Boeing 777 Practice Exam BHome / Boeing 777 Practice Exam B Boeing 777 Practice Exam B Boeing 777 Practice Exam B 1 / 124 What is the maximum allowable crosswind for Cat 2 and Cat 3 autoland operations? 15 knots 40 knots 30 knots 25 knots (FCOM1 L.10.5) 2 / 124 From which page is the estimated fuel remaining at destination obtained? APPROACH REF page RTE LEGS page 1 PROGRESS page 1 and CRZ page ROUTE page 1 3 / 124 On which page would you prevent the FMC from using VOR/DME updating? Progress page 2 POS page 2 Nav Radio Nav Data 4 / 124 What must be typed in the scratchpad to create a new waypoint located 15 miles along the 275 deg. radial from the Belfast (BEL) VOR? 275/15BEL 275BEL/15 BEL275/15 BEL27515 5 / 124 During a VNAV climb what speed is normally commanded by the FMC above speed transition altitude? V2 + 100 knots ECON climb speed 240 knots 250 knots 6 / 124 On which page would you enable/disable use of GPS for navigation? Nav Data Menu Approach Ref Pos Ref 7 / 124 To where is data entered on the right FMS-CDU sent? The Right FMC only The FMC selected by the FMC Master switch only The Left FMC only Both FMCs 8 / 124 How is a message in the scratchpad cleared? By pressing the DEL key momentarily By pressing CANC on the Display Select Panel By pressing and holding the DEL key Pressing the CLR key 9 / 124 You are currently looking at Legs page 5 to 7. Which page will be displayed if you now press the Legs button? Legs page 6 Legs page 1 Init/Ref Index Legs page 7 10 / 124 What is the indication of a SELCAL call to the aircraft? A CALL light flashing on the overhead panel An EICAS 'SELCAL' message only A High/Low chime, EICAS 'SELCAL' message, and an Audio Control Panel CALL light Only the appropriate CALL light illuminating on the transmitter select switch 11 / 124 Your PFD is displaying an amber LDG ALT flag. When will this be removed? After entry of the Zero Fuel Weight When the Runway is chosen on the Approach Ref page When the Route in the FMC is activated After first engine start 12 / 124 How is the Caution beeper silenced? By pressing the CANC/RCL switch Only when the condition no longer exists Automatically after four beeps By pressing the Master Caution light 13 / 124 When are the Master Caution lights and beeper inhibited? If one engine is shut down in flight If the aircraft ground speed exceeds 65 knots When both Fuel Control Switches are at Cut-off and the aircraft is on the ground If the aircraft is on the ground with the parking brake set (FCOM2 15.20.39) 14 / 124 On the PFD, how will a Vertical Speed of 500ft/min up be shown? Needle pointing upwards halfway to the 'I' mark and no digits Needle pointing downwards halfway to the 'I' mark, and no digits Needle pointing upwards halfway to the 'I' mark, and '500' above the VS display Needle pointing upwards halfway to the 'I' mark, and '500' below the VS display 15 / 124 What happens to primary engine indications if the upper display unit fails? They are lost They appear on the left PFD They appear on the lower screen They automatically transfer to the right hand PFD (FCOM2 10.20.6) 16 / 124 Which display units are normally controlled by the Display Select Panel? The outboards and inboards The inboards and lower centre The upper and lower The inboard display unit only 17 / 124 The ND is in Map Mode, with Airports de-selected. Which airport(s) are displayed? None All the Alternate Airports The one nominated Alternate Airport The nearest Airport (FCOM2 10.40.20) 18 / 124 You are landing a 777 in Cat 3 weather on a category (L) runway. After touchdown should you disengage the autopilot? Yes, but you must switch on the PVD Yes, as rollout guidance is not assured Yes, but use Flight Director to maintain rollout guidance No (FCOM1 SP.30.7) 19 / 124 At 1500R on an automatic approach, LAND 2 is annunciated. What visual reference would you need at decision height? 