Aircraft General Flashcards
(42 cards)
The emergency lighting system is powered by:
Remote Batteries
The fasten seat belt signs will automatically illuminate when the SEAT BELT SIGNS switch is in AUTO position and…
the landing gear not up and locked.
the flap lever at 5 or greater.
below 10,000 feet MSL.
—–> All of the above conditions are correct.
The oxygen mask microphone can be tested without removing it from the storage box. T/F
T
The passenger oxygen masks automatically drop from the PSU’s prior to the cabin reaching…
10,000 feet.
12,000 feet.
14,500 feet.
9,000 feet.
14,500 feet.
The EICAS advisory message EMER LIGHTS is displayed when…
-the emergency lights switch is not in the ARMED position.
-the emergency lights are on.
Both are correct
A/an _______ light will illuminate on the flight deck access keypad when the door lock is commanded locked.
-green
-amber
-red
-white
Red
The flight deck door incorporates a ______________ system used to secure the flight deck when power is not available to the electronic locking system.
-security grill
-security panel
-keyed mechanical deadbolt
-backup battery power
keyed mechanical deadbolt
During an emergency egress situation, the flight deck crew is able to egress the aircraft using the…
-flight deck overhead door.
-emergency escape ropes.
-E&E compartment escape hatch.
-left and right sliding windows.
flight deck overhead door.
Opening the cargo doors turns off cargo compartment fire detection. T/F
False
The nose gear landing lights are inhibited until…
-the nose landing gear is down and locked.
-all landing gear are down and locked.
-the nose landing gear is out of up.
-the landing gear handle is placed in the down position.
the nose landing gear is down and locked.
Taxi lights are installed on the non-steerable portion of the nose strut. To add lighting during ground roll, taxi lights are illuminated when the nose gear landing lights are ON. T/F
True
The MASTER BRIGHTNESS control provides the means of controlling some panel and display lighting brightness with the use of one control. The control is turned on when the MASTER BRIGHTNESS control is pushed on. Individual lighting controls for the displays and panels have a center detent identified by a…
-white dot at the middle adjustment position.
-white diamond at the middle adjustment position.
-red dot at the middle adjustment position.
-white C next to the appropriate lighting control switch.
white dot at the middle adjustment position.
Passenger cabin lighting near the flight deck door is __________________ when the flight deck door is opened with an engine operating.
-automatically extinguished
-switched to a low intensity red light
-automatically dimmed
-automatically positioned to full bright
automatically dimmed
The 787 is equipped with ____ slide rafts.
8
Regarding the passenger entry doors, …
-with low differential pressure, it is possible to open the door in flight.
-the door handle is locked in the closed position when airspeed is above 90 knots and can not be moved.
-At high differential pressure, the vent can not be opened with handle rotation.
-each door handle is automatically locked when groundspeed is greater than 80 knots.
each door handle is automatically locked when groundspeed is greater than 80 knots.
Each passenger entry door flight lock is unlocked when electrical power is removed or failed or when groundspeed is less than…
70 Kts
The Flight Attendant Crew Rest area can be occupied for Taxi, Takeoff and/or Landing. T/F?
False
The overhead flight crew rest area oxygen system uses the flight deck oxygen bottles as its source. T/F?
False
According to the Airplane General section of the ASM the minimum pavement width for a 180 degree turn for a 787-8 is…
138 feet, 4 inches.
While conducting a battery power only start-up sequence the left Common Computing Resource (CCR) is online when…
-the APU RUNNING message is displayed for 15 seconds on the PFD.
-the EICAS advisory message CCS NORM is displayed on the MFD.
-the captain’s inboard and lower display unit show the default format.
-the APU CONTOL advisory message is displayed on the EICAS.
-the captain’s inboard and lower display unit show the default format.
The flight deck overhead door is hinged to fall ___________ when opened. After egress, descent from the flight deck to the ground is accomplished by _________.
-inward, sliding down a rope that is secured to the aircraft after first throwing it out the open door
-outward, securely fastening the bungee cord around your waste and jumping off the top of the flight deck
-outward, securely holding the securely fastened descent device handle through all egress steps until safely on the ground
-inward, securely holding the descent device handle through all egress steps until safely on the ground
inward, securely holding the descent device handle through all egress steps until safely on the ground
With external power available (AVAIL displayed on either forward EXT PWR switch), the left Common Computing Resource (CCR) begins a start up cycle approximately _________ in duration followed by the right CCR.
-2-3 minutes
-60 seconds
-90 seconds
-4 minutes
2-3 minutes
The right Common Computing Resource (CCR) will not begin the start-up cycle until a power source other than the battery is available. Both CCRs are on-line when…
-the captain’s inboard and lower display units show the default format (CDU pages).
-the First Officer’s inboard and outboard display units show the default format (CDU pages).
-all displays and HUD combiners show their default formats.
-the lower display unit shows the default format.
all displays and HUD combiners show their default formats.
Passenger oxygen masks automatically drop from the passenger service units (PSUs) prior to the cabin reaching the greater of…
-15,000 feet, or origin airfield altitude +1000 feet, or destination airfield altitude +1000 feet.
-14,500 feet, or origin airfield altitude +1500 feet, or destination airfield altitude +1500 feet.
-14,000 feet, or origin airfield altitude +1000 feet, or destination airfield altitude +1000 feet.
-13,000 feet, or origin airfield altitude +1000 feet, or destination airfield altitude +2000 feet.
14,500 feet, or origin airfield altitude +1500 feet, or destination airfield altitude +1500 feet.