operating and cabin crew data 320

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EMERGENCY EQUIPMENT
E. Oxygen Systems

(a) Oxygen Container Location

Refer to Chapter 6.14.1, Figure 14-1 for oxygen container location and number of
masks per container.

(1) Portable Oxygen System

NOTE: Refer to Figure 2-1 above for location and number of portable emergency equip-
ment. Placards show where the equipment is stowed.

There are portable oxygen bottles stowed in various locations in the passenger cabin. The Printed in the Federal Republic of Germany
oxygen bottles are installed in brackets with quick-release clamps.

The bottles are fitted with a transport strap, pressure gauge, pressure regulator valve, shut-off
valve and a ready installed continuous flow mask.
The oxygen flow can be switched to 2 or 4 liters per minute by a knob (flow selector) on top of
the regulator assembly by defined 30° “click stop“ positions. An indication window shows the
selected flow rate. The 4 liter flow is recommended for medical/first aid use.

To use the portable oxygen bottle (handle oxygen bottle with care):
(Ref. Figure 1-2)
• Remove bottle from bracket.
• Remove mask from transport bag.
• Select the desired flow rate by rotating the flow selector knob. In the indication window

below the selector appears the digit “2“ for an oxygen flow of 2 liters per minute or the digit
“4“ for an oxygen flow of 4 liters per minute.
• Place mask over nose and mouth.
• Set shut-off valve to ON by a full turn counterclockwise.
Use transport strap for easy handling if required.

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EMERGENCY EQUIPMENT

Carry Strip

Cylinder

Mask Bag

Swivel Pressure Gauge

Shut-off Valve

Flow Rate
Indicator
Window

Flow Selector

Bayonet Outlet with Swivel Printed in the Federal Republic of Germany

Portable Oxygen Bottle (Example) cLufthansa Technik
Figure 1-2

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EMERGENCY EQUIPMENT
F. Medical Supplies

NOTE: Refer to Figure 2-1 above for location and number of portable emergency equipment.
Placards show where the equipment is stowed.

(1) First Aid Kits (FAK)
The FAK is provided for treatment of minor injuries. A FAK contains bandages, antiseptic
swabs, adhesive tape, arm and leg splints, scissors and ammonia inhalants. The content list is
attached to the case.

6.2.2 Emergency Equipment Cabin Crew Data (OSD)

Instead of two portable ELT devices there is only one portable ELT installed in the aft area of the
cabin.

Printed in the Federal Republic of Germany

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6.3 IN-FLIGHT ENTERTAINMENT (IFE) AND RELATED SYSTEMS / EQUIPMENT
6.3.1 IFE Cabin Crew Information

A. General
The installed Astronics PGA IFE/CMS System offers video and audio distribution throughout the
cabin for passenger convenience.
The system consists of passenger entertainment and cabin management functions.
The cabin is divided into the following zones (Ref. Figure 3-1):

Cabin Zoning Printed in the Federal Republic of Germany
Figure 3-1
cLufthansa Technik
The aircraft is equipped with thirteen (13ea) monitors installed on walls throughout the VVIP, VIP,
and forward wall of the Director Staff Zone, as well as on the forward wall of the Passenger Zone.
The Passenger Zone is also equipped with eight bin-mounted, retractable, 12-inch monitors.

The Video Control Center (VCC) contains four (4ea) Blu-ray players, USB connectors, and HDMI
aux inputs. The VCC is located in the aft left-hand bin.

Four (4ea) aux port panels are installed in the credenzas on the left and right sides of the VIP and
VVIP Zones to provide HDMI inputs for local playback (Ref. Figure 3-2).

The IFE/CMS system is operated from two (2ea) Master Control Panels (MCPs), one (1ea) at D1
LH and one (1ea) at the VCC. Passenger control is from several PCUs installed within each seat
(Ref. Figure 3-3).

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The MCP offers extensive control over the whole system, whereas the fixed mounted PCUs only
provide the following control functionalities:

• One (1ea) headphone jack
• Audio volume adjustment
• Audio channel indication
• Audio channel selection

In the command center and the VVIP and VIP Zones, the PCU offers the following additional con-
trol options:

• Reading light on/off
• PAX call button

The IFE/CMS System is switched on and off with a switch installed at the forward entry area atten-
dant station.

IFE Components
Figure 3-2

IFE Control Interfaces Printed in the Federal Republic of Germany
Figure 3-3
cLufthansa Technik
As part of the IFE/CMS system, the cabin is equipped with ceiling and PSU speakers. In the VVIP
and VIP Zones, the speakers are driven in a stereo configuration, while the rest of the cabin is pro-
vided with mono audio.

For the purpose of passenger call, both the Passenger and Director Staff Zones are each treated
as a complete zone, regardless of the actual seat the call was initiated from.

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6.3.2 IFE Cabin Crew Data (OSD)

A. Safety Instructions

• Required services, such as emergency evacuation and announcements must be addressed
with the Passenger Address (PA) system only.

• In case of an emergency announcement, cabin crew must ensure that all passengers are
aware of the intent and of the announcement itself.

• The Inflight Entertainment Systems must be switched OFF in case the system does not mute
the entertainment overhead speakers during a PA announcement.

NOTE: Any PA overrides and mute the Inflight Entertainment. The priority of the PA
announcements remain unchanged. For details refer to CCOM chapter 05-030 Pas-
senger Address

• The Inflight Entertainment System must be switched OFF in case no passengers are in the
cabin.

• The flight/cabin crew shall not reset the electrical power to the Inflight Entertainment System
where a hazardous fault (e.g. short circuit) is suspected.

• In a decompression event the Inflight Entertainment System will automatically mute the IFE
speakers and turn the cabin monitors off.

B. Activation / Deactivation

The Inflight Entertainment Systems can be enabled/disabled at any time by pressing the PES ON/
OFF switches located at the FWD Entry and in the VCC.

The PES ON/OFF switch will toggle the standby mode for the IFE speakers and video monitors,
CMS functionality will still be available.

NOTE: In case of a suspected hazardous IFE system failure or short circuit, the IFE System Printed in the Federal Republic of Germany
power can only be cut-off by the flight crew by pressing COMMERCIAL pushbutton
switch (22XN) located on overhead panel 35VU.