1 light 3 consecutive lights including a lateral element 3 consecutive lights without a lateral element Depends on the lighting system 20 / 124 Visual reference is lost below the decision height on a 777 Cat 3a approach. What should you do? Hand over control and try to regain the reference Go around at 14 feet Carry on and land Go-around (FCOM1 SP.30.7) 21 / 124 For a reported RVR of 75 metres and a centreline light spacing of 15m, what is the minimum number of centreline lights you would be able to see? 5 6 3 4 (777 tech study guide Page 79) 22 / 124 What is the decision reference for Cat 2 and 3 operations? QFE Barometric altitude Radio altitude QNH 23 / 124 What colour are taxiway stopbar lights? Red Green Red and yellow Green and yellow 24 / 124 For Cat 3b operations a pilot may not continue an approach below the decision height unless he has which of the following in sight? Centreline light Runway edge light Touch down zone light Side row barrette 25 / 124 Where can the RVR requirements for a PVD assisted take off be found? FCOM Volume 1 Standard Sector Standard 150m FCOM Volume 1 Supplementary Procedures CARD or relevant Performance Manual page ) (FCOM1 SP.30.2 26 / 124 Where are Time Critical Warnings displayed? On the CDU On the ND On the EICAS display On the PFD (FCOM 2 15.20.1) 27 / 124 How can you differentiate between Caution and Advisory messages? Cautions are red, Advisories are amber Cautions are amber, Advisories are white Advisories have no associated aural Only Advisories show on the EICAS display 28 / 124 An EICAS Caution message is at the top of the list of Caution/Advisory messages? What does this mean? It has the highest priority of the Caution alerts It is the first to have appeared It has the lowest priority of the Caution alerts It is the most recent message (FCOM 2 15.20.3) 29 / 124 When will the Ram Air Turbine (RAT) automatically deploy? The RAT can only be deployed manually If both AC transfer buses lose power in flight (FCOM 2 6.20.14) If both main AC buses lose power in flight If all four TRU's fail in flight 30 / 124 What electrical supply(s) is required to feed the entire aeroplane AC electrical load without load shedding? Secondary EXT power APU power OR an IDG Primary EXT power Primary EXT power with APU power (FCOM2 6.20.1) 31 / 124 If both Transfer buses are lost, what is the first backup source to power the captain's flight instrument bus? The PMGs The RAT The battery The AC standby bus (FCOM2 6.20.13) 32 / 124 The main battery provides standby power to the following: The hot battery bus, the battery bus, captain's flight instrument bus, standby inverter The hot battery bus, the battery bus, captain's flight instrument bus, F/O's flight instrument bus, standby inverter The hot battery bus, the battery bus, the left transfer bus, F/O's flight instrument bus, standby inverter The hot battery bus, the battery bus, captain's flight instrument bus, the left transfer bus, standby inverter (FCOM2 6.20.13) 33 / 124 When will a backup generator power one or both transfer buses? When power to one or both AC main buses is lost When LOC is selected on the autopilot MCP If one of the IDGs fails with the APU serviceable If the APU is unserviceable, but both IDGs are serviceable (FCOM2 6.20.8) 34 / 124 How is the fuel freeze temperature entered? As a default value of -49 degrees C Through the FMS CDU By maintenance during aircraft fuelling By using a selector on the overhead fuel panel (FCOM2 12.20.1) 35 / 124 When is each centre tank pump switch PRESS light inhibited? When the centre pumps are operating When the L or R main tank pumps are operating When the centre tank contains less than 180kgs of fuel When the switch is selected to OFF (FCOM2 12.10.1) 36 / 124 What is normally used for the thrust setting parameter on GE90 powered aircraft? EPR N2 Combined N1 and N2 N1 (FCOM2 7.20.2) 37 / 124 During climb with the EECs in normal mode, what will happen if the thrust levers are manually positioned forward? The engines will exceed the maximum rated thrust limit The engines will produce the reference thrust value shown on the EICAS display. The engines will produce maximum rated thrust The engine fuel valve will be fully open (FCOM2 7.20.6) 38 / 124 Why is it necessary to monitor engine oil pressure during an autostart? Because the autostart system will not abort the start for oil parameter anomalies Because the autostart system has a history of aborting the start too late for oil parameter anomalies To ensure the oil pressure does not rise until the N2 speed reaches 30% To ensure the oil pressure does not rise until the N1 speed reaches 30$ (FCOM2 7.20.10) 39 / 124 If the source of engine vibration is unknown, the Secondary Engine display will show what indication? Indications in amber Only a pointer for each engine Both N1 and N2 together BB (FCOM 7.20.26) 40 / 124 How is APPROACH idle selected? If a hydraulic pump fails with flap UP Automatically with flap selection of 25 degrees or more Manually adjusted to 5% above normal idle Automatically if that engine bleed air switch is OFF (FCOM2 7.20.8) 41 / 124 What indications provide warning of a 'Stuck On' VHF/HF