 28 30 31 32 33 35 36 38 39
30 82 79 82 85 88 91 95 98 102 107 112 114
31 30 31 32 33 34 35 37 38 40 42 43
35 90 87 90 93 96 99 103 106 111 115 120 123
34 33 34 35 36 37 39 40 41 43 45 46
40 97 95 97 101 104 107 110 114 118 123 127 130
37 36 37 38 39 40 41 43 44 46 48 49
45 104 101 104 107 110 113 117 120 125 129 134 137
39 38 39 40 41 42 44 45 47 48 50 51
50 110 107 110 113 116 119 123 126 131 135 140 143
41 40 41 42 44 45 46 47 49 51 52 53
55 115 113 116 119 122 125 128 132 136 141 146 148
43 42 43 44 46 47 48 49 51 53 54 55
60 120 118 121 124 127 130 134 137 141 146 151 153
45 44 45 46 48 49 50 51 53 55 56 57
65 125 123 125 128 132 135 138 142 146 151 155 158
47 46 47 48 49 50 52 53 55 56 58 59
70 129 127 130 133 136 139 143 146 150 155 160 162
48 47 49 50 51 52 53 55 56 58 60 61
75 133 131 134 137 140 143 147 150 154 159 164 167
50 49 50 51 52 54 55 56 58 59 61 62
80 137 135 138 141 144 147 151 154 158 163 168 170
51 50 52 53 54 55 56 58 59 61 63 64
- After Engine Start
In the case of a false BRAKES HOT alert displayed on the EWD:
  • EMER CANC pbPress
NOTE:
In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION:
The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
32-07-01ABrakes Temperature Indication on the WHEEL
Applicable to: -
- Flight Preparation/Limitations
The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :
  • Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS).
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
  • Enter with the aircraft landing weight, and
  • Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
  • Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases.
    NOTE:
    In the case of a dispatch with one brake inoperative ( Refer to item 01 Main Wheel Brake or Refer to item 02 Green System Brake), the brake energy accumulated is increased by 34 %.
Brake Energy with Thrust Reverser Use
MMEL ILLUSTRATION
Brake Energy without Thrust Reverser Use
MMEL ILLUSTRATION
Brake Cooling Time Table
Determination of the brake cooling time:
EXAMPLE:
55
152
46
153
46
154
46
155
46
155
47
====> TIME (min) WITHOUT BRAKE COOLING FAN
====> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row.
For Example, with Energy = 78 MJ, and OAT = 15 °C, entering the next adjacent column/row (Energy = 80 MJ, OAT = 20 °C) gives the following results:
  • Without brake cooling fan: 189 min
  • With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY
(MJ)
OAT (°C)
-50
-40
-30
-20
-10
0
10
20
30
40
50
55
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
5
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
10
0
0
0
0
0
0
4
1
9
3
14
4
19
6
23
7
27
8
31
9
35
10
37
11
15
31
9
35
10
38
11
42
12
45
13
48
14
51
15
54
16
57
17
60
18
62
19
64
19
20
59
18
62
19
65
19
67
20
70
21
72
22
74
22
77
23
79
24
81
24
83
25
84
25
25
81
24
83
25
85
25
87
26
89
27
91
27
92
28
94
28
96
29
98
29
99
30
100
30
30
98
29
99
30
101
30
103
31
104
31
106
32
107
32
109
33
110
33
112
34
113
34
114
34
35
112
34
113
34
115
34
116
35
117
35
119
36
120
36
121
36
123
37
124
37
125
38
126
38
40
124
37
125
37
126
38
127
38
129
39
130
39
131
39
132
40
133
40
134
40
135
41
136
41
45
134
40
135
41
136
41
137
41
139
42
140
42
141
42
142
42
143
43
144
43
145
43
145
44
50
144
43
145
43
146
44
146
44
147
44
148
45
149
45
150
45
151
45
152
46
153
46
153
46
55
152
46
153
46
154
46
155
46
155
47
156
47
157
47
158
47
159
48
160
48
160
48
161
48
60
160
48
160
48
161
48
162
49
163
49
164
49
164
49
165
50
166
50
167
50
167
50
168
50
65
167
50
167
50
168
50
169
51
170
51
170
51
171
51
172
52
172
52
173
52
174
52
174
52
70
173
52
174
52
174
52
175
53
176
53
176
53
177
53
178
53
178
54
179
54
180
54
180
54
75
179
54
180
54
180
54
181
54
182
54
182
55
183
55
183
55
184
55
185
55
185
56
186
56
80
185
55
185
56
186
56
186
56
187
56
188
56
188
56
189
57
189
57
190
57
190
57
191
57
85
190
57
190
57
191
57
191
57
192
58
193
58
193
58
194
58
194
58
195
58
195
59
196
59
90
195
58
195
59
196
59
196
59
197
59
197
59
198
59
198
60
199
60
199
60
200
60
200
60
95
199
60
200
60
200
60
201
60
201
60
202
61
202
61
203
61
203
61
204
61
204
61
205
61
100
204
61
204
61
205
61
205
62
206
62
206
62
207
62
207
62
208
62
208
62
208
63
209
63
105
208
62
208
63
209
63
209
63
210
63
210
63
211
63
211
63
212
63
212
64
212
64
213
64
110
212
64
212
64
213
64
213
64
214
64
214
64
215
64
215
64
215
65
216
65
216
65
216
65
115
216
65
216
65
217
65
217
65
217
65
218
65
218
65
219
66
219
66
219
66
220
66
220
66
120
219
66
220
66
220
66
221
66
221
66
221
66
222
67
222
67
222
67
223
67
223
67
223
67
A320
Messier/Goodrich - 03.01.05 - F476021.txt
- After Engine Start
In the case of a false BRAKES HOT alert displayed on the EWD:
  • EMER CANC pbPress
NOTE:
In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION:
The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
32-07-01ABrakes Temperature Indication on the WHEEL SD page
Applicable to: -
- Flight Preparation/Limitations
The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :
  • Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS).
