1.- ALL NAV AID ARE NORMALLY AUTO TUNED BY:. A - THE FMGC. B - MCDU. C - ADIRU.
2.- ALL NAV AID ARE NORMALLY AUTO TUNED BY:. A - THE FMGC. B - MCDU. C - ADIRU.
3.- ALL PFD DISPLAYS EXCEPT ATTITUDE; SPEED; HEADING; ALTITUDE; AND VERTICAL SPEED ARE REMOVED WHEN PITCH ATTITUDE EXCEEDS 25 DEGREES NOSE UP OR 13 DEGREES NOSE DOWN. A - TRUE. B - FALSE.
4.- AMBER BOX PROMTS ON THE MCDU INDICATE DATA: A - ENTRY IS OPTIONAL FOR FMGS OPERATION. B - ENTRY IS REQUIRED FOR MINIMUM FMGS OPERATION. C - WILL BE FILLED IN BY THE FMGS.
5.- AN AMBER BOX ON THE MCDU SCREEN INDICATES: A - AN OPTIONAL DATA ENTRY. B - A MANDATORY DATA ENTRY. C - A COMPULSORY REPORTING POINT. D - THE WAYPOINT INDICATED WILL BE OVER FLOWN.
6.- AN FMGS MESSAGE WHICH REQUIRES IMMEDIATE ATTENTION IS DISPLAYED IN: A - RED. B - AMBER. C - MAGENTA.
7.- APPR PB. IS USED TO ARM/ENGAGE THE GUIDANCE MODES RELATED TO THE APPROACH: A - SELECTED ON THE NAVIGATION RADIOS. B - INSERTED INTO THE FLIGHT PLAN (ILS ONLY). C - INSERTED INTO THE FLIGHT PLAN (ILS OR NON ILS).
8.- BOTH AUTOPILOTS CAN BE ENGAGED AND ACTIVE IN ANY PHASE OF FLIGHT. A - TRUE. B - FALSE.
9.- BOX PROMPTS ON THE MCDU INDICATE DATA: A - ENTRY IS OPTIONAL FOR FMGS OPERATION. B - ENTRY IS REQUIRED FOR MINIMUM FMGS OPERATION. C - WILL BE FILLED IN BY THE FMGS.
10.- CAN THE AUTOPILOT BE USED FOR A SINGLE ENGINE APPROACH AND AUTO LAND? A - YES. B - NO.
11.- CAN THE CREW DEPRESS THE RMP ON NAV PUSHBUTTON AND USE THE RMP FOR NAVIGATION SIMULTANEOUSLY WITH FMGC AUTO TUNING? A - YES, BECAUSE THE OPPOSITE FMGC WILL CONTINUE TO AUTO TUNE NAVAIDS. B - NO, RMP BACKUP TUNING SUPERSEDES THE AUTO TUNING FUNCTION OF BOTH FMGC\'S.
12.- COST INDEX = 0 (ZERO) CORRESPONDS TO: A - MINIMUM FUEL CONSUMPTION (MAX RANGE). B - MINIMUM TIME. C - BEST RATIO BETWEEN THE FLIGHT TIME COST AND THE FUEL COST. D - LRC (LONG RANGE CRUISE).
13.- DASHES ON THE MCDU INDICATE DATA: A - ENTRY IS NOT ALLOWED. B - IS BEING CALCULATED BY THE FMGS. C - EITHER A OR B.
14.- DURING A TURNAROUND, YOU NOTICE THAT THERE IS A RESIDUAL GROUND SPEED ON BOTH NDS. HOW DO YOU CORRECT THIS? A - AS THE ENGINES HAVE BEEN SHUT DOWN, IT IS NECESSARY TO CARRY OUT A FULL REALIGNMENT. B - THERE IS NO CORRECTIVE ACTION POSSIBLE UNTIL THE AIRCRAFT IS COMPLETELY ELECTRICALLY SHUT DOWN. C - IT IS POSSIBLE TO CARRY OUT A RAPID ALIGNMENT BY TURNING OFF ALL 3 ADIRS MOMENTARILY.
15.- DURING DESCENT, IF YOU PUSH THE EXPEDITE (EXPED) PUSH BUTTON, WHAT SPEED WILL THE AIRCRAFT TRY TO MAINTAIN? A - GREEN DOT. B - 340 KNOTS. C - 3.000 FPM VERTICAL SPEED. D - STANDARD 3.0 DEGREES ANGLE OF DESCENT.
