756 Additional Questions

A detailed cockpit dashboard of an airplane with various instruments and displays, showcasing aviation systems and controls in a modern aircraft, emphasizing a professional and educational atmosphere.

Aviation Systems Mastery Quiz

Test your knowledge of aviation systems with this comprehensive quiz designed for aviation enthusiasts and professionals alike! Featuring 42 multiple-choice questions, this quiz covers essential topics such as engine anti-ice, flight mode annunciations, and stabilizer trim systems, ensuring a robust understanding of critical aircraft operations.

Whether you're preparing for a certification, brushing up on your skills, or simply curious about aviation, this quiz will challenge you and enhance your knowledge!

  • 42 meticulously crafted questions
  • Instant feedback on your answers
  • Engaging and informative
42 Questions10 MinutesCreated by FlyingFalcon42
The ________ can be operated in flight only. It is inhibited on the ground.
Pitot Heat
Wing Anti Ice
Engine Anti-Ice
AOA Heat
The engine-anti ice valve is located upstream of the associated engine bleed air valve. When the associated engine bleed air valve is closed, engine anti-ice is:
Unavailable
Available
Available, only if the isolation valve(s) is open
Unavailable, if the isolation valve(s) is closed
The ____ probe is not heated on the ground.
CAPT PITOT
L AOA
TAT
R AOA
Operation of the ________ system is fully automatic.
Wing anti-ice
Flight deck window heat
Engine anti-ice
Probe heat
Flight mode annunciations (FMAs) are the only valid indication of the operating status of the auto throttle and/or AFDS. When the respective mode is engaged, annunciations appear in:
Green
White
Amber
Blue
Flight mode annunciations (FMAs) appear in _____ when the mode is armed for engagement.
Green
White
Amber
Blue
An AFDS pitch or roll mode fault is indicated in the flight mode annunciations (FMAs) by a:
Blue fMA
Green box around the mode
White FMA
Yellow line through the mode
The _____ provide the means for the pilot to make inputs to and control the FMCs.
PCP (Pilot Control Panel)
MCP (Mode Control Panel)
CDUs (Control Display Unit)
ACP (Audio Control Panel)
757/767: With the NAV Filter Selector in the RANGE position:
Only range audio (station identifiers) can be heard
Voice transmissions and station identifiers can be heard
Only voice transmissions can be heard
HF or SATCOM can be heard
757/767: There is no push-to-talk (PTT) switch on:
The control wheels
Any hand microphone
Flight Deck Handset
The audio control panels
757: The ENG FIRE/Overheat test Switch, when pushed and held, tests the:
Turbine and Strut Overheat Detection System
Engine fire and overheat detection system
APU fire detection system
Cargo fire detection system
757: The ENG/APU/CARGO test switch does not test the:
Cargo fire detection
Engine and fire overheat detection
APU fire detection
Turbine and strut overheat detection system
757/767: There are two engine fire extinguisher bottles. Which of the following statements is true?
Both bottles must be discharged into the same engine.
Only one bottle can be discharged into either engine.
Either or both bottles can be discharged into either engine.
An engine fire on the ground is automatically extinguished a few seconds later after automatic shutdown.
757: An APU fire on the ground with both engines shutdown requires what action?
Pulling the APU fire handle and rotating it in either direction
No action is required; the fire is automatically extinguished
The BTL DISCH switch is pushed on the APU Ground Control Fire Protection Panel
Pushing the fire override switch located beneath the fire handle
753/767: Each lavatory has a single smoke detector. If smoke is detected:
The LAV SMOKE light illuminates
There are no flight deck annunciations of smoke detected in any lavatory
EICAS advisory message LAVATORY SMOKE displays
EICAS Advisory message FIRE/OVHT SYS displays
757/767: The UNSCHED STAB TRIM light illuminates when:
One of the two stabilizer brakes failed to release when trimming the stabilizer trim switches
Fault in the Mach speed trim system
Stabilizer trim movement without signal from trim switches, Mach/speed trim system or autopilot
The engaged autopilot is in a degraded mode
757: When the TRAILING EDGE light illuminates, hydraulic power is removed from the drive unit(s) of the:
Flaps
Slats
Slats and Flaps
Slats, flaps, and spoilers
757/767: With the speed brake lever in the ARMED position, the ground spoilers automatically extend upon landing and the handle moves to the UP positions when three conditions are met, including:
The flaps are in the landing position
Both truck tilt sensors detect a no-tilt condition on the ground
Radio altitude is below 800 feet
The iRS senses the aircraft pitch at 1 degree or less
757/767: If pilots inadvertently activate aileron trim while an autopilot is engaged, the repositioning of the aileron neutral point:
Is not apparent until the autopilot is disengaged
Causes the autopilot to disengage
Causes the AIL LOCK light to illuminate
