Corendon Aircraft Type Specific PDF

Page CCOM – 05-1 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0...

Page CCOM – 05-1 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 TABLE OF CONTENTS CHAPTER 5 – AIRCRAFT TYPE 05- AIRCRAFT TYPE SPECIFIC.......................................................................................................................................... 3 05.01- SPECIFICATIONS.............................................................................................................................................. 3 (05.01.01)- Auxiliary Power Unit (APU)................................................................................................................. 4 (05.01.02)- Electrical Power................................................................................................................................... 4 (05.01.03)- Air Conditioning and Pressurization.................................................................................................... 4 (05.01.04)- IFE (In Flight Entertainment)............................................................................................................... 4 05.02- CONFIGURATION............................................................................................................................................ 5 (05.02.01)- Passenger Seating............................................................................................................................... 6 (05.02.02)- Overhead Stowage Bins...................................................................................................................... 6 (05.02.03)- Passenger Service Units and Oxygen System...................................................................................... 7 05.03- CABIN DOORS................................................................................................................................................. 8 (05.03.01)- Opening Doors – Normal Operation.................................................................................................. 9 (05.03.02)- Closing Doors.................................................................................................................................... 11 (05.03.03)- Exterior Operation of Doors.............................................................................................................. 12 05.04- ARMING AND DISARMING ESCAPE SLIDES................................................................................................... 13 05.05- EMERGENCY OPERATION OF DOORS........................................................................................................... 15 (05.05.01)- Escape Slide Specifications................................................................................................................ 15 (05.05.02)- Deployment of Slides........................................................................................................................ 16 (05.05.03)- Using Slides for Ditching................................................................................................................... 16 05.06- EMERGENCY EVACUATION ROUTES............................................................................................................. 18 (05.06.01)- Slide Length, Width and Doorsill Height........................................................................................... 19 (05.06.02)- Usable Exits....................................................................................................................................... 20 05.07- OVER WING EMERGENCY EXITS................................................................................................................... 21 (05.07.01)- OW Escape Ropes............................................................................................................................. 23 05.08- CABIN CREW STATIONS................................................................................................................................ 24 05.09- CABIN LIGHTING SYSTEM............................................................................................................................. 25 05.10- CABIN COMMUNICATION SYSTEM............................................................................................................... 30 05.11- GALLEYS........................................................................................................................................................ 33 (05.11.01)- Galley Power, Circuit Breakers and Power Jacks.............................................................................. 33 (05.11.02)- Potable Water................................................................................................................................... 33 (05.11.03)- Galley Waste Containers................................................................................................................... 34 (05.11.04)- Galley Sinks....................................................................................................................................... 34 (05.11.05)- Galley Water Shut-off Valve.............................................................................................................. 34 (05.11.06)- Service Trolleys................................................................................................................................. 34 (05.11.07)- Coffee Makers / Water Heater (Boiler)............................................................................................. 35  Page CCOM – 05-2 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.11.08)- Ovens................................................................................................................................................ 