DOC AIRBUS | MMEL ITEMS A320FThrust Reverser
| 78-30-01 | Thrust Reverser |
|---|
Applicable to: -
78-30-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 0 | Yes |
(o)(m)
1)
2)
3)
4)
One or both may be inoperative provided that:
1)
The inoperative thrust reverser is deactivated
and secured in the stowed position, and
2)
All stow and deploy switches circuits
on the inoperative thrust reverser are checked operative, and
3)
The ENG 1(2) REV PRESSURIZED alert is not displayed on the EWD after deactivation, and
4)
The appropriate performance
adjustments are applied.
| 78-30-01 | Thrust Reverser |
|---|
Applicable to: -
78-30-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 0 | Yes |
(o)(m)
1)
2)
3)
4)
One or both may be inoperative provided that:
1)
The inoperative reverser is deactivated and secured in the stowed
position, and
2)
Both LVDTs on the inoperative
reverser are checked operative, and
3)
The ENG 1(2) REV PRESSURIZED alert is not displayed on the EWD after deactivation,
and
4)
The appropriate performance
adjustments are applied.
| 78-30-01 | Thrust Reverser |
|---|
Applicable to: -
78-30-01-A
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | 2 | 0 | Yes |
(o)(m)
1)
2)
3)
4)
One or both may be inoperative provided that:
1)
The inoperative thrust reverser is deactivated and secured in the
stowed position, and
2)
The ENG 1(2) REV INHIBITED alert is displayed on the EWD after deactivation,
and
3)
The ENG 1(2) REV UNLOCKED alert and the ENG 1(2) REV PRESSURIZED alert associated with the inoperative thrust reverser
are not displayed on the EWD after deactivation,
and
4)
The appropriate performance
adjustments are applied.
+ Reference