Boeing 777 Progress Test 1Home / Quiz Page / Boeing 777 Progress Test 1 Boeing 777 Progress Test 1 Boeing 777 Progress Test 1 1 / 50 On Which CDU page are Waypoint Altitude Constraints entered? ROUTE LEGS PROGRESS CLIMB and DESCENT 2 / 50 What is the minimum glideslope angle for an automatic landing? 2.5 degrees 3.25 degrees 2.0 degrees 1.5 degrees 3 / 50 If page 1 of EICAS alerts is being displayed, how would you view the next page? Press the CANC/RCL switch Select the STATUS display onto the lower MFD Press the NEXT PAGE key on the CDU Reset the Master Warning/Caution switch 4 / 50 How would you remove accumulated ADIRU errors with the ADIRU switch? Switch it OFF for 30 seconds, then ON Select ATT, then NAV Move it to ATT, then ALIGN Select ALIGN, then NAV 5 / 50 How can Warning messages be cleared from the EICAS display? By pressing the CANCEL switch By pressing the STATUS switch By correcting the fault which caused the warning By pressing the RECALL switch 6 / 50 Where will the PFD move to if an outboard display unit fails? To the EICAS display if PFD is selected on the display selector To the inboard display. If the Inboard Display Selector is at MFD To the CDU when MENU is selected Automatically moves to the inboard display unit regardless of the position of the Inboard Display Selector 7 / 50 When is the route offset function unavailable? When flying a SID or STAR When UNABLE RTA is shown in the scratchpad When more than 2.5 miles off the LNAV track North of 82 degrees 8 / 50 When can Contingency Fuel be used? After top of descent The cruise phase only After the Reserve Fuel has been used Any time after the commencement of the flight 9 / 50 If a checklist, or an item, is overridden, to which colour will it change? Yellow Cyan Red Green 10 / 50 Which CDU page can be used to enable the Off Path Descent? PROG 2/3 ACT ECON DES NAV DATA NAV RAD 11 / 50 Above what bank angle do the Bank Pointer and Slip/Skid indicator turn amber? 55 degrees 25 degrees 35 degrees 45 degrees 12 / 50 Which of these calculations represents Accelerate-Stop Distance Available (ASDA)? TODA x 1.25% TORA + STOPWAY TODA x 1.25% TORA + CLEARWAY 13 / 50 What entry is required in the scratchpad to create a new waypoint situated 20 miles along the 280 degrees radial from Brecon (BCN)? 20-BCN280 BCN280-20 BCN20/280 BCN280/20 14 / 50 When an inboard Display Selector is in the PFD position can any other display be shown? Yes, any Yes, but only ENG, FUEL and AIR No they all inhibited Yes, any but ENG and STAT 15 / 50 How are Unannunciated checklists accessed? By using the MENU key on the centre CDU They are inhibited until after the flight Just press the CHKL switch – they appear automatically CHKL switch, Non-Normal menu selection 16 / 50 How can the ILS receivers be tuned for a PVD take-off? Via the radio tuning panel Using EFIS control panel Automatically when the runway is entered on the ROUTE page Manually on the NAV/RAD pages 17 / 50 Which of these conditions will cause the Pitch Limit Indicator to be displayed Below 20,000ft Below 1500RA Slow speeds with flaps UP Gear Down 18 / 50 What is the maximum wind strength for taxi? 50 mph 65 mph 65 knots 45 knots 19 / 50 Which of these calculations represents Take-Off Run Available (TORA)? ASDA – STOPWAY ASDA – CLEARWAY TODA – TORA TODA – ASDA 20 / 50 What does ‘TIME TO ALIGN/XXXX’ on the NDs indicate? Time remaining for the Navigation Database to re-establish Time left for the RNP to re-engage Time remaining for the ADIRU to align Time remaining for the FMCs to update 21 / 50 What is the TOPL Weight? The weight limit at take-off based solely on aircraft performance parameters The weight based on aircraft structural limitations The maximum at which take-off is permitted by conditions other than available performance The maximum permitted take-off weight of the aircraft at the start of the take-off run 22 / 50 How many cursors can be in use at the same time? 1 (2 if the First Officer uses the side display) Only 1 belonging to whoever used the cursor last 2, but only on the Electronic Checklist 2, on different displays on different screens 23 / 50 Following the EICAS advisory message ‘NAV AIRc DATA SYS’, what information is being displayed to you? Both PFDs display SAARU data The left PFD displays Left SAARU data; the right PFD – displays right ADIRU data The standby ASI and Altimeter displays SAARU data The left PFD displays ADIRU air data; the right PFD – displays SAARU data 24 / 50 What is the maximum allowable tailwind for an automatic landing? 