35 (05.11.09)- Galley Curtains.................................................................................................................................. 35 05.12- LAVATORIES.................................................................................................................................................. 36 (05.12.01)- Lavatory Doors.................................................................................................................................. 37 (05.12.02)- Water Heaters................................................................................................................................... 38 (05.12.03)- Water and Waste System.................................................................................................................. 38 (05.12.04)- Water Drain and Shut off Valves....................................................................................................... 39 05.13- FLIGHT DECK................................................................................................................................................. 40 (05.13.01)- Flight Deck Video Surveillance System............................................................................................. 40 (05.13.02)- Flight Deck Door................................................................................................................................ 40 (05.13.03)- Flight Deck Windows......................................................................................................................... 41 (05.13.04)- Flight Deck Seats............................................................................................................................... 43 05.14- INTERNAL DOORS AND CURTAINS................................................................................................................ 44  Page CCOM – 05-3 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05- AIRCRAFT TYPE SPECIFIC 737-Flight Attendant Manual / AMC3 ORO.MLR.100 05.01- SPECIFICATIONS B737 800 Range - 4,600km (with max. pax) Speed - 844 km Max. operating altitude - 41,000 ft (12,497m) Pax seating capacity - 189 economy Crew - 1 PIC, 1 FO, 6 CCMs  Page CCOM – 05-4 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.01.01)- Auxiliary Power Unit (APU) 737- Flight Attendant Manual An APU is mounted in the tail of the airplane. The APU is a gas turbine engine capable of operating both in the air and on the ground. On the ground, the APU provides the electrical power and bleed air necessary to operate the airplane systems, if external ground services are not available. In flight, the APU is capable of serving as a back-up for the engine bleed air system up to 17,000ft. (05.01.02)- Electrical Power 737- Flight Attendant Manual The electrical power system supplies 115-volt AC and 28-volt DC electrical power to the airplane. On the ground, power can also be provided by the APU or by external power carts. If one or more generators is to lose power, electrical power in the galleys are shut off automatically. (05.01.03)- Air Conditioning and Pressurization 737- Flight Attendant Manual Normally, bleed air for air conditioning and pressurization is supplied by the turbofan engines, mounted under the forward section of the wings. The APU can also be used to supply bleed air. Cabin temperature is controlled by the flight deck. Temperature is controlled separately for the flight deck and for the passenger cabin. (05.01.04)- IFE (In Flight Entertainment) 737- Flight Attendant Manual Some aircraft’s in our fleet have an In-flight entertainment system that can be used for boarding music, passenger safety briefing films, air map and other movies or promotional entertainment films. Controls for the IFE are located on the system itself. The IFE system is mounted in the FWD or AFT section of the cabin. The use of IFE must be established by the SCCM before flight, ensuring that the system is turned off for taxi, take-off, and landing, except for showing safety briefing prior to take-off.  Page CCOM – 05-5 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.02- CONFIGURATION 737- Flight Attendant Manual B737 800 Flight Deck Lavatory Galley Station Section A - seats 1-11 Section B - seats 12-22 Section C - seats 23-33 Lavatory Station Station Galley  Page CCOM – 05-6 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 4.0 Rev Date 15 July 2024 (05.02.01)- Passenger Seating 737- Flight Attendant Manual The B737 800 cabin configuration consists of 189 economy class passenger seats. Each seat has its own reading light and reading light control switch located in the Passenger Service Unit (PSU). An attendant call button is also installed at each PSU. On all aircrafts, the seats are 6 abreast, 3 on either side of the aisle. All passenger seats are equipped with seats belts. The aisle armrests are fixed, however on certain seats provided for PRM passengers armrests may be tilted up. The passenger seats located at the over wing emergency exits do not recline, in order for a safer evacuation route. All seats are equipped with a restraint bar at floor level that prevents passengers from stowing hand baggage under their own seat. This restraint bar also prevents baggage from moving forward. All baggage must be placed under the seat in front of each passenger or in the overhead compartments. (05.02.02)- Overhead Stowage Bins 737- Flight Attendant Manual Above the passenger seats are overhead stowage bins which run the length of the cabin. They are used to store baggage, blankets, pillows, and sometimes emergency and safety equipment. Each bin has a placard stating its maximum weight capacity. Never overload bins so that you have to force the lid to lock. In a possible hard landing or turbulence, forcible closed lids may be released and create an unsafe