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
  • Enter with the aircraft landing weight, and
  • Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
  • Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases.
    NOTE:
    In the case of a dispatch with one brake inoperative ( Refer to item 01 Main Wheel Brake or Refer to item 02 Green System Brake), the brake energy accumulated is increased by 34 %.
Brake Energy with Thrust Reverser Use
MMEL ILLUSTRATION
Brake Energy without Thrust Reverser Use
MMEL ILLUSTRATION
Brake Cooling Time Table
EXAMPLE:
55
152
46
153
46
154
46
155
46
155
47
====> TIME (min) WITHOUT BRAKE COOLING FAN
====> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row.
For Example, with Energy = 78 MJ, and OAT = 15 °C, entering the next adjacent column/row (Energy = 80 MJ, OAT = 20 °C) gives the following results:
  • Without brake cooling fan: 189 min
  • With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY
(MJ)
OAT (°C)
-50
-40
-30
-20
-10
0
10
20
30
40
50
55
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
5
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
10
0
0
0
0
0
0
4
1
9
3
14
4
19
6
23
7
27
8
31
9
35
10
37
11
15
31
9
35
10
38
11
42
12
45
13
48
14
51
15
54
16
57
17
60
18
62
19
64
19
20
59
18
62
19
65
19
67
20
70
21
72
22
74
22
77
23
79
24
81
24
83
25
84
25
25
81
24
83
25
85
25
87
26
89
27
91
27
92
28
94
28
96
29
98
29
99
30
100
30
30
98
29
99
30
101
30
103
31
104
31
106
32
107
32
109
33
110
33
112
34
113
34
114
34
35
112
34
113
34
115
34
116
35
117
35
119
36
120
36
121
36
123
37
124
37
125
38
126
38
40
124
37
125
37
126
38
127
38
129
39
130
39
131
39
132
40
133
40
134
40
135
41
136
41
45
134
40
135
41
136
41
137
41
139
42
140
42
141
42
142
42
143
43
144
43
145
43
145
44
50
144
43
145
43
146
44
146
44
147
44
148
45
149
45
150
45
151
45
152
46
153
46
153
46
55
152
46
153
46
154
46
155
46
155
47
156
47
157
47
158
47
159
48
160
48
160
48
161
48
60
160
48
160
48
161
48
162
49
163
49
164
49
164
49
165
50
166
50
167
50
167
50
168
50
65
167
50
167
50
168
50
169
51
170
51
170
51
171
51
172
52
172
52
173
52
174
52
174
52
70
173
52
174
52
174
52
175
53
176
53
176
53
177
53
178
53
178
54
179
54
180
54
180
54
75
179
54
180
54
180
54
181
54
182
54
182
55
183
55
183
55
184
55
185
55
185
56
186
56
80
185
55
185
56
186
56
186
56
187
56
188
56
188
56
189
57
189
57
190
57
190
57
191
57
85
190
57
190
57
191
57
191
57
192
58
193
58
193
58
194
58
194
58
195
58
195
59
196
59
90
195
58
195
59
196
59
196
59
197
59
197
59
198
59
198
60
199
60
199
60
200
60
200
60
95
199
60
200
60
200
60
201
60
201
60
202
61
202
61
203
61
203
61
204
61
204
61
205
61
100
204
61
204
61
205
61
205
62
206
62
206
62
207
62
207
62
208
62
208
62
208
63
209
63
105
208
62
208
63
209
63
209
63
210
63
210
63
211
63
211
63
212
63
212
64
212
64
213
64
110
212
64
212
64
213
64
213
64
214
64
214
64
215
64
215
64
215
65
216
65
216
65
216
65
115
216
65
216
65
217
65
217
65
217
65
218
65
218
65
219
66
219
66
219
66
220
66
220
66
120
219
66
220
66
220
66
221
66
221
66
221
66
222
67
222
67
222
67
223
67
223
67
223
67
A319
Messier/Goodrich - 03.01.05 - F476021.txt
- After Engine Start
In the case of a false BRAKES HOT alert displayed on the EWD:
  • EMER CANC pbPress
NOTE:
In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION:
The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
32-07-01ABrakes Temperature Indication on the WHEEL SD page
Applicable to: -
- Flight Preparation/Limitations
The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time.
