FLIGHT ENGINEER PRACTICE EXAM

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

645 "IF DURING FLIGHT, THE #3 PROPELLER RPM STABLIZES AT 97% AND IS AUDIBLE AND THE USE OF THE SYNC SYSTEM DOES NOT CORRECT THE UNDERSPEED;"
"PULL THE ""E"" HANDLE."
OPERATION MAY BE CONTINUED.
NULL THE TD.
DO NOT ATTEMPT TO FEATHER DUE TO PROPELLER CONTROL FLUID LEAKAGE.

17 "IF THE RADOME HYDRAULIC SYSTEM SELECTOR VALVE GOES TO A NEUTRAL POSITION OR MALFUNCTIONS, IT IS POSSIBLE TO RECEIVE A BYPASS IN THE ___________."
NO. 1 HYD SYSTEM
NO. 2 HYD SYSTEM
IT IS NOT POSSIBLE FOR THE SYSTEM TO BYPASS PRESSURE.
BOTH 1 AND 2 ARE CORRECT.

139 "NORMAL POWER TO THE PILOTS TURN AND BANK INDICATOR IS _______________, WITH BACKUP POWER OF _______________________."
"FLIGHT DC, MONITORABLE ESSENTIAL DC"
"MONITORABLE ESSENTIAL DC, FLIGHT DC"
"FLIGHT DC, FLIGHT AC"
"MONITORABLE ESSENTIAL DC, FLIGHT AC"

660 THE COMMAND TO EXECUTE BAILOUT IS ANNOUNCED:
VERBALLY AND FOUR SHORT RINGS ON THE COMMAND BELL.
VERBALLY ONLY.
"VERBALLY AND ONE LONG RING (10 SECONDS OR LONGER) ON THE COMMAND BELL."
"ONE LONG RING ON THE COMMAND BELL, ONLY."

298 "DURING PROPELLER DEICE OPERATION, FAILURE OF ONE SPINNER TO FUNCTION WILL CAUSE:"
"THE ""MASTER DEICE"" LIGHT TO ILLUMINATE."
REDUCED AMPERAGE (APPROXIMATELY HALF) WHEN THAT SPINNER IS SELECTED ON THE PROPELLER DEICE AMMETER.
THE ENTIRE DEICE SYSTEM TO SHUT DOWN UNTIL THE SPINNER IS REPAIRED.
HAS NO EFFECT ON PROPELLER DEICE OPERATION.

89 "WHEN TAXIING BACK FOR TAKEOFF AFTER A FULL STOP LANDING, THE #4 ENGINE PROP PUMP 2 LIGHT IS ON IN LOW RPM."
"THIS IS CAUSED BY LOWER PROP PUMP OUTPUT AND HIGHER OIL TEMPS ASSOCATED WITH LOW RPM. IF THE PROPE
"PERFORM FUEL GOVERNOR PITCHLOCK & REVERSE SHAFT HORSEPOWER CHECK AND CLOSELY MONITOR RPM. IF RPM I
"VERIFY PROPER OPERATION OF PROPELLER THROUGHOUT GROUND RANGE. IF PROPELLER OPERATES NORMMALLY, CON
RETURN TO THE LINE AND SECURE THE ENGINE. MAINTENANCE ACTION IS REQURIED.

308 "WITH A ""LE HOT"" LIGHT ON, THE FOLLOWING IS TRUE:"
INDICATES AIR TEMPERATURE IN THE PLENUM AREA EXCEEDS SAFE LIMITS. (BROKEN DUCT) SECURE WING DEICE A
"INDICATES WING LEADING EDGE SKIN TEMPERATURE HAS INCREASED ABOVE 110 DEGREES C, DUE TO A MODULATING
"INDICATES EITHER A PARTING OR CYCLING STRIP POWER RELAY HAS DEENERGIZED, TURN SWITCH ""OFF"" THEN "
INDICATES THAT THE MODULATING VALVES ARE SIMPLY IN TRANSIT FROM THE OPEN TO CLOSED OR CLOSED TO OPEN

223 "IF THE THREE PHASE AC CIRCUIT BREAKER BEHIND THE COPILOT TRIPPED PRIOR TO TURNING ON THE APU GENERATOR (DURING PREFLIGHT), WHAT AC BUS OR BUSES WILL RECEIVE POWER WHEN THE APU GENERATOR IS TURNED ON ?"
"FLT ESS AC, MAIN AC BUS A, AND MAIN AC BUS B."
"MON ESS AC, MAIN AC BUS A, AND MAIN AC BUS B."
FLT ESS AC ONLY.
MON ESS AC ONLY.

396 THE FLUID IN THE AIRCRAFT 2 MAIN HYDRAULIC SYSTEMS IS FILTERED PRIOR TO LEAVING THE RESERVIORS.
TRUE
FALSE

621 NTS IS DISARMED BELOW ____ DEGREES COORDINATOR BY THE:
24 ; BETA SET CAM
28 ; FEATHER AND DISARM CAM
24 ; FEATHER AND DISARM CAM
32 ; ALPHA BACKUP CAM