transmitter? A light on the Radio Tuning Panel A light on the Audio Control Panel A loud tone during receive mode An EICAS 'RADIO TRANSMIT' message (FCOM2 5.20.3) 42 / 124 When may the maximum manoeuvring speed indication be displayed on the PFD? When operating at low altitude at relatively high gross weights When operating at high altitude at relatively low gross weights When operating at high altitude at relatively high gross weights When operating at low altitude at relatively low gross weights (FCOM2 10.10.4) 43 / 124 In which form is Vertical Speed displayed on the PFD? Only analogue Both analogue, and digital when greater than 400ft/min Analogue and digital when less than 400ft/min Only digital (FCOM2 10.30.3) 44 / 124 What form does the slip indicator take? Ball in a tube Box against a pointer Pointer against a scale No slip indicator is provided (FCOM2 10.10.6) 45 / 124 With the Air Data/Attitude source switches in the ALTN position F/Os air data is from the right pitot/static system through the SAARU Captains air data is from all pitot/static systems through the SAARU Captains air data is from the right pilot/static system through the SAARU F/Os air data is from all pilot/static systems through the ADIRU (FCOM2 10.10.38) 46 / 124 What is the maximum range at which weather radar turbulence returns can be displayed? Dependent upon gain selection 80mm 160mm 40mm (FCOM2 11.10.12) 47 / 124 What comprises the ATC transponder system? Two transponders controlled by a single panel Two transponders controlled by separate panels Three transponders controlled by separate panels A single transponder and control panel (FCOM2 11.20.14) 48 / 124 What does the PFD autothrottle annunciation display when the TO/GA switch is pressed once to carry out a go-around? THR REF. TO/GA SPD THR (FCOM2 4.10.20) 49 / 124 During climb with no altitude constraints, what happens if the altitude selector on the MCP is pushed with the altitude window set above the FMC cruise altitude? The FMC cruise altitude is changed to the altitude window altitude Nothing The FMC cruise altitude remains the same until the aircraft reaches it, at which point the FMC cruise altitude is updated automatically and the aircraft continues to climb The FMC cruise altitude is deleted and requires re-entering via the CDU (FCOM2 4.10.14) 50 / 124 How can VNAV be disengaged? By pushing the LAS/MACH selector knob By pressing the VNAV switch (mentioned in FCOM2 4.10.8 but go with other) By selecting auto-throttle THR mode By capturing the glideslope after APP has been selected By pressing the VNAV switch (mentioned in FCOM2 4.10.8 but go with other) 51 / 124 When is the go-around function of TO/GA mode armed? As 1,500ft RA is passed on the descent If LOC capture occurs When G/S is armed When the flaps are not retracted (FCOM2 4.20.16) 52 / 124 What is the lowest altitude at which you can disengage the approach made by pushing the APP switch a second time? 500 feet RA 1000 feet RA 1500 feet RA 2500 feet RA (FCOM2 4.10.16) 53 / 124 In which mode will the autothrottle engage when the TO/GA switch is pushed for take-off? HOLD SPD THR THR REF. (FCOM2 4.20.10) 54 / 124 What does the PFD autothrottle annunciation display during a FLCH climb? TO/GA THR THR REF SPD (FCOM2 4.20.9) 55 / 124 When using the DESCEND NOW feature before top-of-descent, what will be the initial autothrottle mode? HOLD THR REF THR IDLE (11.31.28) 56 / 124 In flight, what happens if the Centre hydraulic system quantity is sensed to be low? Flight controls are isolated from the Centre system and remain operable Main gear steering reverts to cable operation Left thrust reverser ceases to operate Reserve brakes are isolated from the Centre system and remain operable (FCOM2 13.20.3) 57 / 124 When will the RAT deploy automatically? When the Centre hydraulic system pressure is low If both Back-up generators fail If both AC Transfer buses are unpowered If both engine driven hydraulic pumps fail (FCOM2 13.20.3) 58 / 124 What effect does the landing gear lever have on Alternate gear extension? The lever lock must be removed, before alternate selection It may be in any position It cannot be raised after extension It must be in the DN position (FCOM2 14.10.2) 59 / 124 When steering the aircraft using rudder pedals only, at what point will main gear steering activate? After 13° of nose wheel rotation After 8° of nose wheel rotation After 7° of nose wheel rotation Main gear steering will not operate when using rudder pedals only (FCOM2 14.10.3) 60 / 124 What