16.- FMGC 1 IS NOT WORKING. TO ENTER DATA INTO THE FMGC, WHICH MCDU WOULD YOU USE? A - MCDU 1 ON THE CAPTAIN\'S SIDE. B - MCDU 2 ON THE FIRST OFFICER\'S SIDE. C - EITHER MCDU 1 OR MCDU 2.
17.- FOR AUTOLAND, BOTH A/PS MUST BE CONNECTED. A - TRUE. B - FALSE.
18.- GPWS AURAL AND VISUAL WARNINGS CAN NOT BE INHIBITED. A - TRUE. B - FALSE.
19.- HOW DOES THE FMGC COMPUTE RADIO POSITION? A - IRS ONLY. B - IRS AND VOR/DME. C - IRS, DME/DME. D - VOR/DME AND DME/DME.
20.- IF ONE GPS RECEIVER FAILS, THE THREE ADIRUS AUTOMATICALLY SELECT THE ONLY OPERATIVE GPS RECEIVER. A - TRUE. B - FALSE.
21.- IF THE FLEX TEMP IS NOT ENTERED ON THE TAKEOFF PAGE OF THE MCDU: A - A FLEX TAKEOFF STILL AVAILABLE, SET POWER WITH THE THRUST LEVERS. B - THE FMGS WILL ENTER IT FOR YOU BASED ON TAT. C - A FLEX TAKEOFF IS NOT AVAILABLE.
22.- IF THE SPD/MACH KNOB ON THE FCU IS NOT PULLED WITHIN A PREDETERMINED TIME TO ENGAGE SELECTED SPEED: A - THE SELECTION CAN BE MADE AT ANY TIME. B - THE SELECTION IS LOST AND DASHES ARE RE-DISPLAYED. C - THE SELECTION IS LOST AND THE DISPLY GOES BLANK.
23.- IF THE SPD/MACH KNOB ON THE FCU IS NOT PULLED WITHIN A PREDETERMINED TIME TO ENGAGE SELECTED SPEED: A - THE SELECTION CAN BE MADE AT ANY TIME. B - THE SELECTION IS LOST AND DASHES ARE RE-DISPLAYED. C - THE SELECTION IS LOST AND THE DISPLY GOES BLANK.
24.- IF YOU HAVE DEPRESSED THE EXPED PUSH BUTTON AND WANT TO CANCEL THIS FUNCTION, HOW COULD THIS BE ACCOMPLISHED? A - PUSH THE EXPED PUSH BUTTON AGAIN. B - PULL THE ALTITUDE, VERTICAL SPEED, OR SPEED KNOB. C - RETARD THE THRUST LEVERS TO IDLE.
25.- ILS 1 INFORMATION IS DISPLAYED ON _______ WHEN OPERATING IN THE ROSE ILS MODE: A - PFD 2 & ND1. B - PFD 1 & ND1. C - PFD 1 & ND2.
26.- IN FLIGHT, EITHER THE AP/FD PITCH CONTROL, OR AUTOTHRUST MAY ACQUIRE AND HOLD A TARGET SPEED OR MACH NUMBER, DEPENDING ON THE ENGAGED MODES. SPEED CONTROL IS "MANAGED" WHEN THE TARGET COMES FROM THE SPD/MACH FCU WINDOW. A - TRUE. B - FALSE.
27.- IN THE EVENT OF FAILURE OF THE AIR DATA FUNCTION OF ADIRS 1 OR 2, THE AFFECTED DISPLAYS CAN BE MANUALLY SELECTED OVER TO ADR 3 BY THE: A - ECAM/ND TRANSFER SELECTOR. B - AIR DATA SELECTOR. C - ATT HDG SELECTOR.
28.- IN THE EVENT OF FAILURE OF THE AIR DATA FUNCTION OF ADIRS 1 OR 2, THE AFFECTED DISPLAYS CAN BE MANUALLY SELECTED OVER TO ADR 3 BY THE: A - ECAM/ND TRANSFER SELECTOR. B - AIR DATA SELECTOR. C - ATT HDG SELECTOR.
29.- MANAGED GUIDANCE IS ENGAGED BY: A - PULLING ON THE DESIRED FCU SELECTOR KNOB. B - PUSHING ON THE DESIRED FCU SELECTOR KNOB. C - ROTATING 90º THE DESIRED FCU SELECTOR KNOB.
