DOC AIRBUS | MMEL ITEMS A320FAC Main Generation (IDG, GCU, Line Contactor)
| 24-22-01 | AC Main Generation (IDG, GCU, Line Contactor) |
|---|
Applicable to: -
24-22-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 1 | Yes |
(o)(m)
1)
2)
3)
4)
5)
6)
7)
8)
One may be inoperative provided that:
1)
ETOPS is not conducted, and
2)
The flight altitude is limited to 33500 ft, and
3)
The APU and AC auxiliary generation are operative
and used throughout the flight, and
4)
The APU fuel pump is operative, and
5)
The APU oil quantity is checked
to be adequate before each flight, and
6)
All busses have power, and
7)
The indications and alerts for the remaining AC main generation and the AC auxiliary generation
are operative, and
8)
The galley automatic load shed system is checked operative.
| 24-22-01 | AC Main Generation (IDG, GCU, Line Contactor) |
|---|
Applicable to: -
24-22-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 1 | Yes |
(o)(m)
1)
2)
3)
4)
5)
6)
7)
8)
9)
10)
11)
One may be inoperative provided that:
1)
ETOPS is not conducted, and
2)
The flight altitude is limited to 33500 ft, and
3)
The APU and AC auxiliary generation are operative
and used throughout the flight, and
4)
The APU fuel pump is operative, and
5)
The APU oil quantity is checked
to be adequate before each flight, and
6)
The fuel recirculation system associated
with the operative IDG is checked operative before each
flight, and
7)
All busses have power, and
8)
The indications and alerts for the remaining AC main generation
and the AC auxiliary generation are operative, and
9)
The galley automatic load shed system is checked operative.
10)
If the associated IDG is disconnected, the inner/wing tank fuel temperature
on the affected side is checked to be above -30 °C before takeoff.
11)
If the associated IDG is disconnected, the inner/wing tank fuel temperature
on the affected side is monitored in flight and checked to be above -43 °C.
| 24-22-01 | AC Main Generation (IDG, GCU, Line Contactor) |
|---|
Applicable to: -
24-22-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 1 | Yes |
(o)(m)
1)
2)
3)
4)
5)
6)
7)
8)
9)
10)
One may be inoperative provided that:
1)
ETOPS is not conducted, and
2)
The flight altitude is limited to 33500 ft, and
3)
The APU and AC auxiliary generation are operative
and used throughout the flight, and
4)
The APU fuel pump is operative, and
5)
The APU oil quantity is checked
to be adequate before each flight, and
6)
The bypass valves of the IDG heat exchangers of the remaining AC main generation are checked operative before each flight,
and
7)
All busses have power, and
8)
The indications and alerts for the remaining AC main generation
and the AC auxiliary generation are operative, and
9)
The galley automatic load shed system
is checked operative, and
10)
If the associated IDG is disconnected,
the wing tank fuel temperature on the affected side is checked to
be above –39 °C before engine start.
| 24-22-01 | AC Main Generation (IDG, GCU, Line Contactor) |
|---|
Applicable to: -
24-22-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 1 | Yes |
(o)(m)
1)
2)
3)
4)
5)
6)
7)
8)
9)
10)
11)
One may be inoperative provided that:
1)
ETOPS is not conducted, and
2)
The flight altitude is limited to 33500 ft, and
3)
The APU and AC auxiliary generation are operative
and used throughout the flight, and
4)
The APU fuel pump is operative, and
5)
The APU oil quantity is checked to be adequate before
each flight, and
6)
The bypass valves of the IDG heat exchangers of the remaining AC main generation are checked operative before each flight,
and
7)
All busses have power, and
8)
The indications and alerts for the remaining AC main generation
and the AC auxiliary generation are operative, and
9)
The galley automatic load shed system is checked operative, and
10)
If the associated IDG is disconnected,
the wing tank fuel temperature on the affected side is checked to
be above -30 °C before take-off.
11)
If the associated IDG is disconnected, the wing tank fuel
temperature is monitored in flight and checked to be at or above -38 °C.