situation. On the Sky Interior fitted aircraft, to help crew to close bins which are fully loaded a small lever called BAM lever (Bin Assist Mechanism) is fitted to the exterior of the bin, by moving this lever down to the armed position it will make it easier to close the bin. Items that may break and leak inside the overhead bins should be removed from the bin and stored under the seat in front of the passenger or an available unit in the galley. Traditional Interior Sky Interior Standard Pivot Bins Sky Interior Bins with BAM Lever BAM Lever on Sky Interior Pivot bins  Page CCOM – 05-7 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.02.03)- Passenger Service Units and Oxygen System 737- Flight Attendant Manual The passenger service units are located beneath the overhead bins in the passenger cabin. Each unit has air vents, reading lights, a speaker, Attendant call buttons and Fasten Seat Belt and No Smoking indicators. The lighting system for the Fasten Seat Belt (FSB) and No Smoking (NS) signs are controlled by the flight deck. However, in some aircrafts the no smoking signs are stickers that indicate the no smoking regulation on board. The passenger oxygen masks are located in the overhead modular compartments. This service unit contains 1 chemical oxygen generator and 4 masks. Each lavatory and CCM station is equipped with 2 oxygen masks. No-Smoking Sticker  Page CCOM – 05-8 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.03- CABIN DOORS 737- Flight Attendant Manual The B737 800 aircraft has 4 main doors and 4 over wing exit windows, two at each side. All doors and over wing exits are considered as "emergency exits". The doors on the left are entry doors intended for normal passenger entry and exit and the doors on the right are service doors. Left doors are referred to as L1 (FWD door) and L2 (AFT door). Right doors are referred to as R1 (FWD door) and R2 (AFT door). All doors can be opened from the inside and outside. They are inward-outward opening plug type doors. The doors operate on two hinges and have four roller-type latches for positioning and locking. The two forward doors are slightly more curved in their structure and somewhat more difficult to open and close. If the door is not closed properly, a warning light in the flight deck indicates that the door is unlocked. In such cases the PIC will inform the SCCM that the relevant door needs to be opened and closed again. The over wing exits are canopy type exits that are held in place by mechanical locks. Once opened they automatically extend upwards, against the fuselage. The door handle is located on the door itself. Each door has a small window with a red Slide Safety Strap above it. All doors are single width doors with a single lane escape slide stowed in a container on the lower part of the door. The pressure of the slide can be checked through a viewer in the slide container. CCMs are responsible for checking the pressure before each departure. The gauge indicator must be in the green band. Each door has a Door Warning Strap attached adjacent to the door.  Page CCOM – 05-9 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Pre-flight Check of Main doors 1. Slide pressure gauge indicator in the green range or towards a higher pressure to the right of the green mark. 2. Slide safety strap (red flag) operative. 3. Clear visibility from viewing window. 4. Slide girt bar attached on the slide container (disarmed position) 5. Girt bar floor brackets operative. 6. Door hinge release handle operative. 7. Door warning strap operative. (05.03.01)- Opening Doors – Normal Operation 737- Flight Attendant Manual  Page CCOM – 05-10 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 All doors open by rotating the handle up and aft and pushing out and forward until the door automatically locks against the fuselage. To open the door: 1. Rotate the door handle in the direction of the arrow, 2. The door unlocks and moves slightly, 3. Then push the door outboard to the open position until locked against the fuselage. An open door shall not be left unattended. The ‘Door Warning Strap’ should be attached to the door hinge if it is necessary for the crew member to leave the area for a short period. All doors can be opened without stairs or a bridge for ventilation or technical requirements. In such cases, use extreme care. The door must be secured with a door warning strap and guarded by a cabin crew member at all times.  Page CCOM – 05-11 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.03.02)- Closing Doors 737- Flight Attendant Manual After the door is open and is locked against the fuselage, the door must be released prior to closing. This is accomplished by pushing the door hinge release handle down and pulling the door to the closed position. 1. Press down / up on the door hinge release handle, 2. Grasp the assist handle and start pulling the door to the closed position, 3. Release the door hinge release handle after rotating the door a few degrees and pull the door until the door handle begins to rotate in the opposite direction of the arrow, 4. Grasp the handle and continue to rotate until the door is closed and locked.  Page CCOM – 05-12 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.03.03)- Exterior Operation of Doors 737- Flight Attendant Manual All doors can be opened and closed from the outside. To open from outside: 1. Check that the slide is disarmed (slide safety strap not visible from outside) 2. Pull handle out, 3. Rotate in direction of arrow, 4. Door moves slightly inwards, 5. Pull door outwards until open and locked against fuselage. To close from outside: 1. Push door release handle down / up to unlock door, 2. Rotate door inwards to close, 3. Rotate handle in opposite direction of arrow until fully closed, 4. Push handle in.  