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C. System Operation
The IFE System can be operated from the FWD Entry and VCC.
Both stations are equipped with switch panel and Master Control Panel (MCP).
(1) PES Switch Panel
GREEN when on

PES ON/OFF Enables/Disables the IFE System
BGM ON/OFF Enables/Disables the Boarding Music (playback from Blu-Ray Player 1)
VOLUME UP/DOWN Adjusts the volume of the Boarding Music

Printed in the Federal Republic of Germany

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(2) Master Control Panel (MCP)

The MCP is a multi-purpose terminal offering the following functions: Printed in the Federal Republic of Germany

Entertainment
• Control of video/audio sources
• Control of video monitors
• Control of Hi-Fi speakers
• Video Briefing
• Control of PFIS (3D Moving Map)

Lighting
• Control of room lighting in VIP Zones

Communication
• SATCOM Status indication
• Telephone Call indication

Power
• Executive Power outlet indication

Cabin Management
• Call indication and reset for VIP Zones

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(3) KTS (Keyboard Touch Screen)

The KTS is available in the following locations:
• Crew Rest Area
• Mission Command Center
• VVIP Zone
• VIP Zone
• Director Staff Zone

Each KTS has one or both of the following functions:
• Lighting Control of the respective Area
• Entertainment Control of the respective Area

D. Video Control Center (VCC)
The VCC is located in the aft LH overhead bin in the Passenger Zone.

Printed in the Federal Republic of Germany

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The VCC is equipped with:
• 4ea Blu-Ray Player (with local control and USB media playback)
• PES Switch Panel
• HDMI Socket (for global video input)
• Master Control Panel (MCP)

Printed in the Federal Republic of Germany

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6.4. IN-SEAT POWER SUPPLY SYSTEM (ISPSS)

6.4.1 ISPSS Cabin Crew Information (Ref. Figure 4-1)

The KID Skypower In-Seat Power Supply System is installed throughout the cabin at each pas-
senger seat to provide electrical 110VAC/60Hz outlets to power PEDs. The only exceptions are
the seat-table arrangements in the VIP/VVIP Zone and the seat in the Mission Command Center,
which are provided with outlets in the credenzas.

The electrical connection is shed in aircraft emergency configuration or via a pushbutton in the for-
ward attendant area. In case of low cabin pressure, the system is deactivated automatically.

ISPSS Component Location
Figure 4-1

6.4.2 Cabin Crew Data (OSD)

A. Safety Instructions

The 110VAC/60HZ electrical power must not be used during critical phases: TAXI, TAKEOFF, and
LANDING.

NOTE: Outlet usage can be monitored by checking the PED Power in-Use Indicator Printed in the Federal Republic of Germany
(PPUI).

WARNING: EACH OUTLET CAN SUPPLY UP TO 150VA. ITEMS CONNECTED TO THE
OUTLET SHOULD BE LIMITED TO PORTABLE ELECTRONIC DEVICES
(PED).

CAUTION: IN CASE A SYSTEM MALFUNCTION OR FAULT IS SUSPECTED - SWITCH cLufthansa Technik
OFF THE ISPSS SYSTEM AND DO NOT ATTEMPT TO RESET THE SYSTEM.

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B. Activation / Deactivation

PED POWER ON/OFF switch (9060ME) located at the FWD Entry
(Combined In-Seat Power Supply and Executive Power System switch)

ISPS OFF/FAULT switch (9054ME) located at the FWD Entry

NOTE: In case of Rapid Decompression, the PSS is disabled automatically.

NOTE: Using the PED POWER ON/OFF switch will also affect the Executive Power Sys-
tem (230V/50Hz).

SYSTEM OPERATION

The 110VAC/60HZ In-Seat Power Supply System consists of:

• PED POWER ON/OFF switch at the FWD Entry
• ISPS OFF/FAULT switch at the FWD Entry (under flap)
• 74ea 110VAC/60Hz Universal Power Outlets
• 28ea PPUI (Power In-Use Indicators)

C. Component Location (Ref. Figure 4-2)

Printed in the Federal Republic of Germany

ISPSS Component Location cLufthansa Technik
Figure 4-2
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Cabin Crew Data

(1) PED Power ON/OFF

Amber: PED POWER is OFF and power is available
Green: PED POWER is ON
Dark/Not illuminated: PED POWER is OFF and no power available

(2) ISPS OFF/Fault Switch

Use the ISPS OFF/FAULT switch to switch OFF the ISPS System manually in case the
Executive Power System should remain functional.
This switch is not illuminated during normal operation.
If pressed a white OFF indication will come on.
An amber FAULT indication is triggered if the ISPS System has detected an internal fault.
In this case power at the 110V outlets can be partly or entirely unavailable. Maintenance
needs to be performed.

(3) Outlet Status Indication
The LED located on each 110V outlet shows the power availability.
LED is GREEN: power is available
LED is RED: power is permanently disabled
LED is OFF: no power or fault

(4) PPUI Indication
The PPUI associated with each outlet is in clear view of the cabin and comes on blue when-
ever a device is connected to an outlet and switched on.

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Cabin Crew Data cLufthansa Technik

6.5 CABIN COMMUNICATION AND NETWORK SYSTEM

6.5.1 Cabin Communication and Network Cabin Crew Information

A. General

The aircraft is equipped with a Cabin Communication System (CCS), using corded and cordless
telephones to initiate VoiP calls. Also wired and wireless networks allow TPED connectivity ser-
vices to connect to the Internet through the existing Ka-Band SATCOM system.

The cabin crew is able to monitor and control the system status and functions at the In-Flight
Entertainment System Video Control Screen. The CCS operation is fully automatic; no further
crew intervention is required for normal system operation.

B. Cabin Network System

The Cabin Network System provides telephony functions and Internet access through the existing
Ka-Band SATCOM system. A wired Ethernet network with cabin LAN ports and Ethernet switches
provides access for passenger laptop computers. Two (2ea) installed wireless access points cre-
ate a wireless network, which can be used by PEDs and wireless telephone units. Wired tele-
phone handsets provides wired IP telephony service. A Cabin Telephony & Data Unit (CTDU)
connects to all systems and functions as the core of the Cabin Network System.

