Floor Proximity Emergency Escape Path Marking System
| 33-51-05 | Floor Proximity Emergency Escape Path Marking System |
|---|
Applicable to: -
33-51-05-A Aircraft equipped with Photo Luminescent Floor Path Marking
System
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | - | - | No |
May be inoperative or missing provided that:
1)
The length of each affected section does not exceed 0.5 m, and
2)
The affected sections are not opposite each other, and
3)
The distance between each affected section is more than 2 m, and
4)
No more than two sections per cabin zone are affected, and
5)
The sections marking right angle intersections, including cross-aisles
and overwing exits, are operative, and
6)
All sections within one meter of the strips marking right angle intersections
are operative.
33-51-05-C Aircraft equipped with incandescent, electroluminescent, or
LED Floor Path Marking System
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | - | - | No |
One or more may be inoperative in accordance with Airbus vertical
separation analysis produced for the specific original aircraft cabin
layout.
| 33-51-05 | Floor Proximity Emergency Escape Path Marking System |
|---|
Applicable to: -
33-51-05-B Aircraft equipped with Photo Luminescent Floor Path Marking
System
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | - | - | No |
May be inoperative or missing provided that:
1)
The length of each affected section does not exceed 0.5 m, and
2)
The affected sections are not opposite each other, and
3)
The distance between each affected section is more than 2 m, and
4)
No more than two sections per cabin zone are affected, and
5)
The sections marking right angle intersections, including cross-aisles,
are operative, and
6)
All sections within one meter of the strips marking right angle intersections
are operative.
33-51-05-C Aircraft equipped with incandescent, electroluminescent, or
LED Floor Path Marking System
| Repair interval | Nbr installed | Nbr required | Placard |
|---|---|---|---|
| C 13.04.2026 | - | - | No |
One or more may be inoperative in accordance with Airbus vertical
separation analysis produced for the specific original aircraft cabin
layout.