FLIGHT ENGINEER PRACTICE EXAM

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195 _______________ IS BASED ON THREE ENGINES OPERATING AT GROUND IDLE AND A MAXIMUM TRUE GROUND SPEED FOR BRAKING DEPENDING ON AIRCRAFT GROSS WEIGHT.
DECISION SPEED
REFUSAL SPEED
VMC GROUND
CRITICAL FIELD LENGTH

329 THE ICING LIGHT ON THE PILOT'S VERTICAL ANNUNCIATOR PANEL INDICATES:
ALERT OR FAULT IN DEICING SYSTEM OR BOMB BAY HEATING SYSTEM.
ICE DETECTOR PROBE ACCUMULATING ICE. THE FREQUENCY OF THE LIGHT INDICATES THE AMOUNT OF ICE BUILDUP
BOMB BAY COLD.
"ICING CONDITIONS. THE LONGER THE LIGHT REMAINS ON, THE LONGER THE PROP DEICE WILL BE REQUIRED."

57 "A SPRING-LOADED, SOLENOID OPERATED MANIFOLD DRAIN VALVE IS LOCTED AT THE FUEL MANIFOLD. IT DRAINS THE FUEL MANIFOLD WHEN FUEL PRESSURE DROPS BELOW _____ TO ____ PSI."
2-4 PSI
8-10 PSI
7.5- 19.5 PSI
4-8 PSI

67 THE CABIN PRESSURE RELIEF VALVE PREVENTS A DANGEROUS BUILDUP OF CABIN PRESSURE IN THE EVENT OF A MALFUNCTION IN THE:
DIFFERENTIAL SYSTEM.
ISOBARIC SYSTEM.
NEGATIVE PRESSURE RELIEF VALVE.
RATE CONTROL KNOB.

5 THE FLOW CONTROL VANES IN THE ENGINE DRIVEN COMPRESSORS (EDC'S) ARE CONTROLLED BY PITOT AND STATIC PRESSURE. THEY ARE ALMOST CLOSED AT SEA LEVEL AND WILL GRADUALLY OPEN AS THE AIRCRAFT CLIMBS TO COMPENSATE FOR THE THINNER AIR AT HIGHER ALTITUDES.
TRUE
FALSE

458 "WHENEVER EXCESSIVE BRAKING IS UTILIZED DURING TAXI, AFTER TAKEOFF THE LANDING GEAR RETRACTION SHOULD BE DELAYED _____ MINUTES TO ALLOW FOR COOLING OF THE BRAKES."
1
2
3
5

391 NOSE WHEEL STEERING IS POWERED BY THE NO.1 HYDRAULIC SYSTEM. THIS HYDRAULIC PRESSURE IS SHUT OFF WHEN:
THE LANDING GEAR IS IN THE DOWN AND LOCKED POSITION.
WEIGHT OF THE AIRCRAFT IS OFF THE LANDING GEAR.
THE LANDING GEAR SELECTOR VALVE IS IN ANY POSITION EXCEPT DOWN.
THE LANDING GEAR IS BEING EXTENDED.

695 "PRIOR TO OPERATING THE APU, THE MINIMUM FUEL REQUIRED IN TANKS 2 & 3 SHOULD BE?"
"1,000 LBS"
"2,000 LBS"
5025 LBS
NO MINIMUM FUEL REQUIREMENT

446 "DURING FLIGHT YOU ARE UNABLE TO SHIFT A BOOST PACKAGE, YOU SHOULD:"
"SECURE HYDRAULIC PRESSURE, THEN SHIFT THE OTHER TWO CHANNELS BOOST OUT."
"SHIFT THE OTHER TWO CHANNELS BOOST OUT, THEN SECURE HYDRAULIC PRESSURE."
"ENGAGE THE AUTOPILOT, THEN GO BOOST OUT ON OTHER TWO CHANNELS."
BOTH 2 AND 3 ARE CORRECT.

493 THE PITCHLOCK RESET MECHANISM WILL RESET PITCHLOCK RPM TO _______ %.
103.5
106
109
103.8