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Flyadeal Training > 12 > Flashcards

12 Flashcards

1
Q

It is a short to medium range, single aisle subsonic transport aircraft and is accepted as being one of the most technically advanced aircraft in the world.

A

A320

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2
Q

Hydraulically active systems are linked by means of an electrical pulse generated by a computer instead of the normal mechanical linkages.

A

Three cargo compartments are installed under the cabin floor

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3
Q

The aircraft is equipped with two high by-pass turbo fan engines mounted under the wings.

A

The APU is mounted in the tail and operates both on the ground and in the air.

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4
Q

The electrical power system consists of a three phase __ AC system and a __.

A

105/200V 400 Hz constant frequency

28V DC system

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5
Q

Electrical transients are acceptable for equipment.
Commercial supply has secondary priority.

A

Normally, the system produces AC current, which is then transformed into DC current. Each generator can supply the whole network.

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6
Q

In case of loss of normal AC generation, an emergency generator can supply the aircraft.

A

In case of total loss of AC generation, the aircraft can be supplied from the batteries. In this case, DC current can be transformed into AC current.

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7
Q

The air conditioning system operation is fully automatic. It provides a continual renewal of air and maintains a constant selected temperature in the three following zones: ___ which are independently controlled.

A

Cockpit, FWD Cabin and AFT Cabin,

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8
Q

In normal operation, pressurization control is fully automatic. The system consists of:

A
  1. 2 Cabin Pressure controllers
  2. 1 outflow valve with actuator including 3 motors (2 auto, 1 main)
  3. 1 control panel
  4. 2 safety valves
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9
Q

Three cargo compartments are installed in the A320’s lower deck - __

A

the FWD, AFT and the Bulk cargo compartments.

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10
Q

__are designed to carry containers and pallets.

A

The forward and aft cargo compartments

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11
Q

There are three cargo compartments doors on the ___.

A

lower right side of the fuselage, below the cabin floor

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12
Q

The FWD and AFT cargo doors open ___and can only be opened from the ___ They are hydraulically operated and mechanically locked.

A

outward and upward

outside

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13
Q

The landing gear consists of:

A
  1. two inboard retracting main gears
  2. a forward retracting nose gear.
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14
Q

__enclose the landing gear bays.

A

Gear doors

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15
Q

They are electrically controlled and hydraulically operated.

A

Gears and doors

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16
Q

They are fitted to the landing struts are mechanically operated by the gear and close at the end of gear retraction.

A

The doors

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17
Q

All gear doors open during ___.

A

landing gear transit

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18
Q

A ___ is provided on the center pedestal for L/G gravity extension in case of hydraulic or electrical power supply failure.

A

hand crank

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19
Q

Each __ is a twin wheel gear incorporating an oleo pneumatic shock absorber.

A

Main Gear

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20
Q

Each ___ is fitted with anti-skid brakes.

A

main wheel

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21
Q

The two-wheel __comprises an oleo pneumatic shock strut and a nose wheel
steering system. It retracts forwards into the fuselage

A

nose gear

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22
Q

It was designed and certificated to render the new generation of aircraft safer, more cost effective, and more pleasant to fly, or ride in, than a conventional aircraft.

A

fly-by-wire control system

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23
Q

All flight control surfaces are:

A
  1. Electrically controlled,
  2. Hydraulically activated.
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24
Q

It can also be controlled mechanically. The pilots use the side sticks to fly the aircraft in pitch and roll (and in yaw, indirectly, through turn coordination). Computers interpret pilot inputs and move the flight control surfaces, as necessary, to carry out these orders.

A

stabilizer and rudder

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25
Q

However, regardless of the pilot’s inputs, computers prevent:

A
  1. Excessive maneuvers.
  2. Flight outside the safe-flight envelope
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26
Q

The flight controls consist of primary and secondary surfaces, which are hydraulically actuated.

A
  1. Primary surfaces are ailerons, elevators, and rudder.
  2. Secondary surfaces are slats, flaps, airbrakes, spoilers, and lift dumpers
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27
Q

There are a total of 10 emergency exits: -

A

LHS & RHS sliding windows in the flight deck.

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28
Q

4 Type I Exits

A

Doors L1, L4 (passenger entry doors)
Doors R1, R4 (service doors)

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29
Q

4 Type III Exits

A

L2/ L3/ R2/ R3 over wing emergency exit at seat rows 12 & 14.

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30
Q

Minimum crew:

A

L1 (SCCM), R1, L4 and R4C.
No 5 – R4. No 6 – R4A.

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31
Q

If 6 Cabin Crew are carried

A

R4A will occupy the 12D seat at the O/wing exit on the RHS.

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32
Q

If 5 Cabin Crew are carried

A

R4 will occupy the 12D seat at the O/wing exit on the RHS and R4C will take over the R4 door.

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33
Q

With a full load, if relocation is not possible

A

passenger at 12D will occupy the vacant crew seat and must be briefed on the use of the crew seat and door operation.

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34
Q

Unprepared Emergencies:
In a 5 Cabin Crew operation,

A

R4 will be responsible for R4 door. R4C will assist with crowd control in an unprepared emergency

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35
Q

The minimum number of Cabin Crew carried is normally four (04). One Cabin Crew will always be designated as a SCCM and will occupy the L1 crew seat.

A

Other Cabin Crew will be designated according to a door or seat station.

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36
Q

It is a mounted seat and is installed on the LAV G door.

A

R4C seat

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37
Q

To install or stow the R4C seat it is necessary to lift the locking lever.

A

All six seats have a full harness; adjustment for fit is made on the lap straps only and there is a central locking box incorporating a rotary quick release buckle.

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38
Q

To Fasten Seat Belt

A
  1. Put both parts of the restraint system over the shoulders
  2. To fasten the seat belt insert the seat belt latch into the buckle until a distinct click is heard
  3. To tighten the seat belt pull the loose seat belt ends.
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39
Q

To Unfasten seat-belt

A

Turn the buckle in either direction to open the seat belt

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40
Q

Pre-Flight Check Seatbelt

A
  1. Seat folds satisfactory.
  2. Harness fits correctly, is free of twists, is in good condition and check for the inertia lock.
  3. Harness quick release operates.
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41
Q

Cabin Crew on vacating their seat must buckle the lap straps and shorten the length of the strap before allowing the seat to fold.

A

Any damage to the protective cover on the lap strap buckle or frayed parts on the belts must be reported to the PIC and entered in the Cabin Defect Report.

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42
Q

L1/R1 Crew Seat

A

FAP
AIP
CAS
Handset
Emergency Equipment

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43
Q

L4 Crew Seat

A

AIP
AAP
CAS
Handset
Emergency Equipment

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44
Q

R4C Crew Seat

A

Lavatory Door
Flag (vacant/occupied)
Door Knob
Shift to secure door
TTL Latch Handle
1/4 Turn Retainer
CAS

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45
Q

R4/R4A Crew Seat

A

Headrest
Seatbelt
Backrest
Bench
Emergency Equipment

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46
Q

Items stowed in the headrest container are indicated by a placard on the top of the headrest.

A

The Portable Breathing Equipment (PBE) is located in the headrest.

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47
Q

They are forward facing and are equipped with a conventional lap type seat belt and quick release buckle.

A

passenger seats

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48
Q

Risk of injury to small children’s fingers when operating the movable armrest.

A

Advise passengers travelling with small children of the potential risk related to the armrest movement.

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49
Q

Preflight Check Passenger Seat

A
  1. Seat belts satisfactory & crossed OR Fastened & Tightened.
  2. Safety card for aircraft type.
  3. LJ in stowage (percentage check).
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50
Q

Each Overhead Locker has one or two doors with a latch on the bottom edge of the door.

A

The Overhead Locker doors open upwards and give access to the compartment from the aisle.

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51
Q

Special damper hinges control the opening and closing speed of the door.

A

When the door is unlatched, the damper hinges hold the door in the fully open position. Each Overhead Locker has a grip rail installed along its length below the compartment door.

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52
Q

Overhead Locker - Door Operation
Opening

A
  1. Lift the latch until the Overhead Locker door is unlatched.
  2. Keep the hand away from the latch. The Overhead Locker door opens automatically.
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53
Q

Overhead Locker - Door Operation Closing

A
  1. Swing in the Overhead Locker door.
  2. Push the Overhead Locker door against the housing until the latch snaps into place.
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54
Q

AFTER CLOSING THE COMPARTMENT DOOR, CHECK THAT THE DOOR OF THE OVERHEAD LOCKER IS LOCKED CORRECTLY.

A

A VISUAL RED INDICATOR IS VISIBLE IF NOT LATCHED PROPERLY STOWED ITEMS COULD FALL OUT OF THE COMPARTMENT AND CAUSE INJURY TO PERSONS. IN THE CASE OF AN OHSC LATCHING FAILURE: UNLOAD, CLOSE AND IDENTIFY AS INOPERATIVE

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55
Q

Make sure that the doors of all stowage compartments are closed and correctly latched during

A
  1. taxi
  2. take- off
  3. turbulence
  4. landing
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56
Q

Depending on the compartment function, the load limit is specific. It is shown on a placard at the inner side of each stowage compartment.

A

Do not overload the stowage compartments: Overload may cause failure of the locking mechanism (danger of uncontrolled door opening) or damage at the stowage compartment Attachment. To avoid passenger injury, distribute some items to other stowage compartments.

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57
Q

They are installed above the seat rows in the cabin. They are attached together to make the Overhead Locker rows.

