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LANDING GEAR

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COMPLETE THE FOLLOWING DESCRIPTION WITH THE SUGESTED WORDS. USE THE INFORMATION SHOWN IN THE FILES.

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a320 family
landing gear
complete system
3 veces realizada

Creada por

Chucho Hernandez
Chucho Hernandez
México

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LANDING GEAR

COMPLETE THE FOLLOWING DESCRIPTION WITH THE SUGESTED WORDS. USE THE INFORMATION SHOWN IN THE FILES.

Chucho Hernandez
1

centered leak overrides automatic DOWN UP steering retraction steering electrically explosion hydraulically isolating decrease

The main operations of the Landing Gear are extension & ? , control and ? braking system . ? The Landing Gears ( L / Gs ) are operated and controlled .
Each L / G main fitting has a spare - seal activating valve for the bottom gland seals if a occurs .
The active LGCIU changes after each retract / extend cycle ( when the L / G control lever is moved away from the position ) .
The LGCIU ( in control ) sends a signal to release the baulk device , to let the L / G control lever move to the position .
The normal braking system has two modes of operation , manual and , and gives anti - skid protection in each mode .
Use of the parking brake all other braking systems when the parking brake pressure is available . ?
When the aircraft speed is above 130 knots , the is not available , and the NLG Wheels are by hydraulic action .
Do not apply a liquid or gas fire extinguisher directly on a hot wheel or brake unit . This could cause an .
The torque link damper is a spring - centered , two - way hydraulic unit which function is to the landing vibrations through the torque links . ?

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