VNAV MAY BE ARMED ON THE MCP PRIOR TO TAKEOFF PROVIDED THE FOLLOWING REQUIREMENTS: A VALID FLIGHT PLAN HAS BEEN ENTERED. ALL ANSWER ARE CORRECT. PERFORMANCE DATA BEEN ENTERED AND EXECUTED BOTH FLIGHT DIRECTOR SWITCHES HAVE BEEN SWITCHED ON TARGET SPEEDS WILL FOLLOW THE PROFILE LISTED IN THE CLIMB PAGE.
FOR VNAV DEPARTURE AND VNAV ARMED ON THE FMA, THE FCC WILL AUTOMATICALLY ENGAGE VNAV AT: 400 FEET ABOVE THE RUNWAY (LFE) 1000 FEET ABOVE THE RUNWAY (LFE) 50 ABOVE THE RUNWAY (LFE) 800 FEET ABOVE THE RUNWAY (LFE).
NOISE ABATEMENT PROCEDURE MAY BE ACCOMPLISHED BY EITHER LVL CHANGE OR VNAV: TRUE FALSE.
LNAV CAN BE SELECTED AT: 100 FEET AGL GROUND LEVEL PRIOR TAKE OFF ROLL. 300 FEET AGL. 200 FEET AGL.
AFTER DEVIATION FROM THE SELECTED ALTITUDE, WHEN DOES THE ALT ALERT LIGHT EXTINGUISH? 200 FEET BEFORE THE SELECTED ALTITUDE WHEN YOU LEVEL OFF AT SELECTED ALTITUDE. 300 FEET BEFORE THE SELECTED ALTITUDE.
DURING APPROACHING TRANSITION LEVEL, THE PM CALL: (TRANSITION LEVEL, ALTIMETER_______SET) TRUE FALSE.
MAXIMUM AIRSPEED FOR SEVERE TURBULENCE ONLY DURING CLIMB AND DESCENT: 0.76/280/250 KTS USE FMC RECOMMENDED THRUST SETTINGS. 0.82/340 KTS.
DURING LANDING ROLL IF THE SPEED BRAKE LEVER IS NOT UP, THE PM CALL: “SPEED BRAKES RETRACTED”. “SPEED BRAKES NOT UP”. “SPEED BRAKES MANUAL”. “SPEED BRAKES DOWN”.
IF AN ENGINE FIRE-ENGINE, SEVERE DAMAGE OR SEPARATION OCCURS AFTER V1, THE PM MUST FIRST EXECUTE: QUICK REFERENCE CARD (QRC), THEN QRH PROCEDURE. QRH PROCEDURE, THEN QUICK REFERENCE CARD (QRC). FLIGHT MANUAL B-737, THEN QUICK REFERENCE CARD (QRC) TECHNICAL BULLETING, THEN QRH PROCEDURE.
DURING LANDING ROLL THE PM MUST ANNOUNCE THE FOLLOWING SPEED CALL OUT: THERE IS NOT SPEED CALL OUT. 60 KNOTS. 80 KNOTS.
THIS IS THE MEMORY ITEM FOR ABORTED ENGINE START: CALL FOR NON-NORMAL QUICK REFERENCE CARD (QRC) ENGINE START SWITCH (AFFECTED ENGINE) …….CUTOFF ENGINE START LEVER (AFFECTED ENGINE) ……..CUTOFF.
AUTO-LAND CAPABILITY MAY ONLY BE USED WITH FLAPS 30 OR 15 AND BOTH ENGINES? FALSE TRUE.
ENGINE COOL DOWN PERIOD PRIOR TO SHUTDOWN IS: 3 MIN 2 MIN.
THE ENGINE OUT ACCELERATION HEIGHT MAY BE MANUALLY ENTERED FOR VNAV DEPARTURES IN THE FMC ON: ROUTE PAGE CLIMB PAGE N1 LIMIT PAGE TAKEOFF REF PAGE 2.
THE PILOT FLYING SHOULD CALL FOR THE DESCENT CHECKLIST AT APPROXIMATELY: 10 MINUTES BEFORE THE TOP OF DESCENT STARTING THE DESCENT 5 MINUTES BEFORE THE TOP OF DESCENT 10 MILES BEFORE THE TOP OF DESCENT.
THE SLIP SKID INDICATION OF THE ATTITUDE INDICATOR WILL TURN AMBER IF BANK ANGLE IS 35 DEGREES OR MORE. TRUE FALSE.
THE RISING RUNWAY IS DISPLAYED WHEN LOCALIZER POINTER IS IN VIEW AND RADIO ALTITUDE IS LESS THAN ________ FEET. 2500 500.
UNDER WHICH CONDITIONS REDUCED THRUST IS NOT BE USED. WIND SHEAR REPORTED. ENGINE OR WING ANTI-ICE ON. CONTAMINTED RUNWAY TAILWIND (MORE THAN 10 KNOTS.) ALL ANSWERS ARE CORRECT.
MAXIMUM TAKEOFF AND LANDING ALTITUDE: 17.000FT. 10.000FT. THERE IS NO LIMITATION. 41.000FT.
THE FMC ADVISORY MESSAGE “DRAG REQUIRED” INDICATE THE AIRPLANE IS _______KNOTS OR MORE ABOVE THE FMC TARGET SPEED OR WITHIN______ KNOTS OF VMO/MMO. 5 & 8 10 & 8 10 & 5.
THE FMC ADVISORY MESSAGE “BUFFET ALERT” INDICATE: CLEAR AIR TURBULENCE HAS BEEN DETECTED IN THE IMMEDIATE FLIGHT PLAN. THE AIRPLANE IS AN PARTIAL OR FULL STALL. CURRENT CONDITIONS RESULT IN A MANEUVER MARGIN LESS THAN SPECIFIED.
THE CIRCUIT BREAKER PROCEDURES ARE DIVIDED INTO ALL ANSWERS ARE CORRECT. PREFLIGHT BEFORE BLOCK OUT FROM TAKEOFF TO BLOCK IN AFTER BLOCK OUT AND BEFORE TAKEOFF.
IF THE LATITUDE/LONGITUDE POSITIONS IS NOT WITHIN 4NM OF THE AIRPORT, THE CDU SCRATCHPAD MESSAGE VERIFY POSITION IS DISPLAYED.? TRUE FALSE.
A FAST REALIGNMENT WILL CORRECT ACCUMULATED IRS POSITION ERRORS AND DRIFT ERRORS? TRUE FALSE.
IF ENGAGED THE AUTO-THROTTLE WILL DISENGAGED ____ AFTER LANDING TOUCHDOWN. 5 SECONDS 2 SECONDS.
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