A

Overhead Lockers

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58
Q

At their bottom side, Overhead Lockers contain ___

A

oxygen containers and Passenger Service Units (PSU)

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59
Q

They incorporate the following facilities:

A
  1. An attendant call pushbutton
  2. Passenger reading light p/b per person,
  3. A seat row identifier & a loudspeaker
  4. A sticker for “NO SMOKING”
  5. an illuminated sign for “PROHIBITION OF PED” and “FASTEN SEAT BELT SIGN”
  6. (These are visible to all passengers and Cabin Crew in their normal seated position).
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60
Q

MANUAL DEMONSTRATION POSITIONS

A
  1. L1 will make the PA
  2. R1 will demonstrate in the FWD of the cabin – row 1
  3. R4C will demonstrate in the mid of the cabin– row 11
  4. L4 will demonstrate in the aft of the cabin– row 21
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61
Q

When operating with 5 Cabin Crew the door checks for the R4 door will be passed by

A

R4 (Cabin Crew) and not R4C.

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62
Q

They are plug type, open outwards and forward and have identical control handles.

A

main cabin doors

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63
Q

They are normally used to embark/disembark guests and to service the aircraft. Hold open latches (gust locks) will engage when the doors are fully open. Each door houses an inflatable escape slide, which when armed and opened, will deploy and inflate.

A

Main doors

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64
Q

In normal operation a door can be opened or closed using either__

A

(internal or external) control handles.

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65
Q

In emergency opening during an evacuation of the aircraft, initial movement of the door must be effected manually.

A

As the door is pushed outwards, it is forced open by a pneumatic system, which is linked to the slide arming mechanism. This acts as a damper for normal opening.

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66
Q

It s in the lower position when the door is closed and locked.

A

Internal Door Control Handle

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67
Q

Lift up to the __position to initiate door movement.

A

“OPEN”

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68
Q

Assist handles,

A

one FWD and aft of each door frame and one on the door.

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69
Q

Near the top of the door to verify the condition of the door.

A

Door Visual Indicators

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70
Q

With the door closed and the door control handle in the lower position the indicator will read___and is __ in colour.

A

“LOCKED”
green

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71
Q

If the door is not properly locked, the indicator will read __and is __ in colour. This must be checked every time a door is closed and locked and before arming the door.

A

“UNLOCKED”
red

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72
Q

Arming and disarming of the slide and power assist / pneumatic system is affected by moving the __

A

slide control lever.

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73
Q

When the lever is in the upper __ position, it protrudes and has a safety pin fitted with a red flag.

A

DISARMED

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74
Q

In the down (flushed) position with the safety pin stowed (red flag hidden), it engages the slide girt bar in floor latches and arms the door opening pneumatic system.

A

ARMED

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75
Q

The position of the slide control lever can be checked by looking at the __and is marked ARMED/DISARMED.

A

slide control lever window

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76
Q

Close to the observation window are two electrical indicator warnings.

A
  1. SLIDE ARMED Warning Light-
  2. CABIN PRESSURE Warning Light-
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77
Q

A caption __illuminates _ when the slide is armed and the door control handle is lifted up from inside.

A

“SLIDE ARMED”
WHITE (steady)

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78
Q

A caption __flashes__when - both engines are stopped, the slide is __ and the cabin differential pressure is above

A

“CABIN PRESSURE”
RED
DISARMED
2.5 millibar

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79
Q

The “SLIDE ARMED” and “CABIN PRESSURE” indicators are also visible from outside through the __.

A

observation window

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80
Q

They are provided and must be fitted across an open door way if no steps or aerobridge are in position at the threshold. The straps have end fittings, which hook into lugs on the door frame.

A

Door safety straps

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81
Q

It secures the door in its fully open position.

A

Gust lock

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82
Q

Preflight Check of Type I door

A
  1. Check door locking indicator reads locked (green).
  2. Door is disarmed – Safety pin is fitted, red flag is visible – and the slide control lever window reads
    disarmed.
  3. Observation Window is clear.
  4. Slide - pressure gauge needle is in the green zone.
  5. No Debris or Obstruction around the exit.
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83
Q

When the aircraft is ready for departure from the terminal, each crew member responsible for a door will move the slide control lever to __ This action is carried out on command from the __after the last cabin door has been locked.

A

ARMED.
SCCM

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84
Q

Arming

A
  1. Check the door locking indicator reads LOCKED (green).
  2. Remove the safety pin.
  3. Push the lever down to the ARMED position.
  4. Stow the safety pin and hide the red flag.
  5. Check the slide control lever window reads ARMED.
  6. Physically Cross Check the opposite Door.
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85
Q

When the aircraft arrives at the gate, each crew member responsible for a door will move the slide control lever to __ This action is carried out on command from the __

A

DISARMED.
Flight Deck

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86
Q

Disarming

A
  1. Remove the safety pin.
  2. Lift the lever to the DISARMED position.
  3. Refit the safety pin and ensure the red flag is visible.
  4. Check the slide control lever window reads DISARMED.
  5. Physically Cross Check the opposite Door.
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87
Q

When the ARMING lever is in the DISARMED position, a safety pin with a red flag must be installed to:

A
  1. Indicate that the door is in the DISARMED mode.
  2. Prevent inadvertent movement of the arming lever.
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88
Q

On the Type I doors the safety pin and flag is removed and stowed on top of the support ARM.

A

When the arming lever is in the ARMED position a flap moves under the disarmed hole, which avoids reinstalling of the safety pin

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89
Q

Normal Opening From Inside

A

Witness is present.
Both crew members must positively agree:
A. The Seatbelt Sign is OFF
B. The door is disarmed. - Check slide is DISARMED and safety pin fitted.
C. Positive Clearance has been received.
Grasp assist handle on the door frame.
Lift up the door control handle slowly 3 to 4 degrees and keep a watch on the Slide Armed warning light. Confirmation from Witness that the Slide Armed Warning Light is OFF, and says “Clear to Open the Door”.
If it does not illuminate, continue lifting it up to the OPEN position.
Push door outwards and forwards by using the door assist handle until the gust lock engages.

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90
Q

IF THE “SLIDE ARMED” CAPTION ILLUMINATES, THE DOOR IS STILL IN THE ARMED CONDITION. RESTOW THE HANDLE.

A

ALWAYS LIFT UP THE DOOR CONTROL HANDLE SLOWLY TO AVOID ACCIDENTAL DEPLOYMENT OF THE SLIDE.

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91
Q

CHECK “CABIN PRESSURE” CAPTION. IF RED LIGHT FLASHES:-

A

DO NOT OPEN THE DOOR - REPORT TO THE SCCM WHO WILL INFORM THE FLIGHT DECK. THE SLIDE SHOULD REMAIN DISARMED.

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92
Q

Normal Closing From Inside

A
  1. No debris or obstruction around the exit.
  2. Grasp assist handle on the door frame.
  3. Press gust lock release button.
  4. Pull door rearwards by door assist handle and pull into its frame
  5. Lower door control handle.
  6. Check door visual indicator reads “LOCKED” (in green).
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93
Q

Door Safety Precautions

A
  1. Never leave a door half open. It must be either fully open or locked closed.
  2. Before opening or closing a door the floor area across the width of the doorway and for 18” (0.5m)
    inboard must be clear of debris or obstruction.
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94
Q

Emergency Opening From Inside

A
  1. Check slide is ARMED.
  2. Check outside conditions are safe.
  3. Grasp assist handle on door frame.
  4. Lift door control handle fully up and release it.
  5. Monitor slide inflation.
  6. If slide FAILS to inflate Pull Red manual inflation handle on right hand side of the door girt.
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95
Q

It should only be conducted once Evacuation Orders have been received and External Conditions are safe.

A

Emergency Opening of the door

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96
Q

DO NOT KEEP HOLD OF THE DOOR CONTROL HANDLE OR DOOR ASSIST HANDLE AS THE DOOR IS OPENED WITH FORCE BY THE PNEUMATIC SYSTEM.

A

IT WOULD PULL THE OPERATOR OUT OF THE AIRCRAFT.
SHOULD THE PNEUMATIC SYSTEM FAIL, PUSH THE DOOR OPEN MANUALLY BY USING THE DOOR ASSIST HANDLE.

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97
Q

Each cabin door can be opened from the outside. Opening instructions are written next to the external door control handle (opening handle).

A

Note: If a cabin door is opened from the outside, and the slide is in the Armed mode, the slide automatically gets disarmed.

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98
Q

Normal Opening From Outside:

A
  1. Look through the observation window to ensure Cabin Pressure Warning light is off.
  2. If Off, push the flap to grasp the handle.
  3. Lift the handle up to the horizontal green line.
  4. Pull the door outward and forward, till the gust lock engages.
  5. Restow the handle to the completely flushed position.
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99
Q

SLIDE

A
  1. The slide at the four Type I doors are all single lane, and can be detached and separated from the aircraft.
  2. There is a dual lane overwing ramp slide at the aft edge of each wing
  3. All are equipped with a manual inflation system in case the automatic inflation system fails during
    operation. Slides take approximately 4 to 6 seconds to inflate.
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100
Q

The inflation reservoir sensors are connected to the __ and the pressure of the inflation cylinder is indicated on the __

A

CIDS
FAP.

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101
Q

The slides at the four Type I doors are all single lane, and can be detached and separated and converted to floatation devices in the event of a ditching.

A

All are equipped with a manual inflation system in case the automatic inflation system fails during operation. The Slides deploy directly to the ground and Hand Grips are stitched to the sides. The Slides are illuminated by integral lighting strips. Slides take approximately 4 to 6 seconds to inflate.