30.- ONE A/P CAN BE ENGAGED ON THE GROUND IF THE ENGINES ARE NOT RUNNING. A - THIS A/P WILL DISENGAGE WHEN BOTH ENGINES ARE STARTED. B - THIS A/P WILL DISENGAGE WHEN ONE ENGINE IS STARTED. C - THIS A/P WILL DISENGAGE WHEN SPEED IS SENSED AT > 10 KTS.
31.- OPEN CLIMB (OP CLB) IS A MANAGED MODE. A - TRUE. B - FALSE.
32.- RADIO HEIGHT IS DISPLAYED ON THE PFD: A - BELOW 2500´ B - WHEN THE LOC OR APP P/B IS PRESSED. C - WHEN A DECISION HEIGHT IS SELECTED.
33.- SELECTION OF THE CORRECT TAKEOFF RUNWAY ON THE FMGC PRIOR TO EACH FLIGHT IS NECESSARY BECAUSE: A - THE FADEC NEEDS IT TO KNOW HOW MUCH TO REDUCE THE THRUST TO TAKEOFF. B - SELECTION OF THE CORRECT RUNWAY INSURES PROPER PRESSURIZATION. C - SELECTION OF THE CORRECT RUNWAY PERMITS THE FMGS TO UPDATE ITS POSITION AT TAKEOFF.
34.- SIDESTICK POSITION AND MAX. SIDESTICK DEFLECTION ARE DISPLAYED ON THE GROUND ON THE PFD: A - CONTINUOSLY AFTER AIRCRAFT POWER IS APPLIED. B - AFTER THE FIRST ENGINE START. C - ON TAKEOFF ROLL WHEN POWER IS APPLIED.
35.- THE A320 HAS ________ AIR DATA INERTIAL REFERENCE UNITS (ADIRS). A - 2 B - 3 C - 4.
36.- THE AIRSPEED INDICATION ON THE PFD STARTS AT: A - 100 KTS. B - 80 KTS. C - 50 KTS. D - 30 KTS.
37.- THE ARMED VERTICAL MODES ARE DISPLAYED ON THE FLIGHT MODE ANNUNCIATOR ON THE SECOND LINE IN: A - BLUE OR MAGENTA. B - BLUE OR GREEN. C - WHITE.
38.- THE CAPTAIN\'S FMA INDICATES - FD2 IN COLUMN FIVE, LINE TWO. WHAT DOES THIS MEAN? A - FMGC #1 HAS TIMED OUT AND FLIGHT GUIDANCE IS LOST. B - THE FIRST OFFICER HAS PUSHED THE PRIORITY TAKE OVER PUSHBUTTON. C - FMGC #1 HAS TIMED OUT AND FMGC #2 IS NOW PROVIDING FLIGHT GUIDANCE FOR BOTH PILOTS. D - THE CAPTAIN\'S FD PUSHBUTTON ON THE FCU HAS NOT BEEN SELECTED "ON" AND FD2 HAS AUTOMATICALLY CROSSED OVER.
39.- THE ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) CONSISTS OF ______ IDENTICAL DISPLAY UNITS. A - 4 B - 5 C - 6 D - 8.
40.- THE ENERGY CIRCLE IS A GREEN ARC, CENTERED ON THE AIRCRAFT'S POSITION AND ORIENTED TOWARDS THE CURRENT TRACK LINE. IT IS DISPLAYED ON THE NDS DURING DESCENT, WHEN HDG TO TRK MODE IS SELECTED. A - TRUE. B - FALSE.
41.- THE ENGAGED VERTICAL MODES ARE DISPLAYED ON THE FLIGHT MODE ANNUNCIATOR ON THE FIRST LINE IN: A - GREEN OR BLUE. B - GREEN OR MAGENTA. C - BLUE.
42.- THE ENGAGED VERTICAL MODES ARE DISPLAYED ON THE FLIGHT MODE ANNUNCIATOR ON THE FIRST LINE IN: A - GREEN OR BLUE. B - GREEN OR MAGENTA. C - BLUE.
43.- THE FMGC HAVE THREE FUNCTIONS. A - ECAM CONTROL, FLIGHT GUIDANCE, FLIHGT MANAGEMENT. B - ECAM CONTROL, EIS CONTROL, FLIGHT MANAGEMENT. C - FLIGHT GUIDANCE, FLIGHT AUGMENTATION, FLIGHT MANAGEMENT.