BRAKE ENERGY GRAPH
If MAX reverser thrust was selected for all reversers during the braking phase:
Enter the brake energy graph: WITH THRUST REVERSERS USE.
If MAX reverser thrust was NOT selected for all reversers during the braking phase:
Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) :
  • Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING :
  • Enter with the aircraft landing weight, and
  • Enter with the touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
  • Apply airport pressure altitude, temperature, wind and runway slope corrections.
  • Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases.
    NOTE:
    In the case of a dispatch with one brake inoperative ( Refer to item 01 Main Wheel Brake or Refer to item 02 Green System Brake), the brake energy accumulated is increased by 34 %.
Brake Energy with Thrust Reverser Use
MMEL ILLUSTRATION
Brake Energy without Thrust Reverser Use
MMEL ILLUSTRATION
Brake Cooling Time Table
Determination of the brake cooling time:
EXAMPLE:
55
152
46
153
46
154
46
155
46
155
47
====> TIME (MN) WITHOUT BRAKE COOLING FAN
====> TIME (MN) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row.
For Example, with Energy = 78 MJ, and OAT = 15 °C, entering the next adjacent column/row (Energy = 80 MJ, OAT = 20 °C) gives the following results:
  • Without brake cooling fan: 189 min
  • With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time.
GROUND BRAKE COOLING TIME (min)
ENERGY
(MJ)
OAT (°C)
-50
-40
-30
-20
-10
0
10
20
30
40
50
55
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
5
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
10
0
0
0
0
0
0
4
1
9
3
14
4
19
6
23
7
27
8
31
9
35
10
37
11
15
31
9
35
10
38
11
42
12
45
13
48
14
51
15
54
16
57
17
60
18
62
19
64
19
20
59
18
62
19
65
19
67
20
70
21
72
22
74
22
77
23
79
24
81
24
83
25
84
25
25
81
24
83
25
85
25
87
26
89
27
91
27
92
28
94
28
96
29
98
29
99
30
100
30
30
98
29
99
30
101
30
103
31
104
31
106
32
107
32
109
33
110
33
112
34
113
34
114
34
35
112
34
113
34
115
34
116
35
117
35
119
36
120
36
121
36
123
37
124
37
125
38
126
38
40
124
37
125
37
126
38
127
38
129
39
130
39
131
39
132
40
133
40
134
40
135
41
136
41
45
134
40
135
41
136
41
137
41
139
42
140
42
141
42
142
42
143
43
144
43
145
43
145
44
50
144
43
145
43
146
44
146
44
147
44
148
45
149
45
150
45
151
45
152
46
153
46
153
46
55
152
46
153
46
154
46
155
46
155
47
156
47
157
47
158
47
159
48
160
48
160
48
161
48
60
160
48
160
48
161
48
162
49
163
49
164
49
164
49
165
50
166
50
167
50
167
50
168
50
65
167
50
167
50
168
50
169
51
170
51
170
51
171
51
172
52
172
52
173
52
174
52
174
52
70
173
52
174
52
174
52
175
53
176
53
176
53
177
53
178
53
178
54
179
54
180
54
180
54
75
179
54
180
54
180
54
181
54
182
54
182
55
183
55
183
55
184
55
185
55
185
56
186
56
80
185
55
185
56
186
56
186
56
187
56
188
56
188
56
189
57
189
57
190
57
190
57
191
57
85
190
57
190
57
191
57
191
57
192
58
193
58
193
58
194
58
194
58
195
58
195
59
196
59
90
195
58
195
59
196
59
196
59
197
59
197
59
198
59
198
60
199
60
199
60
200
60
200
60
95
199
60
200
60
200
60
201
60
201
60
202
61
202
61
203
61
203
61
204
61
204
61
205
61
100
204
61
204
61
205
61
205
62
206
62
206
62
207
62
207
62
208
62
208
62
208
63
209
63
105
208
62
208
63
209
63
209
63
210
63
210
63
211
63
211
63
212
63
212
64
212
64
213
64
110
212
64
212
64
213
64
213
64
214
64
214
64
215
64
215
64
215
65
216
65
216
65
216
65
115
216
65
216
65
217
65
217
65
217
65
218
65
218
65
219
66
219
66
219
66
220
66
220
66
120
219
66
220
66
220
66
221
66
221
66
221
66
222
67
222
67
222
67
223
67
223
67
223
67
A321
Messier/Goodrich - 03.01.05 - F476021.txt
- After Engine Start
In the case of a false BRAKES HOT alert displayed on the EWD:
  • EMER CANC pbPress
NOTE:
In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION:
The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
"WTRUIB" 2025