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102
Q

It is visible through a viewer on the front of the slide- pack cover, indicates whether the pressure in the gas inflation system is sufficient. This must be checked during pre-flight.

A

Pressure gauge

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103
Q

Preflight Check of Pressure Gauge

A

The slide pack pressure gauge needle visible through a viewer must indicate in the green band. Pressure varies with temperature and an abnormally low reading will be obtained after a long flight. In this case, check the gauge again after about 45 minutes, when the pack will have warmed to the surrounding temperature.

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104
Q

Operation

A

When a door is opened with the slide armed, the pneumatic system forces the door fully open. Because the slide girt bar is held in floor latches, the slide is pulled out of its container and will fall outside the aircraft. When the slide has dropped approximately 15” (38 cms), it will inflate automatically.

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105
Q

Manual Inflation Of Door Slide

A

All Slides are provided with a manual inflation system in case the automatic inflation fails during operation. The Red Manual Inflation Handle is located on the RHS of the door girt.

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106
Q

Using As A Hand Held Slide

A

If a slide fails to inflate by any means, it will hang down outside the aircraft. Four people should climb down the slide and extend it using the handgrips. It can then be held at an angle to support evacuating passengers.
Cabin Crew evacuation commands to passengers in this case will be- “SIT AND SLIDE”.

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107
Q

AS THE DOOR OPENS RELEASE THE GRIP ON THE DOOR CONTROL HANDLE.
HOLD ONTO THE DOOR FRAME ASSIST HANDLE AND GUARD THE DOOR EXIT UNTIL FULL INFLATION IS COMPLETE.

A

THE SLIDE INFLATION SEQUENCE TAKES 4 - 6 SECONDS.
IF THE SLIDE PACK IS WITHDRAWN BUT DOES NOT FALL OUTSIDE THE AIRCRAFT, PUSH IT OVERBOARD WITH YOUR LEG.

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108
Q

Method of Detaching and Separating From The Aircraft

A

Step 1 – To detach the slide from the girt, pull on the girt cover to expose the white detach handle
Step 2– Pull the white DETACH HANDLE completely free of the slide (until the slide is unlaced from the girt extension). When detached from the girt the slide is still connected to the aircraft by a mooring line which has one end tied to the girt bar.
Step 3 – To Separate the mooring line
To SEPERATE the mooring line cut the line with the hook knife. To use the the knife remove from its stowage. The Blade is curved with a single cutting edge on the inside. Always replace the knife in its stowage after use.
The mooring line will break if the aircraft sinks before it can be cut.

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109
Q

Four inward opening Type III emergency exits are provided, two on either side of the fuselage at seat rows 12 & 14 in the cabin. They can be located in darkness or smoke by sidewall mounted emergency lights and an exit marking sign.

A

An Over-Wing escape ramp slide assembly, consisting of a dual lane ramp with a dual lane slide is contained in an exterior fuselage compartment near the aft edge (root) of each wing. The slides are always armed and deploy when the exit is removed (opened from inside) or pushed in from the outside.

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110
Q

In an emergency the __situated on both sides of the emergency exit are illuminated.

A

EXIT markers

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111
Q

They are used to remove the exit.

A

Assist Handle
Exit Control Handle

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112
Q

A normal window with a shade is integrated into the __

A

emergency exit.

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113
Q

It covers the EXIT CONTROL HANDLE. The control handle is covered with a protective cover, as the exits are adjacent to passenger seats. To open the exit, the control handle has to be pulled down. When t__ is removed it exposes the Exit control handle, and illuminates the slide armed warning (white steady) light.

A

COVER FLAP

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114
Q

It is a groove on the Cover Flap to enable the passenger to remove it.

A

COVER FLAP RECESS

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115
Q

You can find the It on the backs of the seats next to the emergency exits and on the Exit itself.

A

OPENING INSTRUCTIONS

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116
Q

It is illuminated in case of an emergency evacuation.

A

EXIT sign

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117
Q

It is to indicate the slide status is situated next to the hatch.It is fitted in between the two exits on the left and the right hand side. This light illuminates white steady when the protective cover is removed or tampered with, thus warning the person that the ramp slide is armed.

A

SLIDE ARMED indicator

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118
Q

Pre-Flight Check of Type III Exit

A
  1. Cover flap fitted and secure,
  2. Slide armed indicator not illuminated, and
  3. Check the “exit opening instructions” placard is present on the exit and on the seat backs in front of
    the passengers at row 12 and 14.
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119
Q

Emergency Opening from Inside

A
  1. Check outside conditions are safe,
  2. Pull and discard cover flap,
  3. Grasp assist handle,
  4. Pull down exit control handle,
  5. Pull exit hatch inside, lift out of frame and turn,
  6. Throw hatch outside aircraft,
  7. Leave climb out on the wing,
  8. Monitor ramp slide inflation.
  9. If the Ramp Slide fails to inflate Pull the red manual inflation handle.
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120
Q

The weight of the Over-Wing exit is__

A

15Kg (32lbs).

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121
Q

Emergency Opening From Outside

A

Push the red flap and the emergency exit collapses inside the aircraft.

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122
Q

The ramp slide automatically deploys and inflates if the window is pushed in by the outside red flaps.

A

In a ground evacuation, passengers leaving from an Over-Wing exit are directed aft and ordered to “RUN AND SLIDE”.

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123
Q

In a ditching evacuation passengers leaving from an Over-Wing exit are directed to the nearest available group of passengers using the leading edge of the wing.

A

The Over-Wing ramp slides are fitted with integral emergency lighting strips.

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124
Q

Location Of Over-Wing Ramp Slide

A

The Over-Wing Ramp slide is stowed in the wing / fuselage fairing aft of the emergency exits.

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125
Q

Over-Wing Ramp Slide Deployment And Inflation

A

When one of the two emergency exits is opened, the ramp slide deploys and inflates on that side. Inflation takes only 4-6 seconds.

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126
Q

Manual Inflation

A

The ramp slides are equipped with a manual inflation system in case the automatic inflation fails during operation. The Red Manual Inflation Handle is provided at the top inner corner of each frame when the exit is removed and must be pulled down to inflate the ramp slide

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127
Q

Damaged Over-Wing Slide Operation
In case the Over-Wing Ramp slide has been damaged or does not inflate by any means,

A

it can still be used as a hand held slide. Locate the snap hook and attach to hook attachment point on the wing.
Four ABP’s must hold the slide by using the two handles installed on each side of the ramp slide.

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128
Q

Exit Technique

A

To avoid injuries to the head and body when getting out of the exit, leave by the Leg-Body-Leg technique.

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129
Q

Wing Walkways
The ground evacuation route from an Over-Wing exit is

A

AFT on the non- skid surface to the dual lane ramp.

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130
Q

ALWAYS ENSURE THE COVER OVER THE EMERGENCY HANDLE IS FITTED AS THIS PREVENTS THE HANDLE BEING USED AS A HANDHOLD. THE SLIDE-ARMED INDICATOR IS NOT ILLUMINATED.

A

IN AN EMERGENCY LANDING OR DITCHING, THE EXITS MUST NOT BE REMOVED UNTIL THE AIRCRAFT HAS FINALLY STOPPED.
THE OVER-WING RAMP SLIDE SHOULD ONLY BE USED FOR GROUND EVACUATION.IN AN EMERGENCY LANDING OR DITCHING, THE EXITS MUST NOT BE REMOVED UNTIL THE AIRCRAFT HAS FINALLY STOPPED.
THE OVER-WING RAMP SLIDE SHOULD ONLY BE USED FOR GROUND EVACUATION.

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131
Q

Ditching Warning

A

The Over-Wing ramp slide compartment may be under water. There is no means provided for disconnecting the ramp slide from the aircraft, if the ramp slide deploys when the hatch is removed passengers might mistake the ramp slide for a usable slide .

132
Q

The flight deck compartment can accommodate two pilots and a third and fourth occupant. The third and fourth occupant stations comprise of a forward facing folding seat.

A

The third occupant seat is installed at the rear right of the flight deck compartment. The fourth occupant seat is located against the left rear partition in the flight deck. These seats are suitable for occupation during take-off and landing. In addition, the flight deck is thermally and acoustically insulated.

133
Q

The flight deck has been fitted with an intrusion and penetration resistant (bullet proof) door, which is fully compliant with rapid decompression requirements.

A

This door is fitted with “Flight Deck door locking system” which prevents the unauthorized entry into the flight deck. The door opens into the flight deck.

134
Q

The escape panel enables the crew to evacuate the flight deck, in case of an emergency when the door is jammed or stuck. This panel can only be removed from the flight deck side by pulling the quick release pins toward the center of the flap and kicking the panel open.

A

In case of an electrical supply failure, the door is automatically unlocked, but remains closed. In case of decompression in the cockpit, the door is automatically unlocked.

135
Q

The flight deck door release system (locking) is controlled by a three position __ toggle switch, located on the central pedestal.

A

(UNLOCK/NORM/LOCK)

136
Q

This position is used to enable the Cabin Crew to open the door. The toggle s/w must be pulled and maintained in this position until the door opens.

A

Unlock Position

137
Q

All latches are locked, and emergency access is possible for the Cabin Crew.

A

NORM position

138
Q

Once the toggle s/w has been moved to this position, the door is locked; emergency
access, the buzzer and the key pad are inhibited for a pre-selected time (5-15 mins)

A

LOCK position

139
Q

If the lock position has not been used by the pilot for 5-15 mins, the Cabin Crew is able to request emergency access to open the flight deck door.

A

The UNLOCK position overrides and resets any previous selection.
In case of an electrical supply failure or loss of cabin pressure the flight deck door is automatically unlocked but remains closed.

