2nd half Exercise questions Flashcards
Bleed-air systems are used to extract air from jet engine compressors for ____,____, and ____ the aircraft.
Air Conditioning,
Pressurization System,
Anti-Ice System
The bleed air is extracted from the engine compressor or the…
APU
Aircraft Engines
External Air Carts
____ provide the means of routing extracted air from the air source to the various components
bleed air manifold
The purpose of the ____ is to maintain a cabin altitude that provides comfort and safety for the crew and passengers
Pressurization
What is the principal controlling component of the pressurization system?
Outflow Valve
The ___ valve prevents the cabin pressure from exceeding the design limits of the aircraft structure.
Relief
What will automatically activate when the cabin altitude reaches a predetermined limit?
Cabin Altitude Warning System
The most common bleed air systems
The air conditioning system,
The pressurization system,
The Anti-Ice System
The three sources of bleed air
Aircraft engines,
APU
External Air cart
____ is The principal controlling component of the pressurization system
Outflow Valve
____ is An over-pressure safety valve that prevents the cabin pressure from exceeding the design limits of the aircraft structure.
Relief Valve
Usually consisting of warning horns or bells and annunciator light.
Cabin Altitude Warning System
___ &___ will activate automatically whenever the cabin altitude reaches a predetermined limit
Warning & Lights
The Cabin Altitude Warning System will automatically…
Make cabin lights go full bright &/or deploy passenger oxygen systems.
MLG and NLG stands for
Main Landing Gear & Nose Landing Gear
The ___ absorbs the shock of landing.
Shock Strut
___ is a two-position control marked “UP” & “DOWN”
The landing Gear control lever
pilots use the ___ to assist nose wheel steering and to make minor inputs during taxi and parking.
Steering control wheel “Tiller”
The landing gear warning horn will be triggered when?
When the aircraft is approaching landing conditions and landing gear is not down
The landing gear is ___ controlled and ___ operated for extension and retraction
Electronically; hydraulically
The main cushioning component of the landing gear is the
Shock strut
When two or more wheels are attached to a single shock strut
Bogie
they help absorb the shock of the landing and cushion the forces felt during taxi and takeoff
Wheels & Tires
The left and right side brakes can be operated independently of each other, a capability called
Differential Steering
The left and right side brakes can be operated independently of each other, a capability called
Differential Steering
rudder pedals are normally a flight control, but they can also steer the
NLG
aircraft landing gear are ___ controlled and ___ operated
Electronically; Hydraulically
normally located inside the landing gear control lever. it illuminates whenever the landing gear is not in the same position as the landing gear control lever.
The landing gear warning light
As the gear starts to move, the landing gear warning light will turn on since
the landing gear is in transit
Modern landing gear indicators light: Green
indicates that the gear is down and locked for landing