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RYANAIR CONVERSION SECURITY BUZZ
PRACTICE SOLUTION 2026 SOLVED ITEMS
CONFIRMED A+
◉ Rejected Take - off. Answer: The Captain may decide to reject a take - off for various reasons. These may include conditions either inside or outside the aircraft which could affect the safe operation of the flight , e.g. technical problem , birds / animals on the runway , pilot incapacitation. ◉ Go around/ Missed approach. Answer: A Go Around is when the aircraft is on the approach to land and the Captain has decided for some reason not to land , e.g. adverse weather conditions , technical problems , runway unsuitable for landing. ◉ When will there be a significant increase of engine noise. Answer: Go around/ missed approach ◉ Tail Strike. Answer: A tail strike is said to have occurred when the lower aft fuselage or tail skid contacts the runway during take - off or landing. This is a non - normal situation that has potentially very serious consequences depending on the force of the impact. Differing degrees of aircraft damage can result from a tail strike and the integrity of the hull can be compromised to the point that the aircraft cannot remain pressurised.
◉ Any number of factors can contribute to a tail strike including :. Answer: Weather Runway conditions Pilot error. Loading error passengers not seated correctly (loading rules not followed) , or baggage and cargo incorrectly loaded into the baggage holds. LID / Loadsheet error - miscalculation of the aircraft trim. Aircraft malfunction Unstabilised approach to landing ◉ Factors that may lead Aircrew to suspect a tail strike include but are not limited to :. Answer: Collision noise, Scraping sound, Feeling of impact bump. ◉ If cc suspect a tail strike when should they informed the flight deck?. Answer: Immediately ◉ What is Incapacitation ?. Answer: This generally means that someone is being deprived of his capacity or natural power or to be rendered incapable or unfit. ◉ Use of Pilot's Checklists. Answer: There shall always be two Aircrew in the flight deck ◉ If the pilot is incapacitated what shall cc do with the first officer. Answer: CC checklist and sit in the flight deck on the middle jumpseat until the aircraft has parked after landing
◉ Material Effects of a Rapid Decompression. Answer: A loud explosive noise. Air rising towards the failure ( the hole ) carrying loose articles , papers , dust , etc. A dense fog will form in the cabin momentarily as the moisture held in the cabin condenses. Passengers may confuse this with smoke and need reassurance. This fog may cause toilet smoke detectors to activate. Hot liquids will suddenly boil over ( risk of scalding ) due to the reduced boiling point. Oxygen masks will drop down. Fasten Seat Belts sign will illuminate. ◉ Physical Effects of a Rapid Decompression. Answer: Severe ear and sinus pain. Chest and joint pain caused by nitrogen bubbles in the blood expanding Forced expulsion of air. You will feel very cold, because it is around minus 50 degrees outside. ◉ Slow Decompression. Answer: This is a gradual loss of cabin pressure, which can take more than 10 seconds to equalise with the outside pressure. Causes of a slow decompression include a hissing door seal or cracked window ◉ When will the oxygen masks drop down. Answer: The oxygen masks drop down automatically in the cabin when the cabin altitude reaches 14,000 feet. This may be your first indication that the aircraft was experiencing a slow decompression. ◉. Answer: Emergency
◉ Decompression PA. Answer: "Ladies and Gentleman, there has been a reduction in cabin pressure, keep calm, and remain seated with your oxygen mask fitted until you are instructed to remove there is no cause for alarm Please fasten your seatbelt and refrain There may be a smell of burning , however from smoking. If you need assistance , the Cabin Crew will be with you shortly." ◉ Monitoring of Passengers. Answer: Check the toilets for any incapacitated passenger. Administer first aid - go through cabin with portable emergency 02 Brief ABP's to guard the main doors. (As the aircraft is now unpressurised the doors can be opened). Brief ABP's at the overwing exists NOT to open the overwing exits unless instructed otherwise. ◉ Minimum. Answer: inflow of oxygen should be reduced to minimum by closing toilet door hatbin oven and reducing time when compartment door remains open when spraying firefighting agents )
. If fighting a confined fire , the door / compartment shall be opened only for the extinguisher nozzle to fit in - 2 - 3 cm ( 1 inch. ◉ Fire equipment. Answer: use appropriate equipment (halon / water glycol , Fire Gloves when necessary - PBE Crash Axe , metal bar box).
◉ Actions for specific fires: toilet fire. Answer: ensure nobody is inside the toilet ◉ Actions for specific fires: oven fire. Answer: close the oven door, switch oven off and pull relevant circuit breaker ◉ Actions for specific fires: overhead locker fire. Answer: in aircraft until EI - FOB (non - BSI) , open slightly the Hatbin door adjacent to the one feeling hot ; in aircraft from EI - FOC (BSI) , hot - feeling door can be opened slightly. Do not use water ◉ Actions for specific fires: fire behind panelling. Answer: crash axe to be delivered from the Flight Deck. Panelling to be lifted off or small hole to be made above the hot spot. At least 1 halon extinguisher should be fully discharged. No water shall be used ◉ Actions for specific fires: under floor fire. Answer: cover the area where smoke / fumes enter the cabin with wet materials (to minimize inflow of toxic smoke / fumes). ◉ Actions for specific fires: seat fire. Answer: any non-flammable liquid can be used to rapidly extinguish the fire. ◉ Actions for specific fires: Gash cart fire. Answer: may be caused by Dangerous Goods. Use halon to extinguish the fire.