140
Q

COCKPIT DOOR Fault Open Indicator

A

OPEN light ON
OPEN light flashes
FAULT

141
Q

The door is either not closed, or properly locked.

A

OPEN light ON

142
Q

The Cabin Crew has started an emergency access procedure. If no reaction, the door will unlock at the end of the adjustable time delay (30 secs).

A

OPEN light flashes

143
Q

This light comes ON when a system failure has been identified.

A

FAULT

144
Q

Flight Deck Door Policy

A

The PIC does not have any discretion to waive the flight deck access procedures. Use of ‘Passwords’ or ‘Door-knock Codes’ is prohibited. Before each flight the Captain shall brief the SCCM as to the current flight deck door emergency access code. Please ensure that the code is not written down on any paperwork. On all flights, the cockpit door shall be closed and locked from the time all external doors are closed following embarkation until any such door is opened for disembarkation, except when necessary to allow routine access and exit by authorized persons.

145
Q

Access to the Flight Deck

A
  1. Whenever a Cabin Crew/Authorized Person needs to access the flight deck, they should make an interphone call to the flight deck identifying themselves.
  2. They should then press the # key on the keypad.
  3. After a Cabin Crew/Authorized Person has accessed the Flight Deck, the Flight Deck Door must be
    relocked/blocked immediately.
  4. Authorized person must take their request to access the Flight Deck through a Cabin Crew.
146
Q

Requirement To View the Area Outside the Flightdeck Door

A

If access to the Flight Deck is requested in-flight for any reason then the flight Deck Crew shall verify through the Video device that the person is authorized to enter the flight deck and is not under duress. The flight Deck Crew shall move the toggle s/w to the UNLOCK Posn to Unlock the door.

147
Q

Exit

A

One of the Flight Deck crew shall use the Flight Deck Entry Video to ensure that the area behind the Flight Deck Door is clear. Before exiting, the Cabin Crew/Authorized Person must confirm by the use of the Viewing Lens that the area behind the Flight Deck Door is clear.

148
Q

Flight Deck Emergency Access Code

A
  1. Before each flight the PIC shall brief the SCCM of the current Flight Deck Emergency Access Code.
  2. Prior to departure, the SCCM must brief the R1 & Cabin Crew in charge of the aft cabin of the Flight
    Deck Emergency Access Code.
  3. The Emergency Access Code is being provided to the aft Cabin Crew to enable access to the Flight
    Deck during an emergency should the Cabin Crew in the forward cabin become incapacitated. Crew
    must ensure that the code is not written down to guard against it falling into the wrong hands.
  4. It is recommended, Flight Deck crew check that the Emergency Access Code is functional prior to
    every originating flight.
149
Q

Flight Deck Sliding Windows

A

A sliding window outboard of each pilot’s position provides a secondary escape route from the flight deck; both windows can be opened from the inside only. The sliding windows are operated by the use of a control handle and can be held in the open position by a locking pin.

150
Q

Opening the Window

A
  1. Grip the control handle, located at the aft bottom corner of the window.
  2. Press down the unlocking pin.
  3. Maintain pressure on the pin and at the same time rotate the control handle inboard.
  4. The window will move inboard then slide fully aft. The window is locked in the fully open position by
    a locking pin (3) (only visible when the window is open).
151
Q

Closing the Flight Deck Sliding Window

A
  1. Move the locking pin (3) to the aft position,
  2. grip the control handle (1) and
  3. push window forward using control handle.
  4. The window is correctly locked when the red unlocking pin becomes visible.
    Note: The primary escape route for the occupants of the flight deck is through the F/D entrance door and out through exits in the main cabin.
152
Q

It is located in a recess above each sliding window and can be deployed through an open window to the ground. The rope has one end permanently fixed to a strong point and is coiled inside the recess. To gain access remove cover flap, then pull the rope out.

A

Escape rope

153
Q

It is a gaseous, diluter demand system with individual masks, regulators and face piece for each flight deck and observer.

A

Flight deck oxygen system

154
Q

Flight Deck Oxygen Unit

A

1 - Blinker Flow meter (yellow). - Flashes when oxygen is flowing. 2 - RESET/TEST control slide.
Authorizes testing of blinker operation, regulator supply, system sealing downstream of the valve, regulator sealing and operation.
3 - OXY ON FLAG -Appears once the oxygen supply valve is opened and the left flap door is closed.

155
Q

Description of Flight Deck Oxygen Mask

A

1 - Red Grips
Squeezing the (red) Right Hand Side grip unlocks the two-flap door and authorizes harness inflation.
2 - EMERGENCY pressure selector
This selector creates an overpressure, which eliminates condensation and prevents smoke, smell, or ashes from entering the mask.
Pressing this knob generates an overpressure for a few seconds.
Turning the knob in the direction of the arrow, generates a permanent overpressure.
Note: Overpressure supply is automatically started, when cabin altitude exceeds 30,000 feet. 3 - N/100% Selector
100% the mask delivers 100% oxygen ON DEMAND. The system is locked in this position when selected. When pressed the lever is released.
N- An air and oxygen supply will be given with the selector in Normal position (the content of which varies with cabin altitude).
Emergency & 100%- CONTINUOUS FLOW

Above 35,000 ft the air inlet is closed to give a 100% oxygen supply

156
Q

To access oxygen masks, open cover then carry out the following actions.

A
  1. Take the mask by squeezing the red grip and keep the red grip pressed.
  2. Remove the mask. The harness inflates,
  3. Don the mask (harness inflated).
  4. Release the red grips. The harness deflates and maintains the mask.
157
Q

The PIC & SIC seats are identical except the controls are on the opposite side.

A

All controls levers are on the inboard side of the seats. Opposite seat controls have the same functions.

158
Q

The cabin’s fixed oxygen system supplies oxygen to the occupants (passengers and Cabin Crew), in case of cabin depressurization.

A

Each chemical oxygen unit is made up of a solid-state chemical generator. Each generator feeds a group of 3 or 4 masks. Flexible supply hoses connect the masks to the chemical generators. The temperature of the generators reaches 180o F during Oxygen flow. Therefore, the smell of burning or smoke may be associated with the normal operation of the chemical generators.

159
Q

Generators and mask are installed in containers above the passenger seats (PSU) in the cabin, in the lavatories (ceiling) and at each Cabin Crew station. The chemical generators are activated when the mask is pulled down. Pulling one mask down causes all the masks in that unit to drop and oxygen flows to all masks.

A

A green in-line indicator is visible in the transparent oxygen hose whenever oxygen is flowing to the mask. Oxygen flows for minimum 15 minutes and cannot be shut off.
All “PROHIBITION OF PED” and “FASTEN SEAT BELT” signs come on automatically if the cabin altitude should exceed 11,300 ft. or if the cabin oxygen system is deployed. A taped emergency message is broadcast over the PA system when the oxygen system is activated.

160
Q

The chemical reaction used for Oxygen generation creates heat. Therefore, the smell of burning or smoke may be associated with the normal operation of the chemical generators.

A

ONCE ACTIVATED, OXYGEN GENERATION CANNOT BE STOPPED.
DO NOT RESTORE AN OXYGEN MASK, IF THE OXYGEN GENERATOR IS STARTED IN ORDER TO PREVENT THE SMELL OF BURNING OR FUMES

161
Q

This continuous flow mask provides oxygen due to the loss of cabin pressurization during an emergency descent. It is made up of the following components:

A
  1. Face piece
  2. Reservoir bag
  3. Elastic head strap
  4. Flexible supply hose with Oxygen flow indicator
162
Q

The number of oxygen masks contained in the unit is written on the __

A

door stop

163
Q

Location of Passenger Oxygen Units

A

To test the Oxygen units electrical unlocking system, THE ‘MASK MAN ON’ p/b is pressed in the Flight Deck panel. To prevent the oxygen masks from falling, the door stops on all oxygen containers have to be pulled down and turned 90 degrees clockwise. Then, unit snaps open, but does not drop.

164
Q

Preflight Check

A

Check that the doorstop is in normal position, flush with the door. If the PSU door stop is in the test position (protruding) report to SCCM.
On some aircraft the oxygen flow indicator is located at the base of the reservoir bag.

165
Q

Drop Down of the Oxygen Mask
The oxygen mask in the cabin may be dropped down in three ways:

A
  1. Automatically, at a cabin altitude of approximately 14,000 ft.
  2. Electrically, by using the switch (MASK MAN ON) on the pilot’s overhead panel.
  3. Manually, by inserting the MRT or any pointed object in the access hole.
166
Q

Oxygen System - Flight Deck Panel

A

1 - MASK MAN ON p/b (Guarded in the AUTO position)
AUTO: Oxygen mask/unit doors open automatically when cabin altitude exceeds 14000 ft (+500ft). An
automatic Announcement to passenger is made through the Passenger Address.
DEPRESSED: Oxygen mask drops down. An Announcement to passengers is made through the Passenger Address.
2 - PASSENGER SYSTEM ON light
Illuminates white when the oxygen masks unit doors is activated.

167
Q

Activation Of Chemical Generators

A

The chemical generators are activated when the mask is pulled down. Pulling one mask down causes all the masks in that unit to drop and oxygen flows to all masks. A green in-line indicator is visible in the transparent oxygen hose whenever oxygen is flowing to the mask. Oxygen flows for approx. 15 minutes and cannot be shut off.

168
Q

Fitting The Mask

A

When the drop out occurs, pull the nearest mask down and place it over the nose and mouth. Fit the elastic headband over your head.

169
Q

It operates, controls and monitors the main cabin systems.
It performs different system and unit tests.