Page CCOM – 05-13 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.04- ARMING AND DISARMING ESCAPE SLIDES 737- Flight Attendant Manual All doors are equipped with escape slides located in a container on the lower part of the door. They must be armed (ready for deployment position) before flight and disarmed (safety position) after flight. The slide is equipped with a girt bar, normally stowed in retainer hooks on the slide container. Prior to each flight the slide must be armed. The slide is armed by; removing the girt bar from the hooks on the slide container and fastening it to the brackets on the floor directly in front of the door. To disarm the slide, the girt bar is removed from the floor brackets and placed in the retainer hooks under the slide container. Above each door window there is a Slide Safety Strap. The strap must be places ;  across the window when the slide is armed and  above the window when the slide is disarmed. Floor brackets REMEMBER! If the girt bar is in the floor brackets, the escape slide is in the ARMED position, If the girt bar is in the retainer hooks under the slide container, the escape slide is in DISARMED position.  Page CCOM – 05-14 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Procedure for ARMING slides 1. Place Slide Safety Strap across window. 2. Place girt bar into the floor brackets Procedure for DISARMING slides 1. Remove girt bar from floor brackets and place into the hooks under the slide box 2. Place Safety Strap above window.  Page CCOM – 05-15 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.05- EMERGENCY OPERATION OF DOORS 737- Flight Attendant Manual CCMs shall, upon hearing the command to evacuate the aircraft: 1. Check outside conditions for hazards, 2. Check that girt bar is secured to the floor brackets, 3. Rotate handle in direction of arrow, 4. Push door out forcibly until escape slide is released from its container and deploys, 5. Grasp assist handle and pull red manual inflation handle completely free and discard. (05.05.01)- Escape Slide Specifications 737- Flight Attendant Manual Each cabin door is equipped with a single lane escape slide. All slides are 508 cm in length and 153 cm in width when deployed. The slide inflates in about 4-6 sec. depending on conditions (such as cold and winds). The inflation system consists of a pressurized cylinder filled with either gaseous Nitrogen, or a mixture of gaseous CO₂ and Nitrogen. Re-entry straps are available on the sides of the escape slides. These may be used to enter the aircraft after an evacuation if necessary.  Page CCOM – 05-16 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 4.0 Rev Date 15 July 2024 (05.05.02)- Deployment of Slides 737- Flight Attendant Manual 1. Open the door with the escape slide in the "Armed Position", 2. Pull manual inflation handle so as not to lose time in case of failure. The manual inflation handle is always placed on the right side of the slide at floor level. The manual inflation handle is not fixed in its place, once pulled, throw it away. Caution! If the slide does not inflate, direct passengers to other usable exits. (05.05.03)- Using Slides for Ditching 737- Flight Attendant Manual The possibility of a ditching is remote, but as long as the possibility exists, complete knowledge of procedures and equipment is necessary. Ditching studies indicate that with an aft centre of gravity and high gross weight, the aft doors will be just below the water level. Opening the aft doors would seriously degrade the flotation characteristics of the airplane and therefore, it is imperative that the aft doors are NOT opened during a ditching. The remaining forward cabin doors and overwing exits will provide sufficient ditching capability. Outside conditions must be observed through the window before the FWD doors are opened. If the water level is above the doors, passengers shall be redirected to usable exits, in this case the OW exits. If the fwd doors are above water level slide shall be inflated in the normal manner. Pull the detachment handle after deploying the slide so that a space between the slide and aircraft is available for passengers to jump into the water.  Page CCOM – 05-17 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Escape slides are detached from the aircraft by use of a detachment handle located under the girt bar flap. After the detachment handle is pulled, the slide remains attached to the aircraft by means of a mooring line. The mooring line automatically separates to prevent damage to the slide if the aircraft sinks. The mooring line separates automatically when approximately 350 lbs (159 kg) of force is applied to the mooring line. To manually disconnect the mooring line from the aircraft, pull the quick release handle (pin) located at the side closest to the slide. Escape slides must be turned upside down after the evacuation so they may be used as flotation devices. Passengers may support themselves by holding onto the straps along the sides of the slide, PRM, injured, pregnant, elderly passengers and children / infants may be seated in the slides. Remember that if the total weight of these passengers exceed 350 lbs (159 kg) the mooring line will snap.  Page CCOM – 05-18 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.06- EMERGENCY EVACUATION ROUTES 737- Flight Attendant Manual Emergency evacuation may be accomplished through four entry / service doors and four over wing emergency exits. Flight deck crew members may evacuate the airplane through two sliding flight deck windows.  Page CCOM – 05-19 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 4.0 Rev Date 15 July 2024 (05.06.01)- Slide Length, Width and Doorsill Height 737- Flight Attendant Manual Slide Length Slide Width Door Sill Height – all landing gears down Slide Location (approximate) (approximate) (approximate) B737-800 B737-800 B737-800 L1 and R1 508cm 153cm 266cm L2 and R2 508cm 153cm 292cm  Page CCOM – 05-20 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.06.02)- Usable Exits 737- Flight Attendant Manual On Land All Slides are usable whatever the attitude of the aeroplane. Low angled slides may be used as ramps to run down. Ditching Over wing exits are primary exits in ditching. DO NOT use L2 and R2 doors.  