25-18 COCKPIT ADDITIONAL ELECTRICAL SUPPLY
- PB.001 COCKPIT ADDITIONAL ELECTRICAL SUPPLY - DESCRIPTION AND OPERATION
- PB.401 COCKPIT ADDITIONAL ELECTRICAL SUPPLY - DEACTIVATION/REACTIVATION
-
25-18-00-040-802-A
[10]
Deactivation of the Additional Cockpit Electrical Supply System -
25-18-00-440-802-A
[10]
Reactivation of the Additional Cockpit Electrical Supply System
-
25-18-00-040-802-A
[10]
- PB.401 POWER OUTLET UNIT - REMOVAL/INSTALLATION
-
25-18-11-000-801-A
[10]
Removal of the Power Outlet Unit -
25-18-11-400-801-A
[10]
Installation of the Power Outlet Unit
-
25-18-11-000-801-A
[10]
- PB.401 USB POWER OUTLET - REMOVAL/INSTALLATION
-
25-18-12-000-801-A
[10]
Removal of the USB Converter of the Personal Tablet -
25-18-12-400-801-A
[10]
Installation of the USB Converter of the Personal Tablet
-
25-18-12-000-801-A
[10]
- PB.401 STATIC INVERTER - REMOVAL/INSTALLATION
-
25-18-51-000-001-A
[10]
Removal of the Static Inverter -
25-18-51-400-001-A
[10]
Installation of the Static Inverter
-
25-18-51-000-001-A
[10]