The cabin network system allows flight crews and passengers to:

• Use (T-) PED equipment to connect to a cabin WLAN access point
• Use PED equipment to connect to a cabin LAN port
• Place and receive air-to-ground and ground-to-air voice calls over a satellite link
• Place and receive internal calls including Cockpit calls (seat-to-seat calling)
• Forward calls between handsets
• Conference calls

Internet access and external telephony is provided via the Ka-Band SATCOM System and distrib-
uted via the Cabin Network System.

C. Cabin Network System - Control (Ref. Figure 5-1)

The electrical supply for all Cabin Network System equipment is controlled by the COMMERCIAL
load shedding switch located in the cockpit.

The Cabin Network System is controlled by the CABIN NETWORK ON/OFF switch (1) located in
the door 1L area. System ON/OFF status is indicated by:

• No switch backlighting – No electrical power available for Cabin Network System
• Amber switch backlighting – Cabin Network System switched OFF
• Green switch backlighting – Cabin Network System switched ON

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Cabin Network Controls Printed in the Federal Republic of Germany
Figure 5-1
cLufthansa Technik
The Cabin Network System is OFF (Amber) by default and needs to be activated manually.
In order to provide Internet access to the Cabin Network System, Ka-Band SATCOM must be acti-
vated in the cockpit.

The cabin network system is operated and monitored from the VIP Master Control Panel (MCP)
screen, identified with (2) in the illustration above.

WARNING: USAGE OF MEDICAL EQUIPMENT MIGHT BE AFFECTED BY WIRELESS
SYSTEM COMPONENTS OF THE CABIN COMMUNICATION SYSTEM.

IF WLAN INTERFERENCES TO MEDICAL EQUIPMENT IS DETECTED OR
SUSPECTED, THE WLAN MUST BE SWITCHED OFF.

D. Cabin Network System - Telephone

The cabin telephone system allows flight crews and passengers to:

• Place and receive air-to-ground and ground-to-air voice calls over a Satellite Link
• Place and receive internal calls including Cockpit calls (seat-to-seat calling)
• Forward calls between handsets
• Conference calls

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A total of eleven (11ea) telephones are installed in the following areas (Ref. Figure 5-2):

• COCKPIT
The cockpit has one (1ea) wired handset and cradle installed at the back of the center pedestal.

• MISSION COMMAND CENTER
There is one (1ea) wireless handset and charging cradle located next to the monitor in the Mission
Command Center.

• VVIP ZONE
There is one (1ea) wired handset and cradle located in the LH sideledge (under the flap).

• VIP ZONE
There are two (2ea) wired handsets and cradles located in the LH and RH sideledges (under the
flap).

• DIRECTOR STAFF ZONE
There are two (2ea) wireless handsets and charging cradles located one each on the LH and RH
partition located between the Director Staff Zone and the Passenger Zone.

• PASSENGER ZONE
There are four (4ea) wireless handsets and charging cradles located in this area. One each on the
LH and RH partition located between the Director Staff Zone and the Passenger Zone as well as
one each on the LH and RH Lavatory.

For handset description and operation, refer to Figure 5-3(Sheet 1)

Printed in the Federal Republic of Germany

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Printed in the Federal Republic of Germany

Handset Locations cLufthansa Technik
Figure 5-2
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Printed in the Federal Republic of Germany

Handset Instructions cLufthansa Technik
Figure 5-3 (Sheet 1)
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Printed in the Federal Republic of Germany

Handset Instructions cLufthansa Technik
Figure 5-3 (Sheet 2)
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Incoming phone calls are indicated by means of the following (Ref. Figure 5-4):

• Aural sound at the handset
• Visual indication at the handset
• Visual call indication for phone group on the MCP

Phone Call Indications Printed in the Federal Republic of Germany
Figure 5-4

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E. Cabin Network System - Internet

Internet access is provided via the Ka-Band SATCOM System and distributed via the Cabin Net-
work System. With active Satellite link, the Internet can be accessed by the following means:

Use (T-) PED equipment to connect to a cabin WLAN access point
Use PED equipment to connect to a cabin LAN port (Ref. Figure 5-5)

(1) Access
Wired access to the Cabin Network System can be established via RJ45 Ethernet ports
installed in the following areas:

• MISSION COMMAND CENTER
There are two (2ea) RJ45 Ethernet ports installed in the Mission Command Center.

• VVIP ZONE
There is one (1ea) RJ45 Ethernet port installed in each of the LH and RH sideledges.

• VIP ZONE
There is one (1ea) RJ45 Ethernet port installed in each of the LH and RH sideledges.

• DIRECTOR STAFF ZONE
There are two (2ea) RJ45 Ethernet ports installed at the Director Staff Zone stowage.

(2) Controls and Indications
On the MCP screen, press the Communication button in the menu bar to see the controls
and indications illustrated in Figure 5-6.

Printed in the Federal Republic of Germany

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Printed in the Federal Republic of Germany

Cabin LAN Ports - Location cLufthansa Technik
Figure 5-5
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Printed in the Federal Republic of Germany

Internet Controls and Indications cLufthansa Technik
Figure 5-6
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6.5.2 Cabin Communication and Network System - Cabin Crew Data (OSD)

The Passenger Safety Briefing must include:
• Ensure all cabin telephone handsets are safely stowed in their cradle unit for TTOL. Refer to

chapter 8, “Standard Operating Procedures, Safety-Related Duties: Passenger Safety Brief-
ing.”

For Cabin Crew Safety related duties (refer to OEM CCOM 13-060) consider the following note
and chapter 8.2 of this document.

NOTE: All cabin cordless phones are part of the equipment items, which need to be
stowed. All forward facing cordless phones need to be stowed in foam blocks
located in the last LH aft bin in the Passenger Zone.

Printed in the Federal Republic of Germany

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6.6 WATER AND WASTE SYSTEMS

6.6.1 Water and Waste Systems - Cabin Crew Information

A. Description

The aircraft is equipped with a bleed air pressurized potable water system. Fresh water for the lav-
atories and galleys is provided from two water tanks located in the pressurized under floor area in
the cargo compartments. There is one FWD 200 liters (53 US gal) tank and one additional AFT
200 liter (53 US gal) tank. The water is distributed to the galleys and lavatories via distribution lines
located in the under floor area of the aircraft.