Page CCOM – 05-21 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.07- OVER WING EMERGENCY EXITS 737- Flight Attendant Manual There are 4 emergency over-wing (OW) exits in the passenger cabin of the B737-800. These exits are Type III canopy windows, held in place by mechanical locks. The OW exits can be opened from either inside or outside of the aircraft by a spring loaded handle at the top of the window. A 28 Volt DC flight lock system automatically locks the over-wing doors during take-off and landing and while the airplane is inflight to protect against inadvertent and intentional opening of the exit. The system unlocks the over- wing doors on the ground to allow for opening in emergency situations. Commands for the flight lock to lock and unlock are dependent upon engine speed, thrust lever position, air / ground mode status, and the open / closed status of the doors. Interior Handle: 1. Pull handle down and inward, 2. Door opens out and up automatically, 3. Exit as follows: "Leg-Body-Leg."  Page CCOM – 05-22 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Exterior Opening: To open an over-wing exit from the exterior: 1. Hold knee against lower portion of door 2. Push in Panel, 3. Exit opens out and up automatically. Closing Strap: Straps used for closing the OW exit. B737-800 1. Interior Handle 2. Closing Strap  Page CCOM – 05-23 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.07.01)- OW Escape Ropes 737- Flight Attendant Manual In the B737 800, the aft OW exits are equipped with escape ropes (straps) located inside the upper frame. The ropes are exposed after the exits have been opened. One end of the escape rope is attached to the exit frame. The remainder is stowed in a tube extending into the cabin ceiling. To use, the strap is pulled free from its stowage and attached to a D-ring on the top surface of the wing. In a ditching situation, the escape strap can be used as a hand hold for passengers to walk out on the wing and help stay on the surface.  Page CCOM – 05-24 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.08- CABIN CREW STATIONS 737- Flight Attendant Manual Stations are located at the forward passenger entry door, aft passenger entry door, and aft service entry door. The station seats (jump seats) are designed to automatically return to the stowed position when not occupied. A combination seat belt / shoulder harness with single point release is incorporated into the seat. The shoulder harness is adjustable with a single-point release from a single buckle and retracts into a stowed position when not in use. The buckle has a release plate that must be turned 90 degrees to release the harness. Under turbulent air conditions where rapid airplane movement is expected, failure to firmly connect and properly adjust the cabin crew harnesses may result in personal injury. The station harness must remain unfastened when not in use to allow for quick access. Left stations have an Attendant Control Panel (ACP) with work lights and interphone / PA system. On some aircraft an interphone system is also available at the AFT right stations. Emergency equipment have been mounted close to stations. A service unit containing two (2) oxygen masks are located above each cabin crew station. Pre-flight Station Check  Seat returns to stowed position.  Seat belt / shoulder harness retracts and buckle is operative.  Interphone / PA system operative.  Availability of following items in unit under the seat: - Checklists - MRT - LV - Flash light  Availability of other emergency and safety equipment listed on the station Emergency Equipment Checklist.  Page CCOM – 05-25 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.09- CABIN LIGHTING SYSTEM 737- Flight Attendant Manual GENERAL LIGHTING Ceiling and Window Lighting Ceiling and window lighting is independently controlled, and can be adjusted to: Night-Off-Dim-Medium-Bright (ceiling lights) and Off-Dim-Bright (window lights). The controls are located on the forward ACP. Entry Lights Door entry lights are provided with individual controls at both L1 and L2 control panels. Entry lights illuminate the threshold of each door. The 3 selectable positions are Off-Dim-Bright. Crew Work Lights Crew work lights illuminate cabin crew jump seats. These switches must be off for take-off and landing. Galley Lights Galley lights are controlled in each respective galley. They illuminate the galley work area. Type 1 ACP FWD ACP AFT ACP  Page CCOM – 05-26 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Type 2 ACP When "Lighting" is selected on the screen: - The screen displays available and selected lighting scenes for the passenger seating and entry areas. The Sky Interior AFT ACP also has the same lighting function.  