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
The ________ and ________ of an aircraft support it when on the ground and to provide it with a means of mobility for takeoff, landing, and taxiing.
wheels; tires
help to cushion the aircraft from shocks due to irregularities in the ground surface (bumps) and take some of the shock on landing.
pneumatic tires
The ________ and in a small number of cases, the ________, house brake units which control the movement of the aircraft on the ground and provide a means of deceleration on landing.
main wheels; nose wheels
Because aircraft tires are usually _________ and _________ than the tires found on cars, they also have to be specially designed to facilitate _________.
larger; stiffer; tire replacement
two types of wheels in common use:
- loose or detachable flange type
- divided wheel
Both wheel types are made with one flange integral with wheel body and the other a separate removable part which is machined to fit over the wheel rim.
loose and detachable flange type
The difference between the loose and the detachable flange tires is the method by which the removable flange is ________. In the ________, the flange is retained by a locking device on the wheel rim and held in place by the tire pressure. In the ________ of wheel, the flange is secured to the wheel body by nuts and bolts.
secured; loose flange type; detachable flange type
this maybe a single piece or two or three pieces bolted together.
detachable flange
advantage of the loose or the detachable flange type of wheel:
the tire can be changed without removing the wheel from the aircraft.
The type of wheel most usually found on aircraft.
divided wheel
It consists of two half wheels matched up and joined together by bolts which passed through the two halves.
divided wheel
an example of a divided wheel is having a _________ to prevent abrasion between the two halves and provide an airtight fit.
seal incorporated at the joint
When in service, particularly during heavy braking, there is a tendency for the tire to rotate or ________ around the wheel.
creep
this, if excessive, will tear out the inflation valve on a wheel fitted with an inner tube causing the tire to burst.
creep
less likely to occur if the tire gas pressure is correctly maintained.
creep
In prevention of creep, one method is that wheels are often produced with a _________. The ________ of the wheel flange is milled so that the side pressure of the tire locks the tire walls to the flange.
knurled flange; inner face
Other method involves making wheel rim _________ so that the flange area has a greater diameter than at the center of the rim. When the tire is inflated, the _________ forces the tire outwards to grip the rim.
tapered; side pressure
Under extra hard braking conditions, the heat generated in the wheel tire and brake assembly can be sufficient to cause the pressure to rise to a level that the tire cannot withstand causing it to split with possible catastrophic consequences for the aircraft. This is commonly known as a ________.
tire blowout
To prevent a sudden blow out, these are fitted in some wheels.
fusible plugs or thermal plugs
These plugs are screwed into holes in the wheel rim.
fusible plugs or thermal plugs
They are sealed by a piston which is held in position in the plug by a fusible alloy.
fusible plugs or thermal plugs
Under these conditions, the alloy melts allowing the piston to escape this causes the tire to deflate in a controlled manner.
excessive heat conditions
aircraft wheels are fitted with ________ which may be tubeless or have an inner tube.
pneumatic tires
Tires fitted with inner tubes tend to be used on some _________ and on _________. Most _________ have tubeless tires fitted.
light aircraft; older aircraft; modern aircraft
Tires are usually inflated with _________ which absorb shocks and supports the weight of the aircraft while the _________ maintains the shape of the tire, transmits braking, and provides a wearing surface. If a tube is fitted, the _________ also restrains the tube and protects it from damage.
nitrogen; tire cover; tire
The tire is divided into regions or sections. The tread of the tire is situated in the ________ and _________ section.
crown; shoulder
The _________ allows the tire to be flexible and the _________ is seated inside the flange of the wheel.
sidewall; bead
There are two types of tires in common use. The names originating from the way the tires are constructed. These are known as:
- radial ply; and
- bias or cross ply tires
The _________ consists of a casing made of plies of cotton, rayon, or nylon cords. The cords are not woven but arranged parallel in _________ layers and held together by a thin film of _________ which prevents cords of adjacent plies from cutting one another as the tire flexes in use.
tire; single; rubber
During construction of the tire, the plies are fitted in _________ and set out so that the cords of adjacent plies are at _________ to one another in the case of bias or cross ply tires.
pairs; 90 degrees
The plies are fitted _________ at approximately __________ to the centerline of the tire in radial tires.
bead to bead; 90 degrees