A

The Cabin Intercommunication Data System (CIDS)

170
Q

It is connected to the following cabin systems:

A
  1. Air Conditioning
  2. Communications
  3. Fire Protection
  4. Ice Protection
  5. Lights
  6. Water and Waste
171
Q

The system philosophy makes it easy to change the cabin layout because CIDS hardware provides spare inputs, outputs and circuits. This allows the connection of new and/or additional cabin equipment without a change of CIDS hardware components. If any equipment is changed, only the CIDS software database has to be updated.

A

The CIDS system is also able to detect faults in its components and the connected equipment by itself

172
Q

The PA system distributes announcements from the cockpit and each attendant station through all assigned PAX loudspeakers.

A

Passenger Address

173
Q

it allows the communication via telephone between the ground crew, the Flight Deck and the Cabin Crew when the aircraft is on the ground.

A

Service Interphone System

174
Q

It allows the communication via telephone between all attendant stations and between the attendant stations and the cockpit.

A

Cabin And Flight Deck Interphone

175
Q

It informs the Flight Deck about the cabin status.

A

Cabin ready signalling

176
Q

It controls the illumination of the PAX call-light and the activation of the call-chime.

A

PAX call system

177
Q

The PAX lighted signs system controls the

A

PROHIBITION OF PED (PED), FASTEN SEAT BELT (FSB), RETURN TO SEAT (RTS) and EXIT signs.

178
Q

It transmits the pre-recorded announcement and the boarding music to the related PAX loudspeakers

A

PRAM
Pre-Recorded Announcement And Boarding Music

179
Q

It controls the illumination of the different cabin areas independently.

A

Cabin illumination system

180
Q

It controls the PAX reading lights and attendant work-lights in the cabin. In addition to the above described lights it is possible to install special decor lights and spot lights which are also controlled by the reading light system.

A

Reading lights system

181
Q

The CIDS can select different temperatures for all defined cabin zones. A fine adjustment of the pre-selected temperature for different zones is possible through FAP operations. The actual temperature per zone is indicated on the FAP.

A

Air Conditioning

182
Q

It shows the filling level of the water tank on the FAP and gives the commands for the pre-selection of the water quantity.

A

Potable water indication and pre-selection system

183
Q

It shows the filling level of the waste tanks on the FAP. In addition to that inoperative lavatories are indicated on the FAP and respective messages come on.

A

Waste indication system

184
Q

The smoke detection system controls the visual and acoustical indications in the cabin if a smoke alert is received from the Smoke Detection Control Unit SDCU.

A

Lavatory Smoke Indication

185
Q

It monitors the door and escape-slide bottle-pressure reservoir at the PAX doors and the emergency exits. In addition to that it monitors the status of the doors (OPEN/ CLOSED) and the escape-slides (ARMED/DISARMED). The status is indica

A

Doors And Escape-Slides Pressure Monitoring

186
Q

It controls the evacuation signaling in all cabin areas and in the cockpit. It can be activated from the cockpit, the FAP (guarded push button called EVAC CMD) or, as an option, from the AAP (EVAC CMD) during an emergency.

A

Emergency Evacuation Signaling

187
Q

It gives the remote controlled operation of the PAX reading lights and the PAX call activation/ deactivation.

A

Passenger Service System
The PSS

188
Q

The CIDS system consists of these components:

A
  1. Directors
  2. Decoder/Encoder Units (DEU), Type A and B
  3. Passenger Interface and Supply Adapter (PISA)
  4. Flight Attendant Panel (FAP)
  5. Cabin Assignment Module (CAM)
  6. On Board Replaceable Module (OBRM)
  7. Integrated PRAM (I-PRAM)
  8. Additional Attendant Panel(s) (AAP)
  9. Attendant Indication Panels (AIP)
  10. Area Call Panels (ACP)
  11. Handsets
  12. Loudspeakers
  13. Passenger call/reset pushbuttons
  14. Passenger call lights
  15. Prohibition of PED (PED), Fasten Seat Belt (FSB) and Return To Seat (RTS) signs.
189
Q

All components of the CIDS are connected to the two identical directors, one of them in active mode and the other one in hot standby mode. The directors are the central control components of the CIDS.

A

They monitor the system performance continuously, store detected faults and send them to the Warning and Maintenance System (WMS) and/or the FAP. In the event of a major fault, respective information is sent additionally to the ECAM Status Page or to the ECAM Warning Page.

190
Q

Location of FAP & AAP

A
  1. The Forward Attendant Panel (FAP – L1) is located above the L1 / R1 crew seat.
  2. The Additional Attendant Panel (AAP – L4) is located besides the L4 door.
191
Q

It enables the Cabin Crew to control certain cabin systems and the CIDS, indicates the status of several cabin systems and provides the cabin zone programming.
It is located at the attendant station __

A

FORWARD ATTENDANT PANEL (FAP - L1)
L1

192
Q

The FAP has the following modules:

A
  1. Display unit (touch screen panel)
  2. Sub panel (hard key panel).
193
Q

It indicates all the cabin information.
It is used to select the different cabin functions (like cabin illumination) and the cabin programming.

A

Touch screen panel

194
Q

The sub panel contains all hard keys and some interfaces.

A
  1. EMER (Emergency Lighting System)
  2. PED POWER (In-seat Power Supply System (ISPSS)
  3. LIGHTS MAIN ON/OFF (Cabin Lighting)
  4. LAV MAINT (sets the lavatory lights to full brightness in the case of lavatory maintenance)
  5. SCREEN 30 s LOCK (sets the touch screen in a sleep modus for a time period of 30 s for cleaning
    purposes)
  6. EVAC CMD (activates the Evacuation Alert System)
  7. EVAC RESET (resets the Evacuation Alert System)
  8. SMOKE RESET (resets the Lavatory Smoke System).
195
Q

The SCCM is responsible to ensure that the PED Power switch on the FAP must be switched OFF:

A

Take off : Once last Cabin Door Closed till Seatbelt Sign Off after take - off. Landing : Seatbelt Sign ON till Seatbelt sign OFF at parking bay.

196
Q

Every cabin system (e.g. cabin lighting) shown on the system pages of the FAP is selectable by the SYSTEM AND FUNCTION KEY SET.

A

Related to the cabin systems there are different sets of system and function keys with a maximum of 9 keys. The next/previous key set can be chosen with the forward/backward button.

197
Q

To display the CABIN STATUS page, push the button in the lower right corner of the touch screen. This
page gives an overview of the standard CABIN STATUS page including these pages:

A
  1. AUDIO
  2. LIGHTS
  3. DOORS/SLIDES
  4. TEMPERATURE (AIR CONDITIONING)
  5. WATER/WASTE
198
Q

Additionally there are some push buttons and indications on the display area:

A

CAUT button with active INFO ROW, HEADING ROW, SCREEN OFF button, CABIN READY button, SYSTEM AND FUNCTION KEYS and the active CABIN STATUS button.

199
Q

On the CABIN STATUS page, these systems can also be selected by pushing the __on the touch screen.

A

related A/ C symbol

200
Q

It is always shown in the upper left corner of the touch screen, normally in the de-active mode (OFF). If CIDS receives a message which cannot be indicated the __ is illuminated in flashing mode and a text message is displayed in the INFO ROW. This message will stay as long as the respective page is not selected on the touch screen.
After displaying the page(s) related to the message(s) or after pushing the__ remains on (steady).

A

The CAUT button

201
Q

An arrow, in front of the actual text message in the INFO ROW shows that more than one message are present. The HEADING ROW displays the title of the actual selected page below the INFO ROW in the middle of the screen.

A

The HEADING ROW displays the title of the actual selected page below the INFO ROW in the middle of the screen.

202
Q

The __is located in the lower left corner of the display. Pushing that button switches the screen off.An automatic event (CIDS message) or touching the FAP display reactivates the screen again. This touch does not activate any system function.As an option it is possible to protect the manual reactivation of the screen through an access code against misuse. Then the screen is locked after it is switched off.
Only a SMOKE event is displayed on the screen automatically.

A

SCREEN OFF button
The LAYOUT SELECTION page is also locked and can be activated by typing in the correct access code on the PASSWORD page

203
Q

The __switches the screen off automatically after a time period of 10 minutes if a page was manually selected or an auto page is quit. During this period the screen is dark or, as an option, shows a screen saver.
The reactivation of the FAP is done by a single touch on the screen without activating any other function unintentionally. The FAP then comes back to the previously selected page.

A

TIME OUT function
Note: If the SCREEN OFF function is in use, the TIME OUT function does not work

204
Q

Optionally it is possible to have an external system displayed on the display area to (e.g. Cabin Logbook).

A

The external system is selected by the system and function keys as for the CIDS related systems. Only the display area is under control of the respective system.
To operate external systems via the FAP additional and optional PC hardware must be installed inside.

205
Q

If CIDS receives an important message, the related system page comes up automatically. The automatic activated page is displayed as long as the page is quit.
A smoke alert calls up the SMOKE page and overrides any other page. The following pages come up automatically with these indication priorities:

A

PRIORITY
TITLE OF PAGE
1.
SMOKE
2.
DOORS/ SLIDES
3.
WASTE/WATER
4.
SYSTEM INFO
5.
AUDIO
6.
SOFTWARE DOWNLOAD

206
Q

The cabin attendants can control certain cabin systems
It is installed at the attendant station L4. The AAP is a switch panel consisting of 3 rows x 6 columns of membrane switches.