Page CCOM – 05-27 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 EMERGENCY LIGHTING Interior emergency lighting is provided at each cabin door, over-wing exit, cabin ceiling and floor and in the flight deck. Exterior emergency lighting is provided over each wing and above all exits. When the switch is in the ‘Armed’ mode in the flight deck, the lights switch on automatically when power fails. Flight crew can switch the lights on manually. The lights may be switched on from the FWD or AFT CCM panel (depending on aeroplane type). The switch in the cabin overrides the flight deck switch. The guard over the CCM switch in cabin is red or transparent in colour. Emergency lights last for 15 minutes once they are switched on. The exit lights / signs are located in the aisle or bottom edge of passenger seats, overhead bins, above and below exits and on galley and cabin ceiling. Some aircrafts have photo luminescent strips installed along the cabin aisle instead of bulbs. These strips absorb light and gradually dissipate this energy by glowing. Emergency Light Control Switch  Page CCOM – 05-28 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 B737-800 Interior and Exterior Emergency Lights  Page CCOM – 05-29 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022  Page CCOM – 05-30 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.10- CABIN COMMUNICATION SYSTEM 737- Flight Attendant Manual INTERPHONE AND PA SYSTEM The B.737-800 cabin interphone and passenger address (PA) system is a phone network between CCM stations and the flight deck. The handset is used to make calls between flight deck-cabin, cabin-cabin and also to perform announcements.  Press 2 once to call the flight deck.  Press 5 twice to call a CCM station.  Press 2 three times to alert the Pilot, + 5 immediately after to inform all other CCMs of the alert call to the cockpit.  To make an announcement remove the handset from the cradle, press 8 and push the PTT (push to talk) button while speaking.  Press the re-set button after each use before placing the handset back into its place.  Page CCOM – 05-31 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 MASTER CALL SYSTEM A master call light panel is installed in the fwd and aft ceiling of the passenger compartment. The lights on the panel illuminate when a call has been made. The different coloured lights help verify the call.  Passenger call / Blue light (HI chime)  Lavatory call / Amber light (HI chime)  Flight Deck call / Pink or Red light (HI-LO chime)  Cabin Crew call / Pink or Red light (2 x HI-LO chime) The master call panel also has ‘EXIT’ signs showing the nearest exits.  Page CCOM – 05-32 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 PASSENGER CALL SYSTEM There is one attendant call switch and call light installed at each PSU. A call from the passenger seating area is made by pushing the ATTENDANT CALL button located in the Passenger Service Unit.  Pushing the button:  illuminates the attendant call light located on the PSU  illuminates the blue passenger call light at the associated forward or aft master call light panel sounds a single HI chime. The attendant call light is reset by pushing the attendant call switch in the PSU where the call originated. LAVATORY CALL SYSTEM A call from the lavatory is made by pushing the ATTENDANT CALL switch located on the inboard wall above / near the lavatory sink cabinet. Pushing the switch:  illuminates the lavatory call light / reset switch located on the outside wall of the calling Lavatory  illuminates the amber lavatory call light at the associated forward or aft master call light panel  sounds a single HI chime. The lavatory call light is extinguished by pushing the lavatory call light / reset switch on the outside wall of the calling lavatory. This reset:  extinguishes the call light outside wall of the lavatory.  extinguishes the amber lavatory call light on the associated call light panel if there are no other active lavatory calls for that area.  Page CCOM – 05-33 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.11- GALLEYS 737- Flight Attendant Manual Galleys are installed in the passenger cabin to provide service to the passengers. Generally, they are located adjacent to the FWD and AFT galley service doors. Galleys have provisions for storing and preparing food and beverages. Removable containers and / or trollies (carts), which latch into the galley units, are used for replenishment of supplies, food, beverages, and waste storage. Some galleys are equipped with electrical power and water services. Water is supplied to the galleys from the airplane pressurized water system and, in an emergency, may be shut off at the galley. Lighting controls are located on the galley electric panel. A galley vent system keeps the air fresh. B737-800 (05.11.01)- Galley Power, Circuit Breakers and Power Jacks 737- Flight Attendant Manual Power for the galley is available only if the galley power switch in the flight deck is "ON". In flight, with the loss of one or more generators, galley electrical power is automatically shut off. All galleys have circuit breaker panels for ovens and water heaters. If a circuit breaker needs to be reset during flight, the PIC must be informed before doing so. Each circuit breaker can be reset once only. If the same circuit breaker fails a second time, inform the flight deck and do not use the equipment it assists. Maintenance must be informed. A jack (power point) is available in each galley. They are to be used by cleaners only, it is forbidden for crew and passengers to use the jacks. (05.11.02)- Potable Water 737- Flight Attendant Manual A pressurized water system provides potable water for galleys and lavatories. Hot and cold water is supplied to the lavatories. Cold water is supplied to the galley units that have water. The water supply line to each galley and lavatory includes a shutoff valve that is accessible during flight. Water is not available while the tanks are being serviced. The B737 800 water tanks are under the cabin floor in the aft cargo section and have a capacity of 60 gallons (227.1 litres).  