Aircraft Familiarization Flashcards
Regarding turning radius, what is the minimum pavement width for a 180-degree turn?
60ft
The 2 SPDA’s are located where?
1 in the forward electronics bay,
#2 in the center electronics bay
(Secondary Power Distribution Assemblies)
The maximum fuel quantity (in pounds), including unusable, is _____.
20,935 lbs
How many display units (DUs) are in the flight deck?
5
The flight deck is designed under which of the following concepts?
Dark and Quiet concept
In flight, when all aircraft systems are operating normally, you should expect which of the following?
No lights are illuminated on the overhead panel, main panel, glareshield, or control pedestal;
selector knobs in 12’ o-clock position;
and no aural warnings have been issued
The engines are considered “high bypass turbofans”, which makes them extremely efficient. Approximately what percent of air is actually being bypassed around the Core?
80% goes around/bypass - 20% goes through the engine
(.8)
Where is the fixed ELT located?
near the tail
or
aft pressure bulkhead
True or False: Both the Captain’s and First Officers side consoles have a
nosewheel steering tiller.
False
Each engine produces up to _____ lbs. of thrust.
14,500 lbs thrust single engine
This aircraft is equipped with General Electric _____ engines.
CF34-8E
True or False: If one stick shaker activates inadvertently (stick shaker failure),
nothing can be done in-flight. You must be on the ground to activate the shaker cutout feature.
False (15.2 Vol 2)
True or False: A white striped bar illuminates in a button when that button is not in the normal position.
True
The master WARN and master CAUT switchlights are located on the _____.
glareshield
The EICAS provides the flight crew with a ____-level alert messaging system.
4
True or False: The rudder pedals are in a fixed position and cannot be adjusted.
False
True or False: Failure of an SPDA would be indicated via an EICAS message.
True (Advisory level message) [Secondary Power Distribution Assemblies]
What does EICAS stand for?
Engine Indication and Crew Alerting System
True or False: The aircraft has overwing emergency exits for evacuation purposes.
False
Which of the following is true with regard to a “ramp horn”?
The aircraft has a ramp horn and there is a button for it on the Captain’s and First Officer’s side
The aircraft is equipped with _______ passenger and _______ service plug-type
doors that operate in an identical manner.
2, 2
[left side passenger doors, right side service doors]
True or False: The forward passenger door is the main boarding door, while the aft passenger door can be used as an emergency exit and for galley servicing.
True
Which of the following is true regarding the number and location of the Modular Avionics Units (MAU’s)
3 MAU’s in forward and center E-bays
(MAU 1 and 2 are located in the forward electronics bay and MAU 3 is located in the center electronics bay.)
True or False: There is only one cargo compartment on the aircraft.
False