A

ADDITIONAL ATTENDANT PANEL (AAP)

207
Q

The illumination of the AFT entrance area (The LED on the pushbutton illuminates when the pushbutton is pressed)

A
  1. ENTRY BRT: to set the entrance area lights to 100% brightness
  2. ENTRY DIM 1: to dim the entrance area lights to 50% brightness
  3. ENTRY DIM 2: to dim the entrance area lights to 10% brightness
208
Q

To switch off the entrance area lights, __.

A

press the active (illuminated) pushbutton a second time

209
Q

To switch on the entrance area lights again, __ The entrance area lights illuminate with the corresponding brightness.

A

press one of the pushbuttons ENTRY BRT, ENTRY DIM 1 or ENTRY DIM 2.

210
Q

The illumination of the passenger zone (The LED on the pushbutton illuminates when the pushbutton is pressed)

A
  1. CABIN BRT: to set the passenger zone lights to 100% brightness
  2. CABIN DIM 1: to dim the passenger zone lights to 50% brightness
  3. CABIN DIM 2: to dim the passenger zone lights to 10% brightness
211
Q

All passenger zone lights can only be switched off together on the ___

A

FAP.

212
Q

The reset of the evacuation signaling chime

A

(EVAC RESET)

213
Q

The indication of the evacuation signaling

A

(EVAC)

214
Q

The indication of the lavatory smoke alert and the reset of the respective signaling chime

A

(SMOKE RESET)

215
Q

Internal and external emergency lighting is provided. All the lights are powered by independent power packs and are controlled from a three position

A

(OFF-ARM-ON)
switch on the pilot’s overhead panel and one press switch in the main cabin by (FAP) L1 crew panel. Emergency lights last for atleast 10 minutes.

216
Q

Fixed Internal Emergency Lighting

A
  1. Floor Path/Proximity Emergency Escape marking systems (Escape path lighting system and exit markers)
  2. Overhead Cabin emergency lights / Ceiling Dome Lights
  3. Exit location signs
  4. Exit marking signs above the Exits
  5. The escape-hatch handle lights illuminate the areas of the handles inside the cabin.
  6. Lavatories ceiling dome light
  7. Cockpit ceiling dome light
217
Q

The floor path marking system enables passengers and crew to find the way to the exit in the event of smoke in the cabin.
Features are as follows: -

A
  1. Photo luminescent strips on the floor. (Glow in the dark)
  2. Illumination of the aisle
    They show the way to the exits, if the exit signs and the general illumination the cabin emergency lights are no longer visible. (E.g. the cabin is full of smoke).
218
Q

In the event of excessive cabin altitude (__ the PROHIBITION OF PED, FASTEN SEAT BELT, and the EXIT signs illuminate regardless of the position of the switch in the Flight Deck.

A

11,300 +/-500ft),

219
Q

It comes on automatically when anyone of the Overwing exits is opened on the respective side.

A

Wing lights (2 on each side)

220
Q

These lights come on automatically when the slide / over wing escape ramp slides are deployed.

A

Door slide and over wing exit ramp slide internal lighting strips.
Note: When the door slides are detached from the aircraft their light goes out.

221
Q

EMER EXIT LT “OFF” light
OFF: If EMER EXIT LT Switch is selected OFF,

A

the OFF light comes on amber. When the EMER pushbutton at flight attendant panel is pressed, it activates the emergency lights and exit signs, the OFF light goes off.

222
Q

EMER EXIT LT SWITCH

A

ON: Overhead Emergency lights, Exit signs, Exit Locators illuminates in the cabin.
ARM: Overhead Emergency lights, Exits signs automatically illuminate if A/C normal electrical power is lost. OFF: Overhead Emergency lights, Exits signs, Exit Locators are off.
(The general illumination does not operate)

223
Q

When the switch EMER EXIT LT (1) is in position ARM, and the AC power supply for the general illumination is not available, the cabin emergency lights in the ceiling and above each door come on automatically. The system is supplied by the essential DC power supply
(The cabin pressure is too low)

A

When the switch EMER EXIT LT (1) is in position ARM, and CABIN PRESSURE LOW is detected, all elements of the emergency lighting system comes on automatically (except overwing lights and escape slide emergency lights). The system is supplied by the essential DC power supply.
Note: The emergency lighting can be activated independently of the position of this selector from the FAP (L1).

224
Q

Cabin Controls

A
  1. EMER (on FAP)
    Pressed same function as the EMER EXIT LT Flight Deck switch in the ON position.
    Note: In the event of emergency landing (L/G retracted), a procedure shall be incorporated in the FCOM to read that the OFF-ARM-ON switch must be set to the “ON” position.
225
Q

Cabin Signs

A

Return to Seat Sign
Fasten Seatbelt Sign
No PED Sign
No Smoking Sticker

226
Q

SEATBELT SWITCH

A
  1. ON: FASTEN SEAT BELT and RETURN TO SEAT signs come ON together with a low chime.
  2. AUTO: FASTEN SEAT BELT and RETURN TO SEAT signs come ON automatically together with a
    low chime when slats are extended.
  3. OFF: Signs are off. Low chime sounds upon extinction of lights.
227
Q

NO PORTABLE ELEC DEVICE SWITCH

A
  1. ON: PROHIBITION OF PED and EXIT signs come ON together with a low chime.
  2. AUTO: PROHIBITION OF PED and exit location signs, exit marking signs and escape-hatch handle lights come ON when landing gear is extended and go OFF when the landing gear is retracted (the
    EMER EXIT LT switch is in position ARM)
  3. OFF: Signs are OFF. Low chime sounds upon extinction of Lights.
    Note: If the cabin altitude goes above 11,300 feet (+500 feet), the cabin Illuminates and PROHIBITION OF PED, FASTEN SEAT BELT and EXIT signs come ON regardless of the SEAT BELTS and NO PORTABLE ELEC DEVICE selector switches.
228
Q

The __provides visual and aural alert in the event of impending emergency evacuation of the aircraft, warning lights are installed at the cockpit overhead panel and at the FAP (L1) and AAP (L4) attendant station.
The aural signal will guide evacuating passengers to the exits in smoke and in particular will enable blind passengers to locate the exit.

A

Evacuation signaling system

229
Q

1 - Command pb sw - pressed In the cockpit

A

ON indicator comes on
EVAC indicator flashes red
EVAC horn is triggered

230
Q

In the Cabin

A

EVAC RESET flashes at FWD (L1) and EVAC light flashes at AAP (L4) and A buzzer tone is generated, similar to that generated in the flight compartment, at the fwd and aft Cabin Crew stations and in addition via the PA loudspeakers adjacent to the emergency exits.
All AIPS’s flash red with a message “EVAC ALERT”.

Pressed again - The alert is cancelled.

231
Q

2 - Horn Shut Off - pressed
In the cockpit

A

The cockpit evac horn is silenced EVAC indicator continue flashing.

232
Q

3 - CAPT/ CAPT & PURS Selector

A

The two position selector switch controls the evacuation signal system and is always kept in the “CAPT”
position. This will allow the Flight Deck or the SCCM to activate the evacuation signal.

233
Q

EVAC CMD p/b at FAP - pressed In the cockpit

A

EVAC indicator flashes red
EVAC horn sounds
Pressing it again stops the alert.

234
Q

EVAC RESET (at FAP) - pressed

A

EVAC buzzer is silenced at the forward station and at the emergency exit doors.

235
Q

EVAC RESET (at AAP) - pressed

A

EVAC tone is silenced at the aft attendant station

236
Q

Use Of Signaling System

A

The signals at all panels can only be cancelled simultaneously from the station initiating the command. When the HORN SHUT OFF or RESET switch is pressed, the signal will be silenced at that area only, but the EVAC caption / integral lights will continue to flash.

237
Q

CAPT & PURS/CAPT” Switch

A

The CAPT / CAPT & PURS switch must be in the “CAPT” position at all times.

238
Q

4 Area Call panels are installed in the cabin ceiling:

A

2 in the FWD of the cabin and 2 in the AFT of the cabin.

239
Q

The ACP has coloured lights Blue, Red and Amber indicating the Cabin Crew from where the call has been initiated:

A
  1. Amber steady - Passenger call from the Lavatory.
  2. Amber flashing - Lavatory smoke.
  3. Red steady - Flight Deck to Cabin Crew call & Cabin Crew to Cabin Crew Call.
  4. Red flashing - Emergency call from the Flight Deck.
  5. Blue steady - Passenger call from Seat.
240
Q

LOCATION AND DESCRIPTION OF ATTENDANT INDICATION PANEL (AIP)

Features are as follows:

A

3 AIP (1 FW, 2 AFT)

  1. alphanumeric display with 2 rows each of 16 characters.
  2. display of communication information in upper row.
  3. display of cabin system information in lower row.
  4. red and green indicator lights used as attention getters.
  5. (green illuminates during normal communication, Red flashes during smoke and emergency call).
241
Q

There are two types of priorities of interphone calls:

A
  1. Functional priorities
  2. Source priorities
242
Q

The possible functions have different priorities, i.e. every selected function overrides a function with a lower priority.

A

LEVEL
FUNCTION
1
PA ALL
2
Calls from the Cockpit
3
Emergency Call
4
PA
5
Normal Call
6
Service Interphone
7
All Attendant Call
8
Reset

243
Q

The function of the water system is to supply water from the water tank to:

A
  1. The galleys
  2. The lavatories.
244
Q

The function of the waste system is to discard:

A
  1. The waste from the lavatories in the lavatories to the waste tank
  2. The wastewater from the lavatory wash-basins and galley sinks through the heated drain masts.
245
Q

Water Tank
Location

A
  1. LH behind the bulk cargo compartment, near the partition wall, or
  2. In the underfloor area RH behind the forward cargo compartment.
246
Q

The water tank has a usable capacity of

A

200 l (52 US Gal).

