ALL-FINAL-MODULES-ASLG

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62 Terms

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Landing gear

The system that supports the aircraft during landing and while it is on the ground.

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Fixed gear

Landing gear that is stationary and does not retract for flight.

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Retractable landing gear

Landing gear that can be retracted into the fuselage or wings after takeoff.

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Conventional gear

Also known as tailwheel gear, it is a landing gear configuration with two main wheels positioned under most of the weight of the aircraft and a smaller wheel located at the aft end of the fuselage.

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Tricycle gear

A landing gear configuration with a shock-absorbing nose wheel at the forward end of the fuselage and the main wheels positioned behind it.

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Center of gravity

The point at which the aircraft's weight is evenly distributed.

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Ground-looping

A phenomenon where the aircraft loops or spins on the ground during landing or maneuvering.

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NLG

Abbreviation for Nose Landing Gear.

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MGL

Abbreviation for Main Landing Gear.

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Downlock actuator

A mechanism that locks the landing gear in the down position.

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Retraction actuator

A mechanism that retracts the landing gear into the fuselage or wings.

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Shock absorber

A device that absorbs and dampens the impact forces during landing.

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Hydraulic power

The use of hydraulic fluid to operate and control the landing gear system.

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Differential braking

The use of brakes on one side of the aircraft to steer it during taxiing.

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Bogie beam assembly

A structure that supports and connects the main wheels of the landing gear.

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Pitch trimmer

A device used to adjust the aircraft's pitch attitude.

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Door actuator

A mechanism that operates the doors of the landing gear bays.

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Fairing

A streamlined covering or enclosure for the landing gear components.

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Lock collar

A device that prevents the closure of the landing gear doors when the aircraft is on the ground.

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Skid

A type of landing gear that helps slow the aircraft upon landing and provides directional stability.

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Margin

The number of extra tires an aircraft may have in case one fails.

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Bogie

The attaching mechanism that connects more than two wheels to a landing gear strut.

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Tricycle-type landing gear

A landing gear arrangement where the main gear is attached to the reinforced wing structure or fuselage structure.

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Fixed landing gear

Landing gear that remains exposed to the slipstream as the aircraft is flown and is not retractable.

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Retractable landing gear

Landing gear that stows in fuselage or wing compartments while in flight and does not cause parasite drag.

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Shock absorbing landing gear

Landing gear that alters and transfers shock energy throughout the airframe at a different rate and time than the single strong pulse of impact, and absorbs the shock by converting the energy into heat energy.

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Leaf-Type Spring Gear

Landing gear that utilizes flexible spring steel, aluminum, or composite struts to receive the impact of landing and return it to the airframe to dissipate at a rate that is not harmful.

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Rigid landing gear

Landing gear that directly transfers shock load to the airframe and uses pneumatic tires to soften the impact loads.

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Bungee Cord

Elastic cords positioned between the rigid airframe structure and the flexing gear assembly to take up loads and return them to the airframe at a non-damaging rate.

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Shock Struts

Self-contained hydraulic units that support an aircraft while on the ground and protect the structure during landing by absorbing and dissipating shock loads.

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Shock strut

A component of an aircraft landing gear system that absorbs and dampens the impact forces during landing and taxiing.

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Axle

A shaft on which the aircraft wheels are mounted.

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Upper cylinder

The top part of a shock strut that contains a valve fitting assembly and is used for filling the strut with hydraulic fluid and inflating it with air or nitrogen.

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Lower cylinder

The bottom part of a shock strut that is connected to the axle and provides support and stability to the landing gear.

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Packing gland

A device used to seal the sliding joint between the upper and lower telescoping cylinders of a shock strut.

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Wiper ring

A ring installed in a groove in the lower bearing or gland nut of a shock strut to prevent dirt, mud, ice, and snow from entering the packing gland and upper cylinder.

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Torque links

Components attached to the upper and lower cylinders of a shock strut to keep the piston and wheels aligned and prevent rotation.

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Locating cam assembly

A mechanism used in nose gear shock struts to align the wheel and axle assembly in the straight-ahead position when the strut is fully extended.

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Shimmy damper

An external device attached to a nose gear shock strut to reduce or eliminate shimmy, which is an undesirable side-to-side oscillation of the landing gear.

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Jacking points

Specific points on the shock struts where jacks should be placed for lifting the aircraft during maintenance.

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Towing lugs

Attachments on the shock struts used for towing or positioning the aircraft.

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Instruction plate

A plate attached near the filler inlet and air valve assembly of a shock strut that provides directions for filling the strut with fluid and inflating it.

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Landing gear maintenance

The process of inspecting and maintaining various components of the landing gear system, including wheels, tires, shock struts, and steering mechanisms.

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Wheel bearings

Bearings that support the weight of the aircraft wheels and allow them to rotate smoothly.

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Lubrication

The process of applying grease or oil to reduce friction and wear on moving parts of the landing gear system.

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Tapered roller bearing

A type of bearing commonly used in aircraft landing gear systems that consists of tapered rollers and a cone-shaped race.

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Overtravel

The movement of the landing gear beyond its normal operating range, which must be checked and adjusted when necessary.

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Landing gear latch

A mechanism used in landing gear systems to hold the gear up or down and/or to hold the gear doors open or closed.

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Rigging and adjustment

Procedures that vary from aircraft to aircraft for adjusting and aligning landing gear components.

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Uplock and downlock clearances

The specific distances or gaps required for the proper operation of the landing gear locking mechanisms.

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Linkage adjustments

Fine-tuning the connections and movements of various components in the landing gear system.

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Limit switch adjustments

Setting the limits or boundaries for the movement of certain parts in the landing gear system.

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Manufacturer's maintenance data

Technical information provided by the aircraft manufacturer that outlines the specific procedures and requirements for maintaining and servicing the landing gear system.

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Landing gear door latch

A specific type of latch used to secure the landing gear doors in the closed position.

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Landing gear retraction test

A procedure to check the proper functioning of the landing gear system by raising and lowering the gear while visually inspecting for any issues or abnormalities.

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Emergency back-up extension system

A secondary system that allows for manual extension of the landing gear in case of a failure in the primary system.

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Annual inspection

A routine maintenance check performed once a year to ensure the overall airworthiness of the aircraft, including the landing gear system.

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Landing gear linkages

The interconnected components that transmit motion and force between different parts of the landing gear system.

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Landing gear extension and retraction

The movement of the landing gear from the extended (down) position to the retracted (up) position and vice versa.

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Landing gear doors

Panels or covers that open and close to allow the extension and retraction of the landing gear.

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Alternate/emergency extension or retraction systems

Backup systems that can be used to manually extend or retract the landing gear in case of a failure in the primary system.

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Rubbing, binding, chafing, or vibration

Unusual sounds or sensations that may indicate a problem or malfunction in the landing gear system.