◉ Cabin battery fire - memory items. Answer: 1. Passengers MOVE AWAY
PBE and fire gloves DON (IF REQUIRED)
Halon DISCHARGE FULLY
Repeat if necessary
Non - flammable liquid Water Glycol AS REQUIRED ◉ Features 737-800 Non BSI. Answer: No touch screen panel in the FWD and AFT CSA Panel. Adult life jackets located under passenger seats in the whole cabin. Infant Flotation devices under B and E seats with exception for rows 15-18 OR No touch screen panel in the FWD and AFT CSA Panel. Adult life jackets in the PSU , with exception for rows 1ABC and 2DEF Infant Flotation devices in PSU above B and E seats with exception for rows 1ABC , 2DEF 15- 18 ◉ Time Available Ditching drill. Answer: 1. NITS RECEIVE 2 Life jackets DON Cabin lights .. BRIGHT SOS demo COMPLETE ABPS ...... BRIEF Buddy system SET UP Infant flotation device ...................... DON Assigned area ...... SECURE Cabin preparation checklist COMPLETE Cabin secure GIVE At 2 minutes to landing. Position .. .TAKE 12. ELS .. ON ( No 2 ) At 30 seconds to landing. 13. Brace position .. HOLD
Passengers .. ....... COMMAND " Brace , brace! " After aircraft has come to complete stop. No need to wait for Captain's command as catastrophic. Jumpseat UNSTRAP No 2 / No 3 16. Outside conditions / slide armed ........... CHECK 17. Door .......... ..OPEN 18. Manual
◉. Answer: Rows 16 and 17 ◉ seats are not fitted with an IFD. Answer: IFD under the middle passenger seat row 1B , row 16B and 16E , row 17B and 17E. Row 2 will ◉ Stowage of Cabin Crew Bags. Answer: 1. Where stowage compartments have trolleys installed , CC shall stow their bags behind the trolleys.
- Where trolleys are not loaded or their combination in the compartment does not allow secure stowage of crew bags as per point 1 , CC may stow their bags in the overhead lockers as follows : No.1 and No.4 shall use locker 3 ABC , No.2 , No.3 and supernumerary Crew shall use locker 32 ABC / DEF.
- All CC will ensure their bags are stowed in approved lockers before boarding of passengers.
- Security of CC crew bags must be monitored for the duration of the flight. ◉ Where is the water shut off valve located in the fwd galley. Answer: There are two water shut off valves, one located above each boiler around eye level ◉ If the toilet sink water tap fails to shut off continuously. Answer: If the tap to the sink is continuously running then water be shut off.
Turn the WATER SUPPLY selector valve, located under the sink supply to the sink must bal to the TOILET or SHUT OFF position. ◉ Toilet Flooding. Answer: If a toilet floods due to the water rinse valve sticking open after flushing, immediately flush the toilet evacuate excess water from the toilet bowl. If the water is still flowing, shut off the water for that toilet. Turn the water supply selector to the FAUCET or SHUT OFF position. ◉ Toilet Flush Valve Fails to Reset. Answer: Close the toilet lid Pull the manual shut off handle located at the base of the toilet ◉ Assigned Door Checks. Answer: Open door - check exterior handle in place. An open door way, without airbridge or steps in place, has a safety strap attached. Door - handle is horizontal, door is flush with the fuselage and safety closed strap is stowed. ◉ Jumpseat and Area Check. Answer: Seat retracts correctly. Seat belt / harness operational. Mirrors, where fitted, provide an adequate view of the cabin from the seated position. Covers for electrical sockets are present and intact.
◉ Toilet Checks. Answer: Waste bin flap operational. Ensure water supply selector is set to SUPPLY. Flush , water and vacuum systems operate correctly , i.e. flush and vacuum systems cut out and water not overheating All stowage / compartments closed and securable Internal lights function correctly Lock toilet after checks completed to prevent unauthorised carriage of passengers PDIs on the Freon PDIs on the Smoke Detector ◉ No I's PDIS. Answer: Assigned door checks at LI door .. Jumpseat and area check at No I's jumpseat. Galley checks at FWD galley. PA / Interphone operational. PDIs on : Ll door. L1 slide. Flight deck door
. Under No 1's jumpseat. Above No I's jumpseat. If No 4 is not on board during PDI ( e.g. marshalling ) , the No 1 must also do the No 4's PDIS. ◉ No 2's PDIs. Answer: Assigned door checks at L2 door. Jumpseat and area check at No 2's jumpseat. Toilet checks at AFT left toilet. Cabin checks at rows 21-33. Galley checks at AFT galley including ELS. PA / Interphone operational. Check water and waste system. PDIs on : L2 door. L2 slide. ELT. Under No 2's jumpseat. Behind 33 ABC. All G4 - left hand side stowages and equipment ◉ No 3's PDIS. Answer: Assigned door checks at R2 door. Jumpseat and area check at No 3's jumpseat Toilet checks at AFT right toilet. Cabin checks at rows 11-20. PDIs on: R2 door, R2 slide, Above No 3's jumpseat. Under No 3's jumpseat.