B. Water Quantity Indication

Water quantity is displayed in percentage on the FAP and the AFT service panel.

A water level warning light and buzzer operates when the water level in the potable water tanks is
below 50 liters. Warnings are provided at the mission command center FWD partition. To cancel
the low level warning the water level reset button has to be pushed.

Printed in the Federal Republic of Germany

Water Quantity Indication cLufthansa Technik
Figure 6-1
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C. Potable Water Heater (Ref. Figure 6-2)

Potable water heaters may only be switched on / operated if all supply water lines are filled with
water and vented. To vent potable water lines open faucet of washstand until a continuous flow is
established.

The water heater shut off switch is located at the mission command center FWD partition. This
switch operates all water heaters in the lavatories.

Water heaters have to be switched off prior to draining the potable water system.

Potable Water Heater Printed in the Federal Republic of Germany
Figure 6-2
cLufthansa Technik
6.6.2 Water and Waste Systems - Cabin Crew Data (OSD)

A. Potable Water Supply in VIP Lavatories

In both VIP lavatories, the water supply is controlled by a motorized shut-off valve. The shut-off
valve can be operated in three modes (AUTO/OFF/DRAIN). The mode is selected by a switch
(water shut-off switch). The switches are located inside the washstands beside the waste bin.

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B. Operation and Controls

In normal mode (AUTO), potable water supply for the VIP Lavatories is controlled via an Infra-Red
(IR) sensor. If somebody is detected by local IR sensors, the corresponding potable water room
shut-off valve is opened. After 60 seconds of no detection, the valves are closed automatically.

It is possible to permanently close the local potable water room shut-off valves via override
switches located in the washstands. To get access to the switches, open the washstand door
below the sink.

The OPEN mode of the potable water room shut-off valves at the water shut-off switch (Forward
VIP Lavatory: 9026MB; Aft VIP Lavatory: 9027MB) shall be used only during a draining procedure
on the ground or if the IR sensor fails to open the valve in AUTO mode. OPEN mode permanently
opens the valves independently from the IR sensor.

MODE RESULT
AUTO (Standard Position) Local PW shut-off valve is opened as IR sensor detects somebody
Local PW shut-off valve is closed after 60s of no detection
OFF
DRAIN Local PW shut-off valve is closed

Local PW shut-off valve is permanently open

Printed in the Federal Republic of Germany

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6.7 CABIN LIGHTING SYSTEM
6.7.1 Cabin Lighting System - Cabin Crew Information

A. STANDARD CABIN

GENERAL INFORMATION ABOUT STANDARD CABIN LIGHTING

The standard cabin lighting provides light in the:

• Cabin Zones Director Staff Area (DS) and the Passenger Zone (PZ)
• AFT Entry Area.

The cabin crew can control and monitor the cabin lighting via the following control panels:

• Flight Attendant Panel (FAP)
• Additional Attendant Panel (AAP).

For information about the cabin lighting control panels:
• Refer to CCOM Chapter 06-030-010-30-10 FAP CABIN LIGHTING Page Functions or
• Refer to CCOM Chapter 06-030-010-30-20 Cabin Lighting Control via AAP.

For information about general aspects of the cabin lighting control: Refer to CCOM Chapter 06-
030-010-10 General Aspects of Cabin Lighting Control.

NOTE: The FWD entry and the VIP Cabin are controlled via the VIP CMS System, refer
to 6.7.1 B. General Information about VIP Cabin Lighting, herein.

GENERAL INFORMATION ABOUT READING LIGHTS Printed in the Federal Republic of Germany

Reading lights in the Director Staff Area (DS) and the Passenger Zone (PZ) are part of the Pas- cLufthansa Technik
senger Service Unit (PSU).

In the VIP Cabin the reading lights are controlled via the VIP CMS System. Refer to 6.7.1 B. Gen-
eral Information about VIP Cabin Lighting, herein.

Each passenger can control the assigned reading light via a pushbutton on the PSU.

In addition, the cabin crew can turn ON/OFF the reading lights:

• In the entire cabin or in individual cabin areas via the controls on the CABIN LIGHTING page
on the FAP. Refer to CCOM Chapter 06-030-010-30-10 General Cabin Settings.

• Individual reading lights via the SEAT SETTINGS page on the FAP. Refer to CCOM Chapter
06-080 SEAT SETTINGS - Reading Lights Settings.

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NOTE: When either button is deselected the passengers can switch the reading light
individually again.

READING LIGHTS CONTROLS VIA THE FAP CABIN LIGHTING PAGE

On the CABIN LIGHTING page the cabin crew can control the reading lights via the R/L SET and
the R/L RESET buttons on the GENERAL CABIN SETTINGS control pad.

NOTE: The R/L SET / R/L RESET buttons do not show the status of the reading lights.
NOTE: The R/L SET / R/L RESET control function is available on ground, only.

B. General Information about VIP Cabin Lighting Printed in the Federal Republic of Germany

The cabin crew can control and monitor the cabin lighting via the following control panels: cLufthansa Technik

VIP Area:
• MCP (Master Control Panel)
• KTS (Keyboard Touch Screen)
• Dedicated Buttons for Light Control in:

• Forward Entry Area
• Work Lights in the Forward Entry
• Forward Galley
• Hallway (in front of the aft VIP lav)

Delegation Area: Refer to CCOM Chapter 06-030-010-10.

For information about the cabin lighting control panels in the VIP Area:
• Refer to 6.3.2 - IN-FLIGHT ENTERTAINMENT SYSTEM subchapter OPERATION

For information about the Delegation Area cabin lighting control panels:
• Refer to CCOM Chapter 06-030-010-30-10 FAP CABIN LIGHTING Page Functions or
• Refer to CCOM Chapter 06-030-010-30-20 Cabin Lighting Control via AAP.

C. Types of Cabin Light

For Information about the lighting in the Delegation Area, refer to CCOM Chapter 06-030-010-10.
The following information are for the VIP Area only.

