Topic 3: Wheels, Tires, and Breaks Flashcards
Since the correct operation of the landing gear is of the utmost importance, a number of ________ are included in the retraction and extension systems to ensure its correct operation under all conditions.
safety features
Since the correct operation of the landing gear is of the utmost importance, a number of safety features are included in the ________ and ________ systems to ensure its correct operation under all conditions.
retraction; extension
built-in to stop the gear being retracted when it’s not safe to do so and to warn the crew if they are attempting to land with the gear not
extended.
safety features
To avoid damage to the airframe structure, the ________ must always be aligned in the fore and aft direction prior to retraction.
nosewheel
A number of methods are used to ensure that safety features happen automatically. These are:
- hydraulic nose wheel centering on aircraft with powered steering; and
- self-centering cam system.
To prevent inadvertent retraction of the
landing gear when it’s not safe to do so, a ________ is incorporated which prevents the landing gear selector lever being selected up. This consists of a ________ which retains the selector in the down position and is released by the operation of an electrically operated solenoid.
safety device; mechanical lock
On smaller aircraft, electrical power to the solenoid is controlled by ________ mounted on the main gear shock absorber struts. When the struts are compressed, switches are ________ but as the struts extend after takeoff switch contacts ________ and the electrical supply to the solenoid is completed thus releasing the selector lever lock and allowing the landing gear to be selected up.
switches; open; close
On larger aircraft, a number of additional criteria have to be met before it is safe to raise
the gear. For instance, the ________ may have to be tilted to the correct angle and for the aircraft with body gear steering, the gear will have to be aligned ________ and ________. Only
then will the lever lock be released.
main gear trucks; fore; aft
A means of overriding the lock such as by _________ is provided for use in the event of _________ and for ________.
mechanical means; solenoid failure; maintenance purposes
A means of overriding the lock such as by mechanical means is provided for use in the event of solenoid failure and for maintenance purposes. Flight crews should exercise great care in using this bypass facility. Normally, it should only be used when called for in a checklist as raising the gear hydraulically when parts of it are incorrectly positioned can cause catastrophic damage to both the ________ and the _________.
gear; airframe
further safety features which are intended to prevent inadvertent retraction of the gear when the aircraft is on the ground.
landing gear ground locks or locking pins
They will usually consist of pins or metal sleeves which interfere with the operation of the gear in such a way that it is impossible for the gear to move when they are in position.
landing gear ground locks or locking pins
They are fitted with warning flags which help prevent the crew from inadvertently getting airborne with them still in position on the gear.
landing gear ground locks or locking pins
To guard against landing with the landing gear not locked down an _________ is incorporated in the system.
aural warning
often provided to allow certain flight exercises
to be carried out without unnecessary warnings.
aural warning isolation switch
Different aircraft types use different criteria for the operation of the aural warning and isolation switch. These normally involve a combination of _________ positions.
flap and throttle
If fitted, this will give a “too low” gear warning when passing a specified radio altitude with the gear not locked down.
enhanced ground proximity warning system or EGPWS
A means of lowering the landing gear and locking it in the down position is provided to cater for the possibility of _________.
failure in the normal system
In most modern aircraft, the up locks may be released ________ as in the case of the Boeing 747 where the switches control electric motors which operate up locks or ________ as in the case of the Boeing 737 where the handles in the cockpit are connected by cables to the up-lock release mechanisms.
electrically; mechanically
once the up locks have been released, the _________ lowers or free falls under its own weight and the _________ are engaged mechanically by springs.
landing gear; down locks
pulling the handle to the _________ detent releases the door up lock allowing the door to fall open.
first
Pulling the handle to the _________ detent
releases the gear up lock which allows
the gear to drop to the down position.
second
A _________ in the down lock actuator forces the over center mechanism into the locked down position.
heavy spring
If the gear has been lowered by the free fall method, there will be _________ available to close the ________ after extension so they will remain open, and the door open light will remain illuminated.
no power; hydraulically operated doors