44.- THE FMGS DATA BASE CONTAINS: A - PERFORMANCE INFORMATION, SUCH AS ENGINE FUEL FLOW, ENGINE THRUST, GREEN DOT DATA (L/D DATA), ETC. B - NAVIGATION INFORMATION, SUCH AS NAVAIDS, WAYPOINTS, AIRWAYS, AIRPORTS, RUNWAYS, ETC. C - BOTH ARE CORRECT.
45.- THE IR ALIGNMENT COUNT DOWN STOPS ONE MINUTE PRIOR TO ACCOMPLISHMENT AND THE ALIGN LIGHTS ARE FLASHING. WHY DOES IT HAPPEN? A - IT IS AN INDICATION THAT THERE IS A DISAGREEMENT BETWEEN THE IRS AND THE ALIGNMENT MUST BE RESTARTED. B - IT IS AN INDICATION THAT THE ALIGNMENT IS COMPLETE BUT MUST BE ACKNOWLEDGED. C - IT IS AN INDICATION THAT ALIGNMENT HAS STOPPED AS THE PRESENT POSITION DATA HAS NOT BEEN ENTERED FROM THE FMGS.
46.- THE LOC MODE DISENGAGES WHEN: A - ANOTHER LATERAL MODE IS ENGAGED. B - THE PILOT PRESSES THE LOC PUSHBUTTON AGAIN (ENGAGING THE HDG/TRK MODE ON THE CURRENT HDG/TRK). C - BOTH ARE CORRECT.
47.- THE MANAGED MODE OF FLIGHT GUIDANCE IS USED FOR: A - LATERAL, VERTICAL, AND SPEED COMMANDS AS SELECTED ON THE FCU. B - LATERAL, VERTICAL, AND SPEED COMMANDS AS DETERMINED BY THE MCDU. C - LATERAL, VERTICAL, AND SPEED PROFILES AS DETERMINED BY THE FMGS.
48.- THE ON BAT LIGHT ON THE ADIRS CDU ILLUMINATES: A - ONLY WHEN ALL ADIRS ARE ON BATTERY POWER. B - WHEN AN ADIRS FAULT IS DETECTED. C - WHEN ONE OR MORE ADIRS, ARE SUPPLIED BY AIRPLANE BATTERY ONLY.
49.- THE PILOT INTERFACES WITH THE FMGS USING THE: B - THRUST LEVERS. C - MCDU. D - ALL OF THE ABOVE. A - FCU. .
50.- THE POSSIBLE MODES OF FMGC OPERATION ARE. A - DUAL. B - INDEPENDENT. C - SINGLE. D - ALL THE ABOVE.
51.- THE SELECTED DATABASE DATE HAS EXPIRED. WHEN MUST THE ACTIVE DATA BASE BE CHANGED? A - PRIOR TO ENTERING THE PREFLIGHT DATA. B - ANYTIME PRIOR TO TAKEOFF. C - THE FOLLOWING CALENDAR DAY.
52.- THE SPEED TREND ARROW ON THE PFD AIRSPEED SCALE INDICATES THE SPEED VALUE THAT WILL BE ATTAINED IN ___ SECONDS IF THE ACCELERATION REMAINS CONSTANT. A - 5 B - 8 C - 10 D - 15.
53.- THE STANDBY ATTITUDE INDICATION WILL REMAIN AVAILABLE FOR _____ MINUTES AFTER TOTAL ELECTRICAL FAILURE. A - 5 B - 7 C - 10 D - 22.
54.- THE THREE DISPLAY MANAGEMENT COMPUTERS (DMCS) ACQUIRE AND PROCESS ALL INPUT FROM AIRPLANE SENSORS AND COMPUTERS TO GENERATE THE DISPLAY IMAGES. A - TRUE. B - FALSE.
55.- THE TWO BASIC MODES OF FLIGHT GUIDANCE ON THE A-320 ARE: A - SLAVED AND COUPLED. B - MANAGED AND SELECTED. C - MANUAL AND COUPLED.
56.- THE WEATHER RADAR IMAGE CAN BE DISPLAYED ON WHICH MODES OF THE ND? A - ROSE NAV OR VOR. B - ROSE VOR OR ROSE ILS. C - ROSE NAV OR ARC. D - ALL MODES EXCEPT PLAN.