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EFFECT LIGHTS (MIRROR LIGHTS)
In the VIP lavatories, mirror lights are installed. They automatically turn on once the door is
locked.

DECOR LIGHTS
Decor lights are installed under the IFE monitors in the VVIP and VIP Zones.

WORK LIGHTS
Work lights are installed in the forward entry and are usually controlled via the OEM push-
buttons in between the seats. The work lights are integrated in the IFE/CMS.

STOWAGE LIGHTS
The stowage lights automatically turn on and illuminate the stowage compartment when the
door is opened. Movement is detected using a Passive Infrared Sensor (PIR), which only
functions when not blocked by an obstacle.

TABLE LIGHTS
Table lights are installed in the VIP Area above tables and illuminate the tables’ surface.
Control is done via the MCP or KTS.

READING LIGHTS
Reading lights are installed in the VIP area above seats and illuminate the seat area. Con-
trol is done via the MCP/KTS or pushbuttons in the seats’ armrest or pushbuttons in front of
the seat.

D. Definition of Cabin Lighting Areas

FWD ENTRY AREA
The lights in the forward entry area are controlled via the IFE/CMS system.

VIP AREA
The lights in the VIP area are controlled via the IFE/CMS System.

E. Individually Controlled Lights

All lights in the VIP area are controlled via the IFE/CMS and most controls are done with the help
of lighting scenes. Stowage lights (PIR sensor) and the lights in the VIP lavatories (Door Lock) are
automatically controlled.

The reading lights can be controlled via the PCUs installed in the arm rest, or via pushbuttons in
front of the seat. Additionally, the reading lights can be controlled via MCP/KTS.

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F. Cabin Lighting and Reading Lights (Ref. Figure 7-1 and Figure 7-2)
In the Passenger Zone, existing ceiling and side wall wash lights and PSU reading lights are mod-
ified to suit the new layout.
In the VIP cabin, the lighting is controlled by the IFE CMS. All lights in the Director Staff, Forward
Passenger, Aft Passenger and Aft Entry Area are controlled via the OEM installed Flight Attendant
Panel.

G. Emergency Lighting System (Ref. Figure 7-3 and Figure 7-4)
In the cabin, exit signs, emergency area lights and electrical floor path markers are installed.

Cabin Lighting Zones
Figure 7-1

VIP Zone Lighting Printed in the Federal Republic of Germany
Figure 7-2

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Emergency Lighting - Area Lights
Figure 7-3

Emergency Lighting - FPM System Printed in the Federal Republic of Germany
Figure 7-4
cLufthansa Technik
6.7.2 Cabin Lighting System - Cabin Crew Data (OSD)

A. General Information about Cabin Lighting Control in the VIP Area

In the VIP Area a supplementary Cabin Management System (CMS - which is part of the VIP
Inflight Entertainment System) is installed. The entire control of the general light in the VIP Area
and FWD Entry is integrated in the CMS.

From the Main Lighting Page on the Master Control Panel (MCP) all lights in the VIP Area can be
controlled at once. Via Zone Pages each zone can be controlled separately from the others.

Additionally light scenes are implemented to give easy access to predefined scenarios for the
whole area or individual zones. Local control can by done via the Keyboard Touch Screen (KTS)
installed in the zone.

The following interfaces to the OEM CMS (CIDS) are installed:
• The Main On/Off from the FAP/AAP also controls the VIP Area
• The Cockpit Door Dimming logic is transferred to the IFE/CMS and the Spot lights in the FWD

Entrance are dimmed correspondingly.

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B. Operation and Controls (Ref. Figure 7-5)

All controls of general lighting in the VIP cabin are available via the Master Control Panel (MCP)
installed in the forward entry and in the VCC. Additional Keyboard Touch Screens (KTS) are
installed in each area and allow control of the associated area.

Reading Lights are controlled via pushbuttons in the arm rests or in a wall in front of the passenger
seat. In the forward entry, forward galley, and hallway, additional pushbuttons allow direct control
of the corresponding lights.

Operation and Controls Printed in the Federal Republic of Germany
Figure 7-5
NOTE: cLufthansa Technik
For information about the cabin lighting control via MCP and KTS in the VIP area,
see 6.3.2 IFE Cabin Crew Data (OSD).

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Cabin Crew Data

6.8 EXECUTIVE POWER SYSTEM

6.8.1 Executive Power System - Cabin Crew Information

A. No additional Cabin Crew Information is introduced.

6.8.2 Executive Power System - Cabin Crew Data (OSD)

A. General
The aircraft is equipped with an Executive Power System (EPS). The EPS comprises of two (2)
power converters and nine (9) power outlets installed throughout the whole cabin providing 230V
AC/ 50Hz electrical power for the use of passengers Portable Electronic Devices (PEDs).

CAUTION: ANY USAGE OF PORTABLE ELECTRONIC DEVICES SHOULD BE COORDI-
NATED AND CONTROLLED BY THE CABIN CREW TO AVOID ANY EFFECTS
TO THE AIRCRAFT SYSTEMS.

All power outlets provide protection features that prevent electrical shocks that could occur, if the
outlet is not used correctly (e.g. inserting foreign objects into the outlet). It also has integrated sen-
sors to release power only when a plug is engaged.

For the outlets installed in hidden areas, an additional in-use light provides visual information of
current in-use status of the outlets.

B. Location (Ref. Figure 8-1)

The EPS outlets are located at following positions:
• 1ea in the FWD Galley (G1)
• 1ea in the Mission Command Center (MC), associated in-use light is located outside of MC
on entry frame
• 1ea in the FWD VIP LAV (VL1)
• 1ea in the VVIP zone (VV)
• 1ea in the VIP zone (VZ)
• 1ea in the AFT VIP LAV (VL2)
• 1ea in the AFT LH DS-Stowage, associated in-use light is located outside on stowage
header.
• 1ea in the Passenger Zone (PZ)
• 1ea in the AFT Galley (G5)

Control devices and status indications are installed in the FWD entry area on the Mission Com-
mand Center Wall at door 1L.