happens when the flight controls are operating in the Secondary mode? The PFCs are disconnected Control PCUs are operated directly by the ACEs Thrust Asymmetry protection remains available The autopilot is not available (FCOM2 9.20.7) 61 / 124 With the aircraft in landing configuration and 'SLATS PRIMARY FAIL' being the only message displayed, which of the following is available? Slat load relief only Neither flap nor slat load relief Flap Load relief only Both flap and slat load relief (FCOM2 9.20.22 – flaps are still primary RTFQ!!!) 62 / 124 The alternate pitch trim levers will, if operated, do which of the following? Disengage the autopilot Have a lower priority than control wheel pitch trim commands Blank the Stabilizer Position Indicator Move the stabilizer via control cables and the Stab Trim Control Module (FCOM2 9.20.11) 63 / 124 Where are the aileron trim indicators? Flight control synoptic Aft aisle stand Control stand Control wheel/column (FCOM2 9.20.15) 64 / 124 How can Thrust Asymmetry Compensation (TAC) be disconnected? By opposing rudder application By the switch on the overhead panel Only if trim inputs are not displayed on the rudder trim indicator By the Rudder Manual Trim Cancel switch (FCOM2 9.10.1) 65 / 124 During extension, in which mode(s) do slat movements precede flap movements? Secondary and Alternate only Primary and Secondary only Primary only All three modes 66 / 124 Prior to the first engine start, how should the engine bleed switches be configured? Both ON Only the engine to be started should be ON Only the engine to be started should be OFF Both OFF 67 / 124 When will the pack shut down, if operating in 'Standby Cooling Mode'? High altitude with low temperature Low altitude with low temperature Low altitude with high temperature High altitude with high temperature (FCOM2 2.20.2) 68 / 124 Where is the temperature level for each individual zone set? On the flight deck overhead panel At door 3L At the cabin management panel In each passenger zone (FCOM2 2.20.3) 69 / 124 When is bleed air supplied by the high-pressure section of the engine? When take-off power is set When Anti-Ice selected ON Descent and other low power setting operations On the ground only (FCOM2 2.40.1) 70 / 124 During normal operation, where does the outflow take place? Mostly through the forward valve Always through the forward valve as the aft valve is normally closed Through both valves equally Mostly through the aft valve (FCOM2 2.30.1) 71 / 124 Where does landing altitude barometric pressure correction come from? The SAARU The captain's altimeter setting The ADIRU The F/O's altimeter setting (FCOM2 2.30.2) 72 / 124 In automatic mode, where is the landing altitude for the pressurisation system taken from? The selector on the overhead panel The Centre CDU data page The EFIS control panel The FMC (FCOM2 2.30.2) 73 / 124 What indications on the EICAS display show that an outflow valve is under manual control? The 'FWD' or 'AFT' turns green MANUAL is displayed under the valve position indicator An 'M' appears at the needle base on the display The valve position indication turns amber (FCOM2 2.10.8) 74 / 124 How is heating supplied for the forward cargo compartment? From the forward equipment ventilation system A conditioned air supply Electrical heated floor panels A bleed air heating system (FCOM2 2.20.4) 75 / 124 How is the bulk cargo compartment heated? Ventilated aft equipment cooling air Conditioned air from the packs Independent bleed air system Electrical heating elements (FCOM2 2.20.4) 76 / 124 When is automatic ice detection inhibited? With TAT at 10°C or above Until the aircraft is above 500ft AAL If wing or engine anti-ice is selected OFF On the ground (FCOM2 3.20.1) 77 / 124 Where is the wing anti-ice annunciation displayed? Below the EICAS N1 indication On the overhead panel There is no wing anti-ice annunciation At the bottom of the PFD (FCOM2 3.20.2) 78 / 124 What does the Engine Fire Extinguisher system consist of? Two extinguisher bottles, which can be discharged into either engine One extinguisher bottle for each engine Two extinguisher bottles for each engine One extinguisher bottle, which can be discharged into either engine (FCOM2 8.20.3) 79 / 124 What does the wheel well fire detection system consist of? Single detector loop in nose and main wheel wells Dual detector loops in main gear wells only Dual detector loops in nose and main wheel wells Single detector loop in main wheel wells only (FCOM2 8.20.4) 80 / 124 What action would you take if the caption 'OFFSCALE' appeared on the ND? Switch transponder from TA only to TA/RA Push the TFC switch on the EFIS control panel Change from expanded to Centred MAP mode on ND Increase the ND range on the EFIS control panel (FCOM2 15.10.9) 81 / 124 Which category or categories of TCAS traffic will generate voice aural alerts? All RA and TA only TA only RA only (FCOM2 15.20.15) 82 / 124 What is the maximum landing tailwind component for a slippery runway? 