Page CCOM – 05-34 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 4.0 Rev Date 15 July 2024 (05.11.03)- Galley Waste Containers 737- Flight Attendant Manual Galleys are equipped with waste containers. Check that waste bags have been placed into them container and that the waste lid operates / sits securely closed before each flight. Do not pour liquids into galley waste containers and do not over fill them with waste. (05.11.04)- Galley Sinks 737- Flight Attendant Manual Do not dispose of liquid and solid waste materials (coffee grounds, tea bags, fruit pulp, and so on) in the sinks. A small amount of liquid may be poured into the toilets. Solid waste materials must be placed in the galley waste containers. Do not remove the sink strainer. Cabin crew are not allowed to open / close any drain valves related to galley equipment. (05.11.05)- Galley Water Shut-off Valve 737- Flight Attendant Manual Each galley is equipped with a water shut-off valve. If the water cannot be turned off in any of the galley fixtures, such as the water faucet, coffee maker or water boiler, positioning the water shut off valve to "OFF" turns off the water to that galley. (05.11.06)- Service Trolleys 737- Flight Attendant Manual Service trolley brakes, wheels and locks shall be checked to ensure they are operative before each flight. If any of these items are inoperative, (including trolleys whose brake mechanism is coloured blue (instead of green), as indicated in the picture below), the Caterer shall be told to off-load the trolley and replace it with a safer one. The number of trolleys shall not exceed the number of inflight trolley restrains available. Trolleys that are stowed without support are a threat to flight safety. Cabin crew must ensure trolleys are stowed correctly according to galley layouts, no single trolley should be stowed in a double stowage if there is no divider in place. In addition, no single half trolley should be stowed in a double trolley stowage alone. Pay attention to the placards in the respective galleys. All trolleys must be restrained in their respective storage areas during taxi, take-off, landing, emergencies, severe turbulence and whenever not in use during all phases of flight. Trolleys shall not be left unattended in the cabin during passenger services and brakes shall be engaged while serving passengers. If during flight a trolley becomes inoperative, the SCCM shall label it with an Out of Order sticker, ensure it is stowed away securely and not used again by the crew during passenger services for the entire flight. In the galley unit, trolley compartments have a ‘Maximum Capacity’ label. In addition, there may also be a label indicating that two adjacent BLUE Brake Mechanism compartments MUST have installed a trolley in each compartment or none (instead of GREEN) at all. REFER TO PICTURES ABOVE  Page CCOM – 05-35 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.11.07)- Coffee Makers / Water Heater (Boiler) 737- Flight Attendant Manual The circuit breakers and on / off switches of boilers are checked before each flight. Boilers are to remain off during take-off and landing and they shall not be used if the fresh water tank is empty. (05.11.08)- Ovens 737- Flight Attendant Manual The circuit breakers and on / off switches of ovens are checked before each flight. Ovens are to remain off during take-off and landing. Never place flammable items into ovens e.g. paper / plastic cups, paper towels etc. Ovens shall not be operated without oven insert. (05.11.09)- Galley Curtains 737- Flight Attendant Manual The functionality and sturdiness of curtain straps used to secure open curtains shall be checked before each flight. All curtains shall be open and secured during take-off, landing, turbulence, critical phases of flight and when all CCMs are required to be in the cabin at the same time for passenger meal services.  Page CCOM – 05-36 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.12- LAVATORIES 737- Flight Attendant Manual Each lavatory contains a toilet, wash basin, mirror, and all the necessary vanity items and disposal units. Some of the lavatories have diaper changing tables and are wheelchair accessible. The lavatories contain two oxygen masks which deploy automatically during cabin depressurization. Ventilation is provided for each lavatory and air exhausts through overboard vents. The B737 800 toilet waste system uses a vacuum to collect the waste and deposit it in the waste tank. Below 16,000ft, the waste system vacuums the waste to the tank. Above 16,000ft, the pressure difference between the cabin and outside pressure moves the waste from the toilets to the tanks. Pushing the flush button on the toilet activates the flush cycle. This cycle lasts approximately 7 seconds. Once the flush button is pushed, there is a delay for 15 secs for the system to reset before the next flush cycle can be initiated. If the vacuum system continues to work: 1. close the toilet lid, 2. pull the Manual Shut off Handle (handle only available in B737 800 variant) 3. inform PIC and 4. lock and seal lavatory as INOP. B737-800  Page CCOM – 05-37 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.12.01)- Lavatory Doors 737- Flight Attendant Manual The B737 800 lavatory doors can be locked and unlocked from the outside. 1. Lift the metal flap above the VACANT / OCCUPIED indicator, 2. Move the lock slide to the right or left to lock or unlock the door.  Page CCOM – 05-38 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.12.02)- Water Heaters 737- Flight Attendant Manual A water heater is available under the sink in each lavatory. They maintain a water temperature of approximately 52°C to 56°C. When emptied, the water is heated within a 4 min cycle. An On / Off switch and light is located on the top end of the heater. (05.12.03)- Water and Waste System 737- Flight Attendant Manual The fresh water supply has to be checked before each flight. The control panel for the 60 gallon (227.1lt) fresh water tank is located on the aft CCM’s panel. The fresh water indicator, provided there is power, continuously displays the amount of fresh water remaining in the tank. A waste system quantity indicator is also located on the aft CCM’s panel. The Press to test button is used to check the level of waste remaining in the tank. In the event the waste tank becomes