247
Q

The pressurization of the water system is achieved with compressed air. It makes sure that the water flows from the water tank to the galleys and lavatories.

A

Water Supply

248
Q

They are installed in each wet galley and lavatory. The water supply stops, when the manual water shut-off valves are closed.

A

Manual Water Shut Off Valve

249
Q

The waste water from the galley and lavatory wash basins is discarded overboard through the FWD and AFT heated drain masts.

A

Waste Water Drainage

250
Q

Lavatories

A

Drain-Valve Assembly (Drain Assembly)
The drain assembly is installed at the bottom of the wash basin and is connected to its overflow.
Drain Valve
The drain valve is installed below the drain assembly in the wastewater line of the lavatory. It lets the wastewater drain to the drain masts and prevents the loss of air pressure through the drain mast.

251
Q

Galleys

A

Drain Valve
The drain valve is installed below the sink in the wastewater line of the galleys. It enables the wastewater drain to the drain masts and prevents the loss of air pressure through the drain mast.

252
Q

Waste Tank
Location

A

One waste tank is on board the aircraft located RH behind the bulk cargo compartment, near the partition wall.

253
Q

The waste tank has a usable capacity of

A

200 l (52 US Gal).

254
Q

Water Quantity greater than __. Waste less than __

A

75%
25%.

255
Q

3 lavatories are installed in the cabin area at position A, F and G.

A

Each Lavatory door is equipped with a latching mechanism that enables the crew to unlock the door from the outside. Each lavatory has a toilet function and a washroom function.

256
Q

Following connections are provided:

A
  1. A cold and hot water supply.
  2. A waste and wastewater disposal.
  3. An air outlet.
  4. An electrical power supply (razor socket).
257
Q

Lavatory Water Heater

A
  1. Light – illuminates when water heater is energized (ON position).
  2. ON/OFF s/w
    A. ON : Water heater energizes.
    B. OFF : Water heater disconnects.
258
Q

Power supply of water is cut off when at least one of the following conditions is fulfilled:

A

Water temperature reaches between 72°C and 82°C. Water level in the water tank reaches a certain minimum level.

259
Q

It is located under each wash basin in the lavatory. To shut off the water supply to the water heater and the faucets in the sink rotate the shut off valve to the Vertical position (close position).

A

Manual Water Shut Off Valve

260
Q

Ensure that the water heater has been switched off prior to shutting the water shut off valve.

A

Wet Galleys are equipped with water shut off valve as well.

261
Q

An automatic fire extinguisher is installed on the__Each consist of a container from which nontoxic halon gas will be discharged through two nozzles, direct towards the waste towel container if too high a temperature is reached. Each nozzle is tipped with a sealing compound which will melt when the surrounding temperature reaches 71oC (160oF) and allow the gas in the container to discharge. A gauge is visible to indicate the contents.

A

top panel of the waste bin under the sink in each lavatory.

262
Q

Pre-Flight Check of the Automatic Fire Extinguisher

A

Contents gauge indicator is in the green zone.

263
Q

If there is a discrepancy in the contents inform SCCM who will inform PIC/Engineer.

A

An inspection for fire damage must be made and the extinguisher replaced.

264
Q

Pre-Flight Check of the Lavatory

A
  1. Smoke detector is unobstructed
  2. Passenger Call bell is functional
  3. Waste bin flaps are spring loaded
  4. Automatic Fire extinguisher contents gauge indicator is in the green zone
  5. Return to seat sign functional
  6. Water Faucet functional.
  7. Flush servicable
  8. Lavatory Locks from inside and Outside.
265
Q

A centralized smoke detection system is provided in the lavatories.

A

If there is presence of smoke in any one lavatory, the following visual and aural warnings are triggered.

266
Q

Do not discharge aerosol spray / disinsecting spray near the detector unit as it may activate the smoke detector.

A

A fine will be levied to any person that may tamper with, disable or destroy the smoke detector in any lavatory.

267
Q

Lavatory Smoke In the Cabin

A
  1. Repetitive triple single chime is broadcast via all (CABIN + Cabin Crew) loudspeakers repeated every 30 seconds.
  2. Amber light on the related ACP flashes.
  3. On all AIP red light flashes and message “SMOKE LAV A/F/G” message is displayed.
  4. Lavatory indicator light outside the corresponding lavatory flashes.
  5. SMOKE LAV Integral lights (steady) come on – FAP (L1).
  6. SMOKE RESET light (steady) come on – FAP (L1) or AAP (L4)
268
Q

Lavatory Smoke In the Flight Deck

A
  1. Master Warning p/b illuminates Red.
  2. “SMOKE LAVATORY SMOKE” message appears in red on upper ECAM display.
  3. Continuous repetitive chime sounds.
269
Q

When the Master warning p/b is pressed.

A
  1. Red light of Master Warning goes off
  2. Continuous repetitive chime is silenced.
  3. “SMOKE LAVATORY” message remains on ECAM display until the smoke is dissipated.
270
Q

SMOKE RESET light

A

Illuminates red in case of presence of smoke in one lavatory.
Extinguishes when the smoke concentration drops below the threshold of the respective smoke detector.

271
Q

SMOKE RESET p/b - pressed

A

Reset of all aural (audio) and visual warnings except the “SMOKE RESET light will still remain ON at the FAP (L1) or the AAP (L)4 until the smoke is cleared from the lavatory.

272
Q

Crew Action

A

Once the toilet has been identified all the indications except the “Smoke Lav” internal light, can be cancelled by pressing the RESET p/b on the FAP (L1) or the AAP(L4).

273
Q

Individual galley modules may contain ovens, waste containers, coffee makers, refrigeration units, storage/ servicing carts, sinks and stowage space to aid in food preparation and dispensing.

A

Galleys are equipped with electrical power and water systems. Lighting controls are located on the galley electric panel. A galley vent system keeps the air fresh.

274
Q

Service carts are restrained for takeoff and landing. There are stowage areas for extra carts located at various galleys.

A

The number of carts must not exceed the number of in-flight cart restraints available.

275
Q

Galley sink waste water is drained overboard through heated drain masts. To prevent sink drain blockages do not put solid waste (coffee grounds, tea bags, fruit pulp, and so on) in the sink drain. Put solid waste in the galley waste bins. Mixtures, which can curdle and create a drain blockage, should be diluted with an equal amount of water

A

. Do not remove the sink drain strainer.
You have to pull and release the operating button respective the operating ring of the drain valve, when the waste water does not flow through the sink.

276
Q

Watar Shut off Valve

A

Each galley that has running water is equipped with a water shutoff valve. Positioning the water shutoff valve to OFF turns off water to that galley.

277
Q

The interphone system provides communication and alerting facilities between the Flight Deck , Cabin Crew and ground services staff.

A

The attendant handset is equipped with PA and interphone capabilities. The handsets are accessible to attendants while strapped in their seats

278
Q

FWD p/b / AFT p/b – pressed (Flight Deck Calls FWD/AFT Attendants) - -

A

Chime - I Hi-Lo chime (via respective attendant loudspeakers).

  • ACP - Steady RED light at respective ACP.
  • AIP - Steady green light at respective AIP and “CAPTAIN CALL “(text)
279
Q

EMER p/b – pressed (Flight Deck Emergency Call To Cabin Crew) -

A

Chime - 3 Hi-Lo chime (via all attendant and cabin loudspeakers).

  • ACP - Flashing Red light at all ACP
  • AIP - Flashing Red light at all AIP and text message “EMERGENCY CALL“.
280
Q

After hooking off the handset at the called station

A

a communication link to the cockpit is established.

281
Q

The Cabin Crew handset has integrated keys for PA and crew calls.

A

In order to optimize the handling of the handset and to minimize problems with low level announcements, use the handset like a normal telephone handset.

282
Q

INTERPHONE POLICY

A

Cabin Crew should not hold the handset upside-down during announcements. Used upside-down the sensitivity of the handset is the least. The output level as well as the effect of the noise-cancelling feature is reduced.

Announcements can be hardly heard in the cabin or may be impossible to understand.

Do not stretch the handset cord over 2 meters (80 inches). This may cause damage to the cord supports at both ends of the cord and will lead to handset malfunction.

In order to avoid problems with broken housings, place the handset on the support bracket and push it gently to “click” it into its correct position. This way the handset will stay in its position under normal conditions.
If not placed correctly in the support bracket, the handset may fall out of its cradle, onto the cabin floor, and will be damaged.

283
Q

Normal Call from The Cabin to the Flight Deck

A

Diall “CAPT”

Indications In The Flight Deck:
ATT light flashes on the Audio Control Panel
buzzer sounds - This buzzer is inhibited during take-off and landing.

284
Q

Emergency Call From Cabin To The Flight Deck

A

Hook off the handset.
Dial “ EMER CALL”

Indications in The Flight Deck:
1. ATT light flashes on the Audio Control Panel
2. The EMER CALL and the EMER ON p/b lights flash on the overhead panel.
3. Three long buzzer sounds - This buzzer is inhibited during take-off and landing.

285
Q

Cabin Crew to Cabin Crew Calls
FWD L (L1) Calls AFT L (L4) Attendant

A

Hook off the Handset.
Dial “INTPH + 4/AFT ATTND”

Indications at AFT L (L4) Station:
1. Chime - 1 Hi-Lo.
2. ACP – Red Steady Light Illuminated at the respective ACP.
3. AIP – Green Steady Light illuminated with the text message “CALL FWD L “.

