FLIGHT ENGINEER PRACTICE EXAM

Click the appropriate answer and at the end of your exam click on the done button.

503 "IN ORDER TO PROTECT AIRCRAFT ELECTRICAL COMPONENTS, A MAIN AC GENERATOR SHOULD BE TURNED OFF IF ITS REDUCTION GEAR BOX RPM EXCEEDS:"
103.50%
106%
109%
115%

355 "WHEN RETARDING THE POWER LEVER THROUGH THE CROSSOVER POINT AND THE TIT INCREASES, THE FUEL CONTROL IS;"
RICH.
LEAN.
BYPASSING EXCESS FUEL BACK TO THE INLET SIDE OF THE TD VALVE.
NORMAL.

387 "WITH THE POWER LEVER ABOVE 66 DEGREES COORDINATOR AND ENGINE RPM BELOW 94%, THE TD SYSTEM CAN TAKE _________ OF THE NORMAL FUEL SCHEDULE."
15%
20%
50%
35%

397 THE RED ARCS ON THE DUAL HYDRAULIC QUANTITY GAGE SERVE AS A WARNING THAT:
MINIMUM QUANTITY EXISTS FOR SYSTEM OPERATION OF THE LANDING GEAR.
PUMP CAVITATION MAY OCCUR IF FLUID LOSS CONTINUES.
SYSTEM MUST BE REFILLED PRIOR TO FURTHER USE DUE TO FILTRATION.
THE PUMPS FED BY THAT RESERVOIR MUST BE LEFT OFF.

352 "A FLICKERING FUEL ""PRESS LOW"" CAUTION LIGHT INDICATES:"
A FAILURE OF THE PRIMARY OR SECONDARY PUMP.
AN OBSTRUCTED FUEL LINE.
THE LOW PRESSURE FUEL FILTERS ARE CLOGGED.
THE HIGH PRESSURE FUEL FILTERS ARE CLOGGED.

311 WITH A CRACKED FLIGHT STATION ESCAPE HATCH OPTICAL WINDOW YOU SHOULD:
"INNER PANEL, NO ACTION REQUIRED"
"REDUCE CABIN DIFFERENTIAL PRESSURE TO 2.0"" HG AND MAKE A NORMAL DESCENT TO 10,000 FEET OR LOWER."
"EVACUATE NONESSENTIAL CREW MEMBERS FROM IMMEDIATE AREA (ELECTRONIC RACK A1)."
BOTH 2 AND 3 ARE CORRECT

595 "WHEN THE POWER LEVERS ARE RETARDED ON LANDING ROLLOUT, THE ILLUMINATION OF THE BETA LIGHTS INDICATE:"
PITCHLOCK RESET IS NOW DEENERGIZED.
BLADE ANGLE IS NOW 10 DEGREES OR LESS.
BETA FOLLOW UP HAS BEEN SET TO 13 DEGREES BLADE ANGLE.
BOTH 1 AND 2 ARE CORRECT

384 "IF IT IS NECESSARY TO TAKEOFF OR FLY WITH FUEL IN TANK 5, BUT LESS THAN FULL WING TANKS:"
YOU MUST TRANSFER ALL FUEL FROM TANK 5 TO THE WING TANKS PRIOR TO TAKEOFF.
THE AIRCRAFT DESIGN LOAD FACTOR IS REDUCED FROM 3.0 G'S TO 2.1 G'S.
"THE WEIGHT OF THE FUEL IN TANK 5 MUST BE ADDED TO YOUR ZERO FUEL WEIGHT, TO ASCERTAIN THAT MAXIMUM
THE WEIGHT OF THE FUEL IN TANK 5 MUST BE ADDED TO THE ZERO FUEL WEIGHT TO COMPENSATE FOR THE EXCESSI

669 "WHEN DITCHING, THE FLIGHT ENGINEER EXITS OVER WING ON THE __________ SIDE OR THROUGH THE OVERHEAD HATCH AND BOARDS THE _____ LIFERAFT."
PORT / NO.1
PORT / NO.2
STARBOARD / NO.1
STARBOARD / NO.2

15 "TO PRECLUDE RADAR WAVEGUIDE PRESSURE FAILURES, THE RADOME SHALL NOT BE LOWERED INFLIGHT."
TRUE
FALSE