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EPS System Outlets
Figure 8-1

C. Description and Operation

The cabin crew can control and operate the EPS system any time by using one of the following
pushbuttons:

PED POWER ON/OFF switch (Ref. Figure 8-2)

It is possible to simultaneously disconnect power from all EPS outlets (together with the In-
Seat Power Supply System (ISPSS)) via the PED POWER pushbutton located in the FWD
entry area on the Mission Command Center Wall at door 1L.

Switch status: The switch illuminates amber if the system is OFF and green if the system is
switched to ON.

NOTE: After power up the switch is always in OFF

PED POWER ON/OFF Switch - D1L Aft Wall Printed in the Federal Republic of Germany
Figure 8-2
cLufthansa Technik
EPS Converter Control Pushbutton Switch (Ref. Figure 8-3)
It is possible to disconnect power from each EPS converter independently via pushbuttons
located in the forward entry area on the Mission Command Center wall at door 1L.

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EPS Converter Control Pushbutton Switch - D1L Aft Wall Printed in the Federal Republic of Germany
Figure 8-3
cLufthansa Technik
Converter 1 (2) LEFT pushbutton:

• AVAIL The green AVAIL light comes on if the PED POWER pushbutton located on the same
wall is enabled.

• ON The white ON light comes on if the system is powered (green AVAIL light is still active).

Converter 1 (2) RIGHT pushbutton:

• FAULT The amber light comes on, when the frequency converter fails.
• PUSH TO RESET The white light comes on, when the frequency converter fails. The pushbut-

ton can be pressed to reset the converter.

Refer to following chapter for converter malfunction/ fault reset options.

The entire system will be automatically switched OFF during cabin decompression.

D. Power Outlet (Ref. Figure 8-4)

The power outlets are multi socket type outlets and they are equipped with various safety func-
tions like Ground Fault Interrupters (GFI), mechanical child protection and plug detection and
overload protection.

The power outlets are limited to a maximum of 7A. A label on the outlet indicates the power limit of
“230V 50Hz / 1,61kW / 7A”.

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Power Outlet
Figure 8-4

E. Converter Malfunction / Fault Reset Option

In case of an EPS converter fault the affected converter automatically kept in OFF status and the
amber FAULT indication is active at related control switch.

Perform the following fault-reset sequence to reset/ reactivate the affected converter:

NOTE: Before reset procedure start, disconnect all PEDs from the power outlets.

1. Stage of EPS converter reset:

• press and release the PUSH TO RESET SWITCH Printed in the Federal Republic of Germany
• wait for 10 seconds

In most cases the converter should have been returned to normal operation now (amber FAULT
indication light is OFF).

If the FAULT indication still persists perform the following:

2. Stage of EPS converter reset:

• switch the converter OFF (using the AVAIL/ ON pb-sw) cLufthansa Technik
• wait for 10 seconds
• switch the converter ON again (using the AVAIL/ ON pb-sw)
• wait for 10 seconds

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NOTE: For safety reasons it is allowed to perform the 2nd stage of converter reset only
ONE time.

If the FAULT indication still persist after performing both stages of EPS converter reset, the
affected converter has to remain deactivated (set AVAIL/ ON pb-sw to OFF position) and further
maintenance is required.

If a defective PED has been identified to be the reason for a system fault – do not use this PED on
other power outlets.

F. Operational Limitation

Use of the Executive Power System (EPS) for Portable Electronic Devices (PED, carried by the
passengers) is not authorized in the following flight phases: Taxi, Takeoff, Landing.

Printed in the Federal Republic of Germany

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6.9 SUPPLEMENTAL MEDICAL EQUIPMENT
6.9.1 Supplemental Medical Equipment - Cabin Crew Information

A. No additional Cabin Crew Information is introduced.
6.9.2 Supplemental Equipment - Cabin Crew Data (OSD)

A. Location (Ref. Figure 9-1)

The medical PSU is installed under the AFT LH overhead stowage compartment (OHSC) above
seat 17 A/B/C.

B. General Description

On the medical PSU, a 28VDC power outlet and an 115VAC power outlet are installed. They are
supplied via circuit breakers on panel 2001VU.

The 28VDC power outlet is a 2-pin type socket. A label on the outlet indicates the power limit of
28VDC/420W MAXI.

The 115VAC power outlet is a 3-pin type socket. A label on the outlet indicates the power limit of
115VAC/1150VA MAXI.

The medical PSU has a protective flap to prohibit passenger access.

WARNING: THE MEDICAL POWER OUTLETS WILL BE SWITCHED OFF IN CASE OF
LOAD SHED. DO NOT USE FOR LIFE SUPPORT DEVICES WITHOUT INTER-
NAL BACKUP POWER.

LH PASSENGER ZONE Printed in the Federal Republic of Germany

FLAP CLOSED FLAP OPEN cLufthansa Technik

Medical Outlets
Figure 9-1

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6.10 SMOKE DETECTION SYSTEM
6.10.1 Smoke Detection System - Cabin Crew Information

A. No additional Cabin Crew Information is introduced.
6.10.2 Smoke Detection System - Cabin Crew Data (OSD)

A. Location (Ref. Figure 10-1)
• Smoke detectors are installed in the lavatories, and cabinets.
• The location of the smoke detectors is indicated on the SMOKE DETECTION page on the FAP.
• The ambient smoke detectors of the standard lavatories (Lav A, Lav D and Lav E) are typically
installed in the ceiling.
• The duct type smoke detectors are connected via sniffing points to each VIP lavatory (VL1 and
VL2).
• The duct type smoke detector is connected via sniffing points to the DS-Stowage (FWD and
AFT partition).

Monitored Lavatories and Stowages
Figure 10-1

B. Operation
The duct smoke detectors rely on airflow through the Galley / Lavatory Ventilation system. These
smoke detectors are in-operative when the Galley / Lavatory Ventilation system fails or in case of
a duct connection fault. (Ref. Table 10-1)

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Room / Compartment AIP Indication Connection Type
VIP lavatory (VL1) SMOKE_F-LAV Connected via sniffing point in
the ceiling.
VIP lavatory (VL 2) SMOKE_M-LAV
Connected via sniffing point in
FWD DS-Stowage SMOKE_DS-STOWAGE the ceiling.
AFT DS-Stowage
Connected via sniffing points in
a tube, mounted inside of the
stowage.