10 knots 15 knots 5 knots 25 knots (FCOM1 L.10.1) 83 / 124 In flight, what would you suspect if the fuel temperature display turned amber? The fuel temperature is approaching its maximum The temperature is approaching the freeze temp entered on the FMS CDU The fuel temperature is at or below -10°C There is a fuel temperature imbalance (FCOM2 12.20.1) 84 / 124 What is maximum crosswind for take-off and landing for a dry runway? 15 knots 40 knots 25 knots 30 knots (FCOM1 L.10.1) 85 / 124 What is the maximum Take-off and Landing Altitude? 6,400 feet pressure altitude 6,600 feet pressure altitude 8.600 feet pressure altitude 8,400 feet pressure altitude (FCOM1 L.10.1) 86 / 124 What limit protection is retained when the EEC operates in the Hard Alternate mode? Thrust N1 and N2 overspeed Thrust and N2 overspeed Thrust and N1 overspeed (FCOM2 7.20.8) 87 / 124 What must be annunciated to carry out a Cat 3A – (DH below 100 feet but not less than 50 feet) automatic approach and landing? NO AUTOLAND AUTOLAND LAND 2 OR LAND 3 LAND 3 only (FCOM1 L.10.5) 88 / 124 In Primary mode, what is the complete flap setting range that the load relief facility is operative? 20 to 30 0 to 30 25 to 30 15 to 30 (FCOM2 9.20.21) 89 / 124 During taxi for take-off a system malfunction occurs. What would be your considerations regarding the MEL? Consult the MEL before completing the QRH drill The MEL must not be consulted Consult the MEL after completing the QRH to see if relief is available for continued operation with the fault Consult the MEL for Memo messages only 90 / 124 What is MMO above 30,000 feet to the aircraft ceiling? 0.87 mach 0.77 mach 0.84 mach 0.79 mach (FCOM1 L.10.11) 91 / 124 What is the minimum height for engagement of the autopilot after takeoff? 200ft 300ft 500ft 400ft (FCOM1 L.10.4) 92 / 124 What is the maximum takeoff and landing tailwind component? 10 knots 5 knots 15 knots 12 knots 93 / 124 What is the Maximum Operating Altitude capability, at LRC, for an aircraft weight of 270,000kgs at 1.3G margin to initial buffet? 34,800ft 33,300ft 36,100ft 32,800ft 94 / 124 After engine failure, what is the level off pressure altitude for an aircraft weight of 260,000kgs at ISA +15°C? 15,500ft 19,300ft 18,200ft 17.100ft 95 / 124 From when is trip fuel (TIF) calculated? Achievement of screen height Commencement of taxying Start of the take-off roll Engine start 96 / 124 What is the Reserve fuel figure based upon? Contingency fuel minus Taxi fuel 7% of Trip fuel Trip fuel plus Diversion fuel 30 minutes holding, clean, 1500ft above the alternate 97 / 124 What is the maximum value of TODA equal to? 1.5 x ASDA TORA ASDA 1.5 x TORA 98 / 124 What is the length of an airfield CLEARWAY equal to? 1.5 x TORA TODA – TORA ASDA – TORA TODA – ASDA 99 / 124 What is the length of the Stopway? 46m 258m 304m 2972m 100 / 124 What is the length of the Clearway? 3230m 304m 46m 258m 101 / 124 Due to significant windshear, a Full Power take-off is required. Which of the following fields must be filled in on the CARD Performance Request? Runway Elevation Performance Correction code 56 and EST TOW EST MACTOW Performance correction code 10 102 / 124 You have received a CARD datalink error 'PERF CORRS' after uplinking a performance data request. What would be the reason? No performance corrections have been entered The requested performance corrections are not available An incorrect performance correction number has been entered Two contaminated runway corrections have been entered 103 / 124 Anti-icing will be required in the climbout. What would you enter in the performance request? Enter 25 (air conditioning off) in the performance correction line to allow for air off take Tick the anti-ice box Enter 01 (anti-ice on) in the performance correction line Leave the anti-ice box blank 104 / 124 The CARD system has not responded to a request. What would you do first? Use the generalised data in the performance manual Use SATCOM to contact Flight Technical Dispatch at LHR Reset the Comms system Get a copy of the take-off data page from the station manager 105 / 124 What is the Maximum Landing Weight at Athens on runway 03R at 30 flap slippery, zero headwind? 