57.- THE WIND SHEAR FUNCTION OF THE FAC\'S IS INDEPENDENT OF THE FLIGHT DIRECTOR ON/OFF SWITCH. A - TRUE. B - FALSE.
58.- VOR DATA CAN BE DISPLAYED ON : A - BOTH NDS. B - THE DDRMI. C - BOTH A AND B.
59.- WHAT ARE THE DIFFERENT TYPES OF FLIGHT GUIDANCE? A - SLAVED AND MANAGED. B - AUTOMATIC AND MANUAL. C - MANAGED AND SELECTED. D - MANAGED AND MANUAL.
60.- WHAT DOES PUSHING THE APPR PUSH BUTTON DO? A - ARMS MANAGED NAVIGATION. B - ARMS THE FLIGHT GUIDANCE SYSTEM TO CAPTURE A LOCALIZER AND GLIDE SLOPE IF THE INFORMATION HAS BEEN ENTERED INTO THE MCDU. C - ALLOWS THE AIRCRAFT TO SLOW TO GREEN DOT SPPED. D - ARMS MANAGED VERTICAL NAVIGATION.
61.- WHAT DO THE WHITE ROUND LIGHTS ON THE FCU DISPLAY MEAN? A - SELECTED GUIDANCE HAS BEEN ENGAGED. B - AUTOMATIC GUIDANCE HAS BEEN ENGAGED. C - MANAGED GUIDANCE HAS BEEN ARMED OR ENGAGED.
62.- WHAT HAPPENS IF YOU PRESS THE EXPED PB? A - SPEED IS SET TO 340 KNOTS FOR CLIMB AND GREEN DOT FOR DESCENT. B - SPEED IS SET TO GREEN DOT FOR CLIMB AND 340 KNITS FOR DESCENT. C - DECELERATED SPEED APRROACH IS SELECTED.
63.- WHAT HAPPENS IF YOU PUSH THE V/S KNOB? A - ENGAGE THE V/S MODE. B - COMMAND A ZERO VERTICAL RATE (ALT HOLD). C - REVERTS TO MANAGED CLIMB.
64.- WHAT IS MANAGED CLIMB SPEED ABOVE 10,000 FEET? A - GREEN DOT. B - 250 KNOTS. C - 280 KNOTS. D - ECON CLIMB SPEED.
65.- WHAT IS MANAGED CLIMB SPEED BELOW 10,000 FEET? A - GREEN DOT. B - 250 KNOTS. C - 280 KNOTS. D - ECON CLIMB SPEED.
66.- WHAT SPEED WILL THE FMGS USE IN AN EXPEDITE CLIMB? A - GREEN DOT SPEED. B - ECON CLIMB SPEED. C - 250 KNOTS BELOW 10,000 FEET. D - AMBER DOT SPEED.
67.- WHEN A DOUBLE ENTRY IS NEEDED ON THE MCDU (E.G. WIND DIRECTION/SPEED: 270/110) THE SEPARATING SLASH MUST BE USED. THE TRAILING ENTRY OF A PAIR MUST BE PRECEDED BY A SLASH IF IT IS ENTERED ALONE. A - TRUE. B - FALSE.
68.- WHEN CAN MANAGED VERTICAL NAVIGATION BE ENGAGED? A - ONLY AFTER MANAGED SPEED HAS BEEN ENGAGED. B - AT ANYTIME REGARDLESS OF THE ENGAGEMENT STATUS OF LATERAL NAVIGATION OR SPEED. C - ONLY AFTER MANAGED LATERAL NAVIGATION AND MANAGED SPEED HAVE BEEN ENGAGED. D - ONLY AFTER MANAGED LATERAL NAVIGATION HAS BEEN ENGAGED.
69.- WHEN CAN YOU SELECT BOTH A/PS AT THE SAME TIME? A - AFTER YOU SELECT BOTH NAVIGATION RADIOS ON AL ILS FREQUENCY. B - ONLY AFTER THE APPROACH MODE IS ARMED AND AN ILS APP IS INTERESED INTO THE FLIGHT PLAN. C - NEVER.
70.- WHEN FLYING AT CRUISE ALTITUDE, THE AIRCRAFT NAVIGATES USING RADIO NAV/AIDS ONLY. A - TRUE. B - FALSE.