List of Duct Smoke Detectors Connected to the Galley / Lavatory Ventilation System
Table 10-1

A pressure switch is linked to the Cabin Intercommunication Data System (CIDS), which controls
the smoke detection fan fault indications via its control and indication panels in the cabin:
• Additional Indication Panel (AIP)
• PA Speaker

C. Smoke Fan Fault Indication

If a fan fault is detected there are:

(1) Aural Warnings
The aural warning is a quad chime sequence with 3 repeats. The chime is distributed in the
cabin via all passenger and cabin attendant station loudspeakers:

(2) Visual Warnings
On the AIPs the clear wording SMOKE FAN FAULT is indicated. The red indicator comes
ON steady.

D. Smoke Fan Fault Procedures

If a SMOKE FAN FAULT is detected, do the following procedure:

(1) VIP Lavatory (VL1) EMPTY Printed in the Federal Republic of Germany
EMPTY
Waste Receptacle CLOSED / LOCKED
Stowages LABEL “INOPERATIVE - DO NOT USE”
Room Door CHECK EVERY 10 MINUTES
Room Door PERMANENTLY
Absence of Smoke, or
Monitor Room

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(2) VIP Lavatory (VL2) EMPTY
EMPTY
Waste Receptacle CLOSED / LOCKED
Stowages LABEL “INOPERATIVE - DO NOT USE”
Room Door CHECK EVERY 10 MINUTES
Room Door PERMANENTLY
Absence of Smoke, or
Monitor Room

(3) DS-Stowage (FWD & AFT)

Stowages EMPTY

Cabinet Doors CLOSED AND LOCKED

Cabinet Doors LABEL “INOPERATIVE - DO NOT USE”

Frequency Converter 2 OFF

Refer to 6.8.1 Executive Power System - Cabin Crew Information

Printed in the Federal Republic of Germany

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6.11 CABIN MANAGEMENT SYSTEM

6.11.1 Cabin Management System - Cabin Crew Information

A. ATTENDANT INDICATION PANEL (AIP)

DESCRIPTION OF THE ATTENDANT INDICATION PANEL (AIP)

The Attendant Indication Panels (AIPs) are LCD screens that display messages associated with
all of the following:

• Passenger Call
• Evacuation Signaling
• Smoke Detection
• Smoke FAN FAULT indication
• Passenger Address
• Prerecorded Announcements
• Interphone
• Water/Waste
• ECAS

The AIPs consist of a two-row alphanumerical display and two indicator lights.

The upper row displays communication information (e.g. interphone calls) and the lower displays
system and emergency information (e.g. direct announcements). Each one has a length of 16
characters.

The two indicator lights (red/green) serve as attention getters. The red light is used for system and
emergency information, the green light for communication information.

The AIPs are located near all cabin crew stations, and in the galleys.

Attendant Indication Panel Printed in the Federal Republic of Germany
Figure 11-1
cLufthansa Technik
PASSENGER ADDRESS AND INTERPHONE INDICATIONS

During the dial procedure, the dial information is displayed in the upper row of the respective
Attendant Indication Panel (AIP).

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Example: Do the PA ALL function using the dual dial handset.

STEP ACTION RESULT RESULT
(on the handset)
(on calling AIP) (on all other AIPs)

1 Hook off the handset # (flashing) (no result)

2 Press the PA key # # (flashing) (no result)

3 Press the ALL key PA ALL (no result)

4 Press PTT and start the announcement > PA ALL (no result)

In addition, the following handset operation related messages could appear in the upper row of the
calling AIP while the dialing procedure:

INFORMATION EXPLANATION
BUSY Called station is engaged
CNCL Communication is interrupted by a call with a higher priority
OVER Station is connected to a call with a higher priority
ERR A wrong code has been dialed
RST Reset push button is pressed
WAIT PA CALL Passenger Address system is already in use

If the dial procedure is finished the respective status information is indicated on all assigned AIPs. Printed in the Federal Republic of Germany

To raise the attention for communication information, a chime is heard and the green AIP indicator cLufthansa Technik
light comes on additionally. This light is located on the right side of the AIP.

B. PASSENGER SERVICE UNIT (PSU)

LOUDSPEAKERS

Loudspeakers are located in all of the following areas:

• In the Passenger Service Units (PSUs)
• In the cabin crew stations
• In the galley ceilings
• In the lavatories
• In the VIP area ceilings.

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C. PASSENGER SIGNS

There are several signs in the cabin and in dedicated areas (e.g. in the lavatories).

The signs are controlled either by the flight crew or automatically in specific conditions (e.g. landing
gear up/down). Loudspeakers are located in all of the following areas:

THE PASSENGER SIGNS

Passenger Signs can be installed on both of the following:

• The Passenger Service Unit (PSU) above passenger seats
• The Closure Panel beside passenger seats in the VIP area (as standalone equipment)
• Door areas, and galleys (as standalone equipment).

The information on the Passenger Signs is customized and can contain the following signs:

• Fasten Seat Belts (FSB)
• No Smoking (NS).

Examples of Passenger Signs:

Depending on cabin requirements of the operators, other signs can be available in the cabin (e.g. Printed in the Federal Republic of Germany
No PED or No Mobile signs).

THE RETURN TO SEAT (RTS) SIGNS

The Return to Seat sign is located in the lavatories and comes on during takeoff, landing, or
turbulence. The function of the RTS sign is linked to the FSB sign.

Examples of Return to Seat Signs:

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D. VISUAL AND AURAL ALERTS

VISUAL AND AURAL INDICATIONS

Event Visual Indication on the AIP Aural Indication
(Chime or Announcement)
Smoke Fan Fault Red Light,
SMOKE_ FAN_FAULT indication Quad chime, 3 times

E. CABIN INTERPHONE

NOTE: For general information and operation of the hand set refer to CCOM capter 05-015
Handset.

