b757 review questions. engines and apu what conditions cause the engine to increase from minimum...
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Engines and APU
• What conditions cause the engine to increase from minimum idle to approach idle and how long does approach idle maintained during the
landing rollout?
• When the engine anti-ice is activated, or the landing gear is down, or the flaps are set to 25 or 30 degrees. The engine remains in approach
idle for 5 seconds after touchdown.
Engines and APU
• What is the effect of CLIMB 1 on the TMC?
• When CLIMB 1 is selected, approximately 94% of the normal climb power is supplied
by the engines.
Engines and APU
• TRUE / FALSE: Raising either thrust reverser handle shuts off the auto throttle
system
• True
Engines and APU
• What is the primary purpose of the EEC, and ELC system?
• Over-boost protections, and Over-speed protection respectively.
Engines and APU
• The thrust reverser status indicator is AMBER, what is the position of the
associated reverser?
• The reverser is unlocked or is in transit.
Engines and APU
• What is the function of the thrust management computer?
• Calculates a reference EPR based on existing pressure altitude and ambient
temperature data from the air data computer for Takeoff.
Engines and APU
• What is the function of the TO/GA switch on the TMSP?
• It is used to select takeoff thrust on the ground and go-around thrust in flight.
Engines and APU
• What engine indications are displayed on the EICAS secondary display?
• N2, N3, fuel flow, oil pressure, oil temperature, oil quantity, and engine
vibrations.
Engines and APU
• TRUE FALSE: Normal APU start consists of two flashes of RUN and one flash of a
FAULT light
• True
Engines and APU
• In flight with APU running you shut off the battery, does this cause the APU to
shutdown?
• No
Engines and APU
• What is indicated when the engine fuel valves and/or spar valves are illuminated?
• The valves are not in agreement with the fuel control switch, or the respective fire
switch.
Engines and APU
• What is the function of the engine start selector switched to GND?
• Opens the start valve, arms the selected igniter.
Engines and APU
• What is the function of the start selector in AUTO?
• Closes start valve and terminates ignition. Selected igniters operate continuously with flaps extended and/or engine anti/ice ON.
Engines and APU
• What is the normal starter duty cycle?
• Three cycles of up to 2 minutes continuous operation and run down to N3 0%, followed
by 15 minutes of cooling.
Engines and APU
• What is the extended engine starter duty cycle?
• Up to 4 minutes operation followed by a 15 minute cool down.
Engines and APU
• When would you expect the engines to be in low idle?
• When in ground operation, if flight with gear up, flaps less than 25 degrees, and
engine anti ice off.
Engines and APU
• Under what condition is the APU time-delay feature bypassed during APU
shutdown?
• If the APU bleed has already been closed for 60 seconds.
Engines and APU
• What is the function of the APU battery?
• Electrical power for starter, inlet door, and control circuitry
Engines and APU
• What is the function of the aircraft battery in relation to APU operation?
• Provides electrical power for fire protection, fuel valve operation, DC fuel pump, and
control circuitry backup.
Engines and APU
• What is maximum altitude for APU electrical and pneumatic power?
• 42,000’, and 17,000’ respectively
Engines and APU
• What would the illumination of the APU amber fault light indicate?
• APU fuel valve is not in commanded position, or the APU has shut down due to a
fire or fault.
Engines and APU
• What does the blinking RUN light indicate on APU startup
• A self test of the control circuitry
Engines and APU
• What lights illuminated when the oil pressure is at or below minimums, i.e. the
red line (18psi)?
• ENG OIL PRESS
Engines and APU
• What does the D-TO above the EPR mean on the upper EICAS during takeoff
• A de-rated takeoff using FLEX temperature is scheduled
Engines and APU
• The intermediate pressure compressor section and the intermediate pressure
turbine on a common shaft on the rotor.
• N2.
Engines and APU
• Except during takeoff or go around, if the normal operating range of engine
parameters is exceeded the indicators change from ?
• White to amber or red - as appropriate.
Engines and APU
• If the Secondary Engine display is not in view when the engine vibrations
exceeds_____ , the vibration monitors will automatically display
• 2.5 units
Engines and APU
• During takeoff or go-around, N1, EGT, N2 and N3 remain white for _______after the
amber band is reached and _______for single engine operation.
• 5 minutes; 10 minutes
Engines and APU
• The engine is available for unrestricted use even though the oil temperature is _____in
the band?
• Amber
Engines and APU
• The engines are ______axial flow turbofans of high compression and bypass ratio and
are rated at ________pounds of thrust
• Three-rotor; 42,700
Engines and APU
• Is it normal for the APU FAULT to illuminate temporarily during APU start or
shutdown?
• Yes.
Engines and APU
• TRUE/FALSE: With the APU operating on the ground, and the Battery Switch selected to OFF, the fire detection continues to be
available until the APU actually shuts down?
• False
Engines and APU
• During APU start, the Fault light comes on and goes off as an indication that?
• The fuel valve opened
Engines and APU
• If the APU has been selected to shut down, but the RUN light is still illuminated, the
shutdown cycle can be canceled by ?
• Momentarily rotating the APU selector to START
Engines and APU
• During APU start the APU battery powers the ?
• APU starter motor, the APU control circuitry, and operates the air inlet door.