286
Q

ALL ATTN Call p/b must only be used for receiving arming /disarming checks and for emergency purposes as it activates a buzzer in the flight deck.

A

After hooking off the handset at the called station a communication link is established.
To reset the call place the handset back into the cradle or press RESET button on the handset.

287
Q

There are two kinds of priorities for interphone calls:

A
  1. functional priorities
  2. source priorities.
288
Q

The possible functions have different priorities, that means that every selected function overrides a function with a lower priority.

A

LEVEL
FUNCTION
1
Emergency Call
2
Calls from the Cockpit
3
All Attendant Call
4
Normal Call

289
Q

The sources also have different priorities, that means that e.g. a source with a higher priority interrupts a link to an interphone station with a lower priority. A source with a lower priority and a selected function with a higher priority also interrupts an existing link.

A

LEVEL
SOURCE
1
AMU (Cockpit Audio Equipment)
2
Cockpit Handset
3
Cabin Handsets

290
Q

Pre Flight Check Interphone

A

SCCM makes an ALL Attendant Call. Each Cabin Crew to answer the call and report the serviceability of
the interphone.

291
Q

It provides adequate sound levels at each passenger seat through loudspeakers. In addition, one loudspeaker is installed in each lavatory and galley area.

A

passenger address system

292
Q

Passenger address volume increases automatically as soon as an engine is running and in case of depressurisation.

A

The PA can be operated from all attendant handsets.
Announcements from the flight deck or the cabin are broadcasted through the loudspeakers located in the cabin, lavatories and attendant stations.

293
Q

The Flight Deck can monitor the PA announcements in the cabin via the AMU by pushing the PA reception knob on an AUDIO SELECTOR PANEL (ASP).

A

Turning this knob clockwise or counterclockwise controls the volume of the announcement. Selecting another function stops the PA MONITORING procedure.

294
Q

DIRECT PA

A

PTT
Handset - All LS*

295
Q

PA ALL

A

PA+ALL
Handset - All LS* in the cabin

296
Q

PA FWD

A

PA+1/FWD
Handset - All LS* in the FWD cabin

297
Q

PA AFT

A

PA+4/AFT
Handset - All LS* in the AFT cabin

298
Q

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

A

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

299
Q

A PA source with a higher priority interrupts a PA announcement from a source with a lower priority. Only the announcement from the source with the higher priority is heard. The sources have the following priority levels:

A

LEVEL
SOURCE
1
Boom Set, Oxygen Mask (AMU)
2
Cockpit Handset (HS)
3
Purser Handset (HS)
4
Attendant Handset (HS)
5
Prerecorded Announcement (PRAM)
6
EVAC Signalling Tone
7
Video or Entertainment Sounds (VCU)
8
Boarding Music

300
Q

Level 1 has the highest and

A

level 8 the lowest priority.

301
Q

To Make PA

A

Hook off the handset
- Dial “PA”
- Dial “ALL”
In all the other AIP the text message “PA ALL IN USE” is displayed.
Press PTT (push to talk button) and PA announcement can be performed.

302
Q

Reset Of Selected PA Functions

A

Hooking the handset to the cradle or pushing the RESET button on the handset cancels a PA function initiated by the handsets functional keys.
If a function is initiated by pushing the PTT button, the release of this button cancels the function

303
Q

Flight deck PA takes priority over Cabin Crew PA.

In the case of LOW CABIN-PRESSURE or ENGINE ON the volume of a PA announcement increases automatically

A

If the PA is made from the FWD attendant station, then the FWD galley area speakers will be muted and the AFT galley area speakers will work and vice-versa. This is due to the fact that the FWD galley area speakers are located very close to FWD attendant handset and if they are not muted, then they will induce feed back in handset and a howling/whistling sound will be heard in all speakers.

304
Q

Preflight Check of PA

A

As part of the pre-flight checks the serviceability of the PA system must be checked from every interphone. Any discrepancy must be reported to the SCCM, who in turn will inform the PIC.
The PA can be operated from all attendant handsets.

305
Q

A passenger call facility is provided and accessible from each passenger seat through the __ and in each lavatory by means of a p/b located on the __

A

PSU (Passenger Service Unit)
LSU (lavatory Service Unit).

306
Q

Passenger Call from The Cabin 1. Attendant Call p/b - pressed

A

a. Chime - 1 Hi chime.
b. Passenger seat – The seat row numbering light illuminates. c. ACP - Steady Blue light illuminates at respective ACP.
d. AIP - passenger seat row displayed (eg. text message 16L or 16R) in the respective AIP

307
Q

Passenger Call Cabin - AIP Indication

A

Reset is achieved by pressing the Attendant call p/b again

Push the CALL RESET push button(on the FAP (in the CAN SETTINGS menu of the SEAT SETTING menu).

It is possible to inhibit the HI chime by pushing the CHIME INHIBIT key on the SEAT SETTING page of the FAP. This key is part of the CABIN SETTINGS menu on the page. To reset the inhibit function push the CHIME INHIBIT key again.

308
Q

Passenger Call From Lavatory
Call Button –pressed

A

Indications in the Cabin are:
A. Chime - 1 Hi chime (via respective cabin and C/A loudspeakers). B. Call button in the toilet on the LSU illuminates.
C. ACP - Steady Amber light illuminates at respective ACP.
D. Outside the respective toilet the Amber Lav call light illuminates steady.
E. AIP - Text message indicating the Lavatory from which the passenger call is initiated is displayed.

Note: Reset is achieved by pressing the Call button in the lavatory again

309
Q

Preflight Check in the Lavatory `Pax Call Button

A

Random passenger call tests should be performed in each Cabin zone. To ensure that the buttons are functional and correct indications are displayed in the cabin.

310
Q

Cabin Crew will leave the aircraft by the exit adjacent to their emergency seating position, if available.

A

If any exit is blocked the first alternative is always the opposite exit.

311
Q

AIR-CONDITIONING SYSTEM

A

The engines or the APU supply the A/C with fresh air. This air is controlled for pressure, temperature and humidity to ensure the comfort of the passengers. A certain part of the used air is mixed with the fresh air by mixer units. The rest of the used air is discharged overboard.

312
Q

Cockpit Air-Conditioning

A

The air for the cockpit is delivered from the under floor mixer unit into the cockpit distribution lines, which supply the different cockpit air outlets.
The used air is extracted through grills at the bottom of the cockpit.

313
Q

Cabin Air-Conditioning

A

The air for the passenger cabin is delivered from the under floor mixer unit into the cabin distribution lines, which supply the different cabin air outlets.
The cabin air is distributed through cabin outlets (above and below the Overhead Lockers) and passenger individual air outlets. The PASSENGER SERVICE UNITs (PSUs) below the Overhead Lockers have passenger individual air outlets. Each air outlet is individually adjustable for flow direction and flow rate (0% to 100%).
The used air is extracted through panels near the cabin floor.

To control the cabin temperature individually, the cabin is divided into two areas (AREA 1 (FWD) and AREA 2 (AFT)).

314
Q

Galley Ventilation

A

Some galleys have air outlets in their upper part. The air outlets are connected to the cabin air distribution system. The air outlets are adjustable for the flow direction, and they are closed by turning them into the closed-position. Through connections inside of the galley, the used air is extracted and completely discharged overboard.

315
Q

Lavatory Ventilation

A

Cabin air enters the lavatory through the grills in the door and through the air outlet on the LAVATORY SERVICE UNIT (LSU). The air outlet is adjustable for flow direction and flow rate (0% to 100%).
Through the grill in the lavatory ceiling, the used air is extracted and completely discharged overboard.
Behind the grill in the lavatory ceiling, a SMOKE DETECTOR is installed to monitor the extracted air. If there is smoke in the extracted air, a visual and aural (audio) alert comes on

316
Q

Exit Seats

A
  • 12 ABC, 12 DEF
  • 14 ABC, 14 DEF
317
Q

Inoperative Door, Slide, Over wing Exit Or Slide Ramp

A

The PIC will refer to the Minimum Equipment List - MEL. The PIC will then brief the SCCM on the necessary actions to perform before any departure with inoperative exits and escape equipment. The SCCM will confirm with the PIC that the aircraft has been prepared as briefed.

318
Q

Location for a Suspect Device

A

The Least Risk Area on the aircraft is centre of the R4 door.
The R4 door must be disarmed on PIC’s command in the event of a Bomb Threat.

319
Q

Oxygen in Flight Deck

A

Gases
FW CARGO HOLD

320
Q

Oxygen in Cabin

A

Solid chemical generator

321
Q

PA volume increases

A

Decompression
Engine is on

322
Q

When medical assistance is required on board the aircraft,

A

the PIC bears the ultimate responsibility for the actions of the crew.

323
Q

It is the __ responsibility to keep the PIC informed at all times and thier decisions are based on the available information.

A

Cabin Crew’s

324
Q

When voluntary medical assistance is required from passengers,

A

all reasonable measures must be taken by the Cabin Crew to identify the professional status.

325
Q

Under the circumstances the first crew on the scene ___ should assess and deal with the situation and also call for assistance either verbally or by using the call bell.

The second crew ___ will inform the Senior Cabin Crew Member (SCCM) of the nature/severity and location of the incident and collect the appropriate medical equipment, i.e. EMK, Aero-Medic First Aid Kit (after seeking PIC’s permission) and return to the scene.

The ___informs the PIC as quickly as possible, makes a PA for a medical qualified practitioner.

A

(the Assessor)

(the collector)

Senior Crew Member (Teller)

Flyadeal Training (12 decks)

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