full, the LAVS INOP light will illuminate and all toilets will be inoperative. There are 2 sensors attached to the upper part of the waste tank. Both sensors signal when the waste tank is full. There is also a sensor in each waste tank drain line. It provides data to the waste system indicator. The Clean / Check Sensor light illuminates if a sensor fails or is fouled, indicating system maintenance is required. The waste system is still operational when this lights illuminates, however Maintenance must be informed after flight. Type 1 ACP  Page CCOM – 05-39 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Type 2 ACP When "Environment" is selected on the screen: - The screen displays the Potable Water level, - the Vacuum waste level, - LAV INOP and - the Clean Check Sensors status button. (05.12.04)- Water Drain and Shut off Valves 737- Flight Attendant Manual In the B737-800 aircrafts, each lavatory has a water supply selector valve under the sink with 4 selectable positions. 1. Supply on - normal operating position, 2. Faucet only – water is supplied only to the faucet, 3. Toilet only - water is supplied only to the toilet, 4. Off – No water is supplied to the lavatory. A drain valve in the B737-800 is located in the FWD lavatory. It is to be operated by authorised Technicians only. FWD Lavatory water supply selector valve 1. Water Drain Valve 2. Water Shutoff Valve  Page CCOM – 05-40 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 05.13- FLIGHT DECK 737- Flight Attendant Manual A "flight deck" is the area at the front of an aircraft from which pilots control the aircraft. The flight deck of an aircraft contains flight instruments on an instrument panel, and the controls that enable the pilot to fly the aircraft. A door separates the flight crew compartment from the passenger compartment. The door has a placard indicating ‘crew only’ and a locking means to prevent passengers from opening it without the permission of a member of the flight crew. (05.13.01)- Flight Deck Video Surveillance System 737- Flight Attendant Manual A video surveillance system provides the flight crew with immediate real-time video surveillance of the area outside the flight deck entrance and between the L1 and R1 doors. A display unit displays images from three different cameras in the area near the flight deck entrance. (05.13.02)- Flight Deck Door 737- Flight Attendant Manual The flight deck door opens inwards to the cabin. The FDAS (Flight Door Access System) is checked by the captains before each flight. The door lock switch has 3 positions: - UNLKD (unlocked), AUTO and DENY. The B737 800 flight deck door can only be opened after entering the door code or if the captain unlocks it. A flight deck emergency access panel is located on the passenger side door post. Enter the access code and push the ENT button. A warning sound is heard in the flight deck. If the PIC doesn’t select DENY on the door lock switch, the door becomes unlocked within 30secs for a period of 5 secs. Panel Lights:  Red illuminates when the door is locked,  Amber illuminates, when correct access code is entered,  Green illuminates when the door is unlocked. Pull door to open. Due to flight safety the door access codes are not stated in this manual. These codes are shared during ground training courses and are discussed during the crew pre-flight briefing. If the flight deck door becomes INOP the PIC shall brief the SCCM on alternate door procedures.  Page CCOM – 05-41 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.13.03)- Flight Deck Windows 737- Flight Attendant Manual On the B737 800 aircraft there are two flight deck sliding windows that can be used as secondary escape routes. To open either window, depress the trigger and turn the handle back and inboard. After the window moves inboard, move it back until it locks in the open position. To close the window, it must first be unlocked. Pull forward on the latch mechanism rod to unlock the window. Depress the trigger and move the window forward until the handle can be turned forward and outboard. When the trigger is released, the window latches. Only the first officer’s number two window can be opened from outside the airplane. Escape Ropes: An escape rope is available for each pilot in a compartment above their seats. The rope is thrown out the window and used as an aid to exit the aircraft in an emergency situation.  Page CCOM – 05-42 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 Flight Deck Window Emergency Egress If the flight deck number two window must be used for emergency evacuation:  open the window,  open the escape strap compartment,  pull on the escape strap to ensure it is securely attached,  throw the strap out the window,  sit on the window sill with upper body outside exit in accordance with the following illustration. The illustrated method of departure would probably be the easiest for most crew members. However, this technique is difficult and should be used only in extreme emergency!  Page CCOM – 05-43 CCOM – AIRCRAFT TYPE SPECIFIC Rev No 2.0 Rev Date 15 March 2022 (05.13.04)- Flight Deck Seats 737- Flight Attendant Manual Pilot Seats The captain and first officer seats are adjustable. CCMs should be aware of the usage of following controls in case of a pilot incapacitation occurs and the pilot needs to be secured in his seat. H – allows seat to move forward and back V – allows seat height to be adjusted R – reclines seat back-rest T – tilts the knee rest cushion up and down Flight Deck Observer Seat A first observer's seat is in the aisle in front of the flight compartment door. The seat is folded up to the side when not in use. The first observer's seat includes these features:  An inertial reel shoulder harness  A lap belt  An adjustable crotch strap  A fixed headrest The flight crew is responsible for briefing the seat occupant.