OPERATION: INTERPHONE CALLS FROM THE CABIN

HOW TO INITIATE INTERPHONE CALLS

The following table shows the sequences of keys that must be pressed on the handset in order to
establish a call:

Function Key Sequence Connection --> To
EMER CALL to Cockpit * EMER CALL Handset --> Boomset in the cockpit
Interphone Call to All INTPH + ALL Handset --> All handsets in the cabin
Cockpit Call CAPT Handset --> Handset in the cockpit
Forward Attendant Call INTPH + 1/FWD Handset --> Handsets at attendant stations 1L
Aft Attendant Call (RH) INTPH + 2/MID Handset --> Handsets at attendant stations 4R
Aft Attendant Call (LH) INTPH + 3/EXIT Handset --> Handsets at attendant stations 4L
Aft Attendant Call (RH+LH) INTPH + 4/AFT Handset --> Handsets at attendant stations 4L + 4R

* The EMER CALL call initiates an emergency call from cabin to cockpit only. Printed in the Federal Republic of Germany

HOW TO INITIATE INTERPHONE CALLS

When the handset is in the cradle When the handset is NOT in the cradle

Pick up the handset to establish the commu- It will sound as engaged.
nication. Note: The communication is established,

ongoing calls are overridden. cLufthansa Technik
No action is required to answer an
EMER call.

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INDICATIONS ON THE ATTENDANT INDICATION PANEL

During the dial procedure, the dial information is displayed on the respective Attendant Indication
Panel (AIP) (Refer to Attendant Indication Panel).
If the dialing procedure is finished, the respective status information is indicated on all assigned
AIPs. To raise the attention for communication information, a (customizable) HIGH chime is heard
and the red AIP indicator light comes on additionally.

HOW TO REJECT INTERPHONE CALLS

On the handset press the RESET key.

A selected call from the cockpit is cancelled, when all requested stations have reset the function
on the handset through pushing the Reset button.

The call function is automatically reset after a time period of 5 min, if no requested handset
accepts the call.

NOTE: If a cabin crewmember resets a current EMER call, they must press the EMER
key on the handset to enter again the call.

HOW TO END INTERPHONE CALLS

On the handset press the RESET key.

NOTE: For a Conference call, there are two methods to end a call:

1) The cabin crew who accepted the conference call can press the RESET key,
or

2) The cabin crew who initiated the conference call resets the call via the
RESET key on their handset.

F. PASSENGER ADDRESS Printed in the Federal Republic of Germany
OPERATION: PASSENGER ADDRESS FROM THE CABIN
The cabin crew must use a handset to perform a Passenger Address announcement.
Further information about the operation of the handsets: Refer to Operation of the Handsets.

HOW TO INITIATE A PASSENGER ADDRESS FROM A HANDSET cLufthansa Technik
The handset must first be in the standby mode (ready to use), in order to initiate a PA.

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The following table shows the sequences of keys that must be pressed on the handset in order to
establish a call:

Function Key Sequence Connection (From --> To)
Direct PA PTT Handset --> All loudspeakers
PA ALL PA + ALL + PTT Handset --> All loudspeakers in the cabin (PA1 + PA2 + PA3)
PA 1 PA + 1/FWD + PTT Handset --> All loudspeakers in the Lav A, CA and MC
PA 2 PA + 2/MID + PTT Handset --> All loudspeakers in the VL1, VV, VZ and VL2
PA 3 PA + 3/AFT + PT Handset --> All loudspeakers in the DS, PZ, Lav D and Lav E

PASSENGER ADDRESS INDICATIONS ON THE ATTENDANT INDICATION PANEL Printed in the Federal Republic of Germany

During the dial procedure, the dial information is displayed in the upper row of the respective
Attendant Indication Panel (AIP) (Refer to Attendant Indication Panel).

G. PASSENGER CALL SYSTEM

GENERAL

The VIP area has a dedicated passenger call system based on the In-Flight Entertainment (IFE)
System with interfaces to the OEM Cabin management system to be indicated on the ACP and via
chime.

Calls placed from the VIP areas are indicated and controlled via the Master Control Panels (MCP)
of the IFE System.

In the MISSION COMMAND CENTER, the VVIP ZONE and VIP ZONE, the call buttons are
located in the Passenger Control Units (PCU’s) at each passenger seat location.

In the CREW REST AREA, FWD VIP LAVATORY and MID VIP LAVATORY a dedicated call button
is installed.

VIP CALL INDICATION

VIP calls are indicated on a detailed aircraft layout at the Master Control Panels in FWD

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ENTRANCE and VCC (Video Control Center).

An amber light is displayed on the layout at the seat position when calls placed from the CREW
REST AREA, MISSION COMMAND CENTER, VVIP ZONE, VIP ZONE and VIP lavatories.

Calls from other zones are indicated with a general light on the layout at the respective zone.

To alert the cabin crew when a VIP call has been placed, a chime sounds in the FWD ENTRANCE
area and the call is indicated on the FWD ACP with a blue light.

Call lights are installed outside the VIP lavatories to identify the location of the lavatory call.

NOTE: If more than one call is in progress, the first call light on the layout flashes and
NOTE: additional calls are displayed steady.

The FWD ACP is flashing (blue) when one call active and steady (blue) when
more than one call is in progress.

The Attendant Information Panels (AIP) located at the FWD and AFT entry areas
do not indicate calls from the VIP area except the VIP lavatories.

OPERATION

Printed in the Federal Republic of Germany

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Master Control Panel

VIP calls can be reset from the MCP by pressing the CALL RESET button.
Press the button once to reset the most recent VIP call. When multiple calls are in progress, the
calls will be cancelled in the order they appeared on each button press.
Press and hold the CALL RESET button to reset all of the VIP cabin calls

NOTE: Calls from DIRECTOR/STAFF ZONE and PASSENGER ZONE are managed by
the CIDS and cannot be reset from the MCP.

The chime can be silenced by pressing the NIGHT FLIGHT button on the Master Control Panel
(MCP).

When NIGHT FLIGHT mode is enabled, a VIP call will only appear visually on the MCP and the
chime will not sound.

PCU

The light in call button of the PCU is green when pressed and amber when released. Printed in the Federal Republic of Germany
An active VIP call can be reset by pressing the respective call button on the PCU.
cLufthansa Technik
ADDITIONAL INFORMATION
The VIP cabin is equipped with a VIP Cabin Management System (VCMS) as described above.
All lavatory calls will be indicated in the Cabin Intercommunication Data System (CIDS) and the

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