71.- WHEN IS THE SRS ACTIVE? A - DURING A GO AROUND (AFTER THE THRUST LEVERS ARE PLACED IN THE TOGA POSITION) UP TO THE ACCELERATION ALTITUDE. B - AT T/O, WHEN TOGA OR FLX POWER IS SET, SRS IS DISPLAYED ON THE FMA AND PROVIDES GUIDANCE UP TO THE ACCELERATION ALTITUDE. C - BOTH ARE CORRECT.
72.- WHEN THE AIRCRAFT IS IN THE MANAGED GUIDANCE MODE, IT IS: A - GUIDED BY THE PILOT SELECTING THE SPECIFIC FLIGHT MODES AND PARAMETER TARGET VALUES ON THE FCU. B - RESPONDING TO PILOT INPUTS OF SPEED, ALTITUDE, AND HEADING SELECTED ON THE FCU. C - FOLLOWING LATERAL, VERTICAL AND SPEED PROFILES AS DETERMINED BY THE IRS'S. D - FOLLOWING LATERAL, VERTICAL AND SPEED PROFILES AS DETERMINED BY THE FMGS.
73.- WHEN THE ALTITUDE KNOB ON THE FCU IS PULLED: A - THE ALTITUDE IS ARMED. B - THE CURRENT ALTITUDE IS CANCELED. C - OPEN CLIMB OR DESCENT ENGAGES.
74.- WHEN THE ALTITUDE KNOB ON THE FCU IS PULLED: A - THE ALTITUDE IS ARMED. B - THE CURRENT ALTITUDE IS CANCELED. C - OPEN CLIMB OR DESCENT ENGAGES.
75.- WHEN THE THRUST LEVERS ARE MOVED TO THE TAKEOFF POSITION, THE FMGS UPDATED ITS POSITION AT TAKEOFF USING: A - IRS/DME/DME POSITIONING. B - IRS/ILS/DME POSITIONING. C - THE NAVIGATION DATABASE AND THE TAKEOFF RUNWAY ENTERED INTO THE MCDU BY THE PILOT. D - THE VOR/DME CURRENTLY TUNED.
76.- WHICH OF THE FOLLOWING NAV/AIDS CAN BE AUTO TUNED? A - ILS AND ADF (FOR NDB DATA BASE APPROACHES). B - VOR AND DME. C - BOTH ARE CORRECT.
77.- WHILE TAXIING ON THE GROUND, THE FMGS DISPLAYS THE POSTITION OF THE AIRCRAFT USING: A - IRS AND DME/DME. B - IRS ONLY. C - IRS AND VOR/DME. D - DME/DME AND VOR/DME.
78.- WILL THE AIRCRAFT CAPTURE AND NAVIGATE VIA THE ILS SIGNALS IF THE ILS PUSH BUTTON ON THE FCU IS NOT PUSHED? A - YES. B - NO.
79.- WITH THE AUTOPILOT ENGAGED, EITHER SIDESTICK CAN BE MOVED FREELY. A - TRUE. B - FALSE, MOVING EITHER SIDESTICK WILL CAUSE THE AUTOPILOT(S) TO DESENGAGED.
80.- WITH THE DATA SELECTOR SET TO HDG, THE TIME REMAINING UNTIL THE COMPLETED IRS ALIGNMENT IS DESPLAYED ON THE CONTROL DISPLAY. HOW LONG DOES IT TAKE NORMALLY? A - APPROXIMATELY 1 MINUTE. B - APPROXIMATELY 3 MINUTES. C - APPROXIMATELY 7 MINUTES. . D - APPROXIMATELY 10 MINUTES.
81.- YOU CAN DISENGAGE THE EXPEDITE MODE BY: A - PRESSING THE EXPED SWITCH ON THE FCU. B - ENGAGING ANOTHER VERTICAL MODE. C - EITHER A OR B.
82.- YOU HAVE BEEN CLEARED TO INTERCEPT THE LOCALIZER. YOU HAVE PUSHED THE LOC PUSH BUTTON ON THE FCU. IF ALL NECESSARY DATA HAS BEEN ENTERED IN THE MCDU, CAN YOU NOW ENGAGE BOTH AUTOPILOTS? A - NO, THE LOC MUST CAPTURE BEFORE BOTH AUTOPILOTS WILLL ENGAGE. B - YES. C - NO, THE APPR PUSHBUTTON MUST BE PUSHED.
83.- ZFW IS ENTERED ON: A - INIT B PAGE. B - PROG PAGE. C - PERF PAGE.
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