228.6 265.0 208.6 165.0 106 / 124 What is the threshold elevation for Athens runway 03R? 357 ft 271 ft 435 ft 385 ft 107 / 124 The (B) under Rwy 07 at Barcelona indicates that the runway is suitable for an automatic approach, but with which of the following qualifiers? Available for evaluation Available to a disengage height of 100R No roll-out guidance Black beam is required 108 / 124 Airfield Data for B777-76B at LONDON HEATHROW. RW 27L FULL LENGTH (DRY) W/V CALM QNH 1010 TEMP +16 oC (STRUCTURAL LIMIT FOR T/O is 242.7T)What is the Take-Off Performance Limit (TOPL) Weight for this take-off? 210.0 242.7 259.7 260.6 (TOPL limit!!! Not RTOW) 109 / 124 What is the Basic Index of G-VIIA? 784.0 783.0 782.1 18044 110 / 124 What items comprise the Actual Zero Fuel Weight? Load in cargo compartments plus Dry Operating Weight Actual Take-off Weight less Trip Fuel Actual Landing Weight less Trip Fuel Total Traffic Load plus Dry Operating Weight 111 / 124 How much fuel will be used from take-off on the LHR-DXB sector? 34,092 kgs 45,000 kgs 59,000 kgs 59,800 kgs 112 / 124 What action is required if the letters RF are showing next to a hydraulic system quantity on the status page? Maintenance action to add hydraulic fluid to the associated system Crew action to run the associated system and clear the fault Maintenance action to re-pressurise the associated systems reservoir Maintenance action to drain fluid from the associated system in order to bring down the quantity 113 / 124 What action would you take with the Cargo Temperature selectors if live animals were to be carried in the bulk cargo? Aft low, bulk low Aft low, bulk high Aft off, bulk low Aft high, bulk off (FCOM1 NP.30.6) 114 / 124 Which bus can be powered on the ground only? Right Main AC Bus Ground Service Bus Left Transfer Bus Ground Handling Bus (FCOM2 6.20.5) 115 / 124 What will be the indication against a low (below 0.4) hydraulic quantity on the STATUS page? LO (amber) RF (white) Dashes Blank (FCOM2 13.10.3) 116 / 124 Where is the APU Ground Control Fire Protection Panel located? At the nose wheel Left main gear well At the refuelling Panel At the rear of the forward access bay door. (FCOM2 8.10.5) 117 / 124 What are the memory items in response to the warning STABILIZER? Maintain current trim and airspeed Re enter the weight and cg figures in the FMC There are no memory items for this message Stabilizer cut out switches to CUTOUT and do not exceed current airspeed. 118 / 124 After completing an Emergency Descent due to excessive cabin altitude, how is the boom microphone reselected? Close the right hand Oxygen panel door Close the left Oxygen panel door, then push & release the reset/test switch Press the Flight Interphone Transmitter select switch Operate the Mic/Interphone switch (FCOM2 5.20.1) 119 / 124 For an in-flight cross-bleed engine start, where is the recommended procedure found? In the ..... ECL, Non-Normal 'Engines' section ECL, Non-Normal 'Air Systems' section FCOM Volume 1, 'Supplementary Procedures' section FCOM Volume 1 – Normal Operations' section (in QRH there in ECL section) 120 / 124 With the BRAKE SOURCE light illuminated, what braking is available for landing? Alternate, reserve and accumulator Alternate, reserve and park brake All braking except Normal Accumulator only (QRH 14.1) 121 / 124 Where is the Fuel Jettison procedure located? ECL, Unannunciated and Fuel Sections Technical Manual FCOM Volume 1 – Supplementary Procedures FCOM Volume 1 – Normal Procedures (in QRH) 122 / 124 During a normal Flaps 5 (from 1) extension, the flap indicator turns amber. What does this indicate? The flap drive mechanism has failed The flaps are operating in Secondary mode The flaps are moving electrically to the 5 position Extension of the flaps may be made using the Alternate system (FCOM2 9.10.12) 123 / 124 What is the first action to be taken if airspeed is deemed to be unreliable? Turn off both flight directors Check the pitch altitude and thrust for the phase of flight Inform Air Traffic Control Disconnect the autopilot (QRH 10.1) 124 / 124 In flight, after two extinguishers discharge into the forward cargo compartment, when are the remaining bottles discharged? One bottle automatically after a time delay All remaining bottles automatically after a time delay One bottle manually after 20 seconds All remaining bottles automatically at 20 seconds after (FCOM2 8.20.5) Your score is