Overwing exits. Behind row 33 DEF (if required) All G4 - right hand side stowages and equipment. ◉ No 4's PDIs ( If the No 4 is not at the Boarding Gate ). Answer: the Assigned door checks at R1 door, Toilet checks at FWD toilet, Cabin checks at rows 1-10, PDIs on: R1 door, R1 slide, All G1 stowages and equipment. All G2 stowages and equipment. ◉ No 1's Cabin Secure Checks. Answer: Galley Secure Checks FWD galley Cabin lighting set to appropriate mode Ensure pre - recorded announcements are switched off Receive "Cabin secure" from No 2 and No 4 ◉ No 2's Cabin Secure Checks. Answer: Cabin Secure Checks at rows 21 - 33 Galley Checks in Rear galley. Toilet Checks in Rear left toilet. Receive "Cabin secure" from No 3. Give "Cabin secure" to the No 1 (by pressing the call bell and giving thumbs up) Immediately take seat. ◉ No 3's Cabin Secure Checks. Answer: Cabin Secure Checks at rows 11 - 20 Toilet Checks in Rear right toilet. Give "Cabin secure" to the No
- Immediately take seat.
immediate threat to passengers and crew members on board , but which may escalate into an emergency. ◉ Possible reasons for a rapid disembarkation include:. Answer: a security alert , smoke or fumes in the cabin overheating PEDs a fuel spillage a fire outside the aircraft which could threaten the aircraft , etc. ◉ In the event of a blockage in the mid cabin. Answer: the remaining passengers in the front cabin shall be held in the front part of the cabin ( preventing them from the flow of passengers towards the FWD disembarking ) until the blockage is cleared and LI door has been re - established. ◉ Arming / Disarming No 1. Answer: Front service door R ◉ Arming / Disarming No 2. Answer: Rear service door R. ◉ Arming / Disarming No 3. Answer: Rear passenger door L. ◉ Arming / Disarming No 4. Answer: Front main passenger door L .
◉ Arming a Slide sequence of actions shall be :. Answer: 1. Doors closed. 2. Pax seated. 3. Ready for pushback confirmation given ( 1 + ENT ) ; 4. Command to arm the slides given by the Captain * 5. Slides armed and cross checked and confirmed with css 6. Safety demonstration commences. 7. Practical elements of the demonstration (seatbelts, O2 masks, life jackets, safety cards) completed 8. Cabin secure completed 9. Cabin secure confirmed with the flight crew by the css ◉ Disarming a slide what do cc say?. Answer: Cabin crew, doors to manual and cross check ◉ Where are cc stood during refuelling. Answer: No1 at L1, No4 at R3, No2 at L2, No3 at overwing exits ◉ The No 4 Detects the Hazard :. Answer: The No 4 must inform the No 1 verbally. The No 1 must enter the flight deck and advise defueling must be stopped immediately. the Flight Crew that refuelling / The No 1 must inform the No 2 , via the interphone , of the hazard. The No 1 presses the call bell 3 times to alert the No 3 , who must remain vigilant. The No 1 and No 2 must immediately stop the boarding of passengers. All CC must be ready to evacuate using all available exits. ◉ The No 3 Detects the Hazard :. Answer: Press the call bell 3 times defueling can be stopped immediately. to alert the No 1 to the hazard , so that refuelling The No 1 must enter the flight deck and
◉ Cabin / Galley Light Settings in Hours of Darkness Non Boeing Sky Interior. Answer: Window - Off Work - Off Galley / Work - Off Entry - Off Area - Off Ceiling - Night ◉ Cabin / Galley Light Settings in Hours of Darkness boeing Sky Interior. Answer: Forward entry - Off Aft entry area - Off Work - Off Passenger seating area - Night / Sleep ◉ Cabin / Galley Light Settings in Dusk / Dawn Non Boeing Sky Interior. Answer: Window - dim Work - off Galley - dim Entry - dim Area - off Ceiling - dim
◉ Cabin / Galley Light Settings in Dusk / Dawn Boeing sky interior. Answer: Forward entry - Off Aft entry area - Off Work - Off Passenger seating area - Sunrise / Sunset ◉ Operation of the Emergency Lighting Systems: Automatically. Answer: The system will illuminate automatically once aircraft power is lost ◉ Operation of the Emergency Lighting Systems Electrically:. Answer: The system is controlled by a switch in the flight deck , which has three positions OFF , ARMED , ON. This switch is placed in the ARMED position by the Flight Crew prior to departure. When the switch is flicked from ARMED to ON the lights will operate. ◉ Operation of the Emergency Lighting Systems Manually. Answer: The system can be activated by the CC manually by use of the EMERGENCY LIGHTING SYSTEM (ELS) switch, which is situated on the rear CSA panel. The No 2 is responsible for the ELS operation e.g. time available emergency. ◉ Emergency Lighting Systems Operation. Answer: Lift up the safety guard. Push the switch.