15 kts 7 kts 10 kts 5 kts 25 / 50 Which of the following EICAS alerts has priority in the queue of checklists? Caution Warning Memo Advisory 26 / 50 In what form is the selected altitude displayed on the PFD Altitude indications? Digits only Bug against scale only Bug against scale and in digits A white box enclosing the digital figure 27 / 50 What is the significance of an Advisory message being at the top of its list? It has a QRH reference It is the most recent It has the lowest priority It has the highest priority 28 / 50 With an inboard Display Selector selected to the EICAS position, what DSP selections are available to that screen? ENG, FUEL and AIR DOOR, GEAR and FCTL ELEC, HYD and GEAR ENG and STAT 29 / 50 What automatically resets the electronic Normal Checklist? Go-Around, airborne, TO/GA selected, gear not up After Landing Touch and Go and reversers deployed Selecting Reset All through the FMS menu page 30 / 50 When will the vertical speed be shown digitally on the VSI? Always More than 400 fpm Less than 400 fpm More than 1000 fpm 31 / 50 What is the maximum allowable cabin pressure differential for takeoff and landing? 0.22 psi 0.11 psi 0.01 psi 0.33 psi 32 / 50 What is the maximum crosswind limit for landing (dry or wet runway)? 30 kts 25 kts 65 kts 40 kts 33 / 50 VΜΒΕ is the maximum speed on the ground from which a stop can be made within the energy capabilities of the wheel brakes. What is the constraint on V1 relative to VΜΒΕ? V1 must never exceed VΜΒΕ V1 must be adjusted for TOPL to cater for VΜΒΕ V1 must never be less than VΜΒΕ V1 and V2 can be the same, but never less than VΜΒΕ 34 / 50 You are more than halfway to your destination; which page will be displayed when you hit the INIT REF key? An ‘INDEX’ page The ‘APPROACH REF’ page The ‘IDENT’ page The ‘ARRIVALS’ page 35 / 50 When you press the Master Caution Reset switch, what is cancelled? Master Caution lights and EICAS message Master Cautions lights only EICAS message only Beeper and Master Caution light 36 / 50 During cruise, which key(s) would you press to display the DESCENT page? CRZ VNAV and NEXT PAGE PROG VNAV 37 / 50 Onto which display screen(s) can all synoptics be selected? EICAS display only Primary or lower MFD displays Primary, but only if lower MFD has failed Any selected MFD 38 / 50 Which type of message is normally displayed on the lower MFD Advisory Status Memo Alert 39 / 50 Which FIRE indications are inhibited during a portion of the take-off? Bell only Bell, Master Warning lights and EICAS message Bell and Master Warning lights All indications except the EICAS message 40 / 50 For which flap settings can automatic landings be made with one engine inoperative? 20, 25 and 30 20 and 30 20 only 25 only 41 / 50 Where is the current MACH displayed on the PFD airspeed indication? Top Centre Bottom Bottom, but only when Mach is below 0.4 42 / 50 If an EFIS control panel fails, how can the displays be controlled? Through the – Opposite EFIS control panel Related CDU menu Display Selector Panel MCP 43 / 50 What is the Maximum Operating Altitude? 43,900 ft 39,600 ft 43,100 ft 44,000 ft 44 / 50 VMCG is the minimum speed at which the take-off can be continued safely in the event of the failure of the critical engine. What is the constraint on V1 relative to VMCG? V1 must never exceed VMCG V1 must never be less than VMCG VMCG and MACTOW must always be the same as V1 V1 and VMCG must always be adjusted to the % CG 45 / 50 What is the minimum autopilot engagement height after take-off? 400 ft AGL 100 ft AGL 150 ft AGL 200 ft AGL 46 / 50 When taxiing in a crosswind of 40 knots engine power should be limited to 70% N1 65% N1 70% N2 65% N2 47 / 50 What is the regulated Take-off Weight (RTOW)? The weight limit at take-off based solely on performance parameters Estimated Take-off Weight minus actual Ramp Weight The lower of the Maximum Authorised Take-off Weight (MTOW) and TOPL Weight The higher of the Maximum Authorised Take-off Weight (MTOW) and TOPL Weight 48 / 50 What is the maximum fuel temperature? Plus 49 degrees F Plus 42 degrees C Plus 49 degrees C Minus 47degrees C 49 / 50 What is the Reserve Fuel figure based on? 30 minutes holding, clean, 1500ft above the alternate Trip Fuel minus Taxi Fuel 5% or 15 minutes cruise fuel, whichever is greater Contingency plus Diversion Fuel 50 / 50 What does ‘TIF’ stand for on the Cirrus Fuel Plan? Totalizer Indicated Fuel Time In Flight Total In Flight The Incremental Fuel Your score is