Is shown on the Control Wheel Aileron Trim indicator
757: If during the Before Takeoff Procedure, the stabilizer trim setting shown on FMC TAKEOFF REF page 1 is less than 3.0, what should be done?
Enter the CG printed on the Final Weight Manifest
Use the ALTN STAB TRIM switches
Use the Control Wheel mounted Pitch Trim Switches
Set stabilizer trim to 4.0
767: The Pitch Enhancement System (PES) provides a backup source of hydraulic power to operate the horizontal stabilizer if both the left and center hydraulic systems fail. When the PES operates, trim is only available from the:
Autopilots
Alternate trim switches
Backup trim switches
Control wheel trim switches
757/767: The three modes of stabilizer trim are:
Normal (control wheel), Alternate (control stand), Automatic (autopilot or Mach speed trim)
Electric (control wheel), Manual (control stand), Automatic (autopilot or Mach speed trim)
Electric (control wheel), Alternate (control stand), Automatic (autopilot or Mach speed trim)
Normal (control wheel), Backup (control stand), Electronic (autopilot or Mach speed trim)
757/767: If a single autopilot is engaged, ________ trimming causes the autopilot to disengage:
Electric
Allternate
Automatic
Aileron
757/767: The _____ trim switches are inhibited if multiple autopilots are engaged in the approach mode.
Rudder
Alternate
Electric
Aileron
767: In conjunction with trailing edge flap position 5 (or greater), which of the following will droop by being hydraulically driven to 50% down?
Spoilers
Outboard ailerons
Leading edge slats
Inboard ailerons
757/763: The double magenta symbol shown in the graphic indicates:
Rotation
Maneuvering speed
Command airspeed
Minimum maneuvering speed
757/763: The top of the amber bar shown in the graphic indicates:
Rotation speed
Maneuvering speed
Command airspeed
Minimum maneuvering speed
757/763: The speed trend vector shown in the graphic indicates predicted airspeed in _____ seconds:
5
10
15
20
757/763: The top of the red symbol shown in the graphic indicates:
Maximum speed
Maneuvering speed
Minimum operating speed
Minimum maneuvering speed
757/763: The bottom of the red symbol shown on the graphic indicates:
Maximum speed
Maneuvering speed
Minimum operating speed
Minimum maneuvering speed
757/767: Maximum speed is the maximum permissible airspeed as limited by the lowest of:
Vmo/Mmo, Landing gear placard speed, Flap placard speed
Vmo/Mmo, Maximum maneuvering speed, maximum approach speed
Maximum maneuvering speed, Maximum approach speed, Flap placard speed
Maximum maneuvering speed, Landing gear placard speed, Flap placard speed
757/763: The Vertical Pointer and Deviation Scale displays vertical deviation from the selected VNAV PATH during descent only. The scale indicates a deviation of:
+/- 300 feet
+/- 500 feet
+/- 600 feet
+/- 400 feet
757/763: The ______ ILS receiver provides information to the Standby Attitude Indicator:
Left
Center
Standby
Right
(763 6441-6677): As shown in the graphic, the F is displayed when valid DME is available from the:
ILS
FMC
VOR
ADF
757/763: If the DME(s) shown in the RDMI(s) is being received from a VOR or VORTAC it is depicted by:
An “L” prefix
An “F” prefix
No prefix
An “I” Prefix
757/763: RDMI(s) depict unreliable airspeed data with
A “U”
Dashes
A “D”
A blank display
757/767: The Master Warning Reset Switch, when pushed, silences most aural alerts, except:
Takeoff & Landing configuration warning, and autopilot disconnect warning
Cabin altitude warning, and overspeed warning
Engine fire warning, and APU fire warning
Auto throttle disconnect caution, and altitude alert caution
757/767: The cancel/recall buttons are powered by the ________. Should there be a loss of power to that bus, the pilots are prohibited from cycling through subsequent pages of EICAS messages.
Left main AC bus
Right main AC bus
Battery bus
Right main DC bus
757/767: The cancel/recall buttons allow certain alert messages to be displayed or removed, including:
Advisory, communication alert, and status messages
Caution, advisory, and warning messages
Advisory and communication alert messages
Caution and advisory messages
757/767: The AUTOPILOT DISC master warning light, EICAS warning message, and aural warning can be reset:
By choosing a different roll or pitch mode
By pushing either Master Warning reset switch
By pushing the autopilot disengage switch
By pushing the auto throttle disconnect switch
757/767: During cruise above ______, the crew alertness monitor determines pilot activity. When a predefined time elapses after the last control activation, the EICAS advisory message PILOT RESPONSE displays.
FL 200
FL 100
FL 250
FL 150
Status messages identify system faults affecting aircraft dispatch are not considered crew alerts. Normally, status messages that appear during flight do not require the execution of a non-normal checklist. The status message ________ requires execution of a non-normal checklist
FWD or AFT CARGO DET 1 or 2
L/R ENG OH LP 1 or 2
L/R STRUT OH DET 1 or 2
L/R ENG FIRE LP 1 or 2
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