Section 7 - Airframe And Systems Description - 9 Landing Gear System Flashcards

1
Q

What is the landing gear type?

A

Electro-hydraulic type

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2
Q

How is it powered?

A

Powered by a reversible pump

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3
Q

How is the pump contorlled?

A

Electrically, by a the LG control knob located on the LH instrument panel and by the legs position micro switches

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4
Q

What do the leg position micro switches allow us to detect?

A

Landing gear down-locked and up positions and for alerting the pilot by aural needs should the approach and landing configuration be incorrect, in terms of flaps/throttle levers/landing gear positon, in order to aviod and unintentional gear-up landing

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5
Q

What modes of landing gear are there?

A

2: normal and emergency

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6
Q

What does the normal operation provide?

A

Gear extension and retraction by means of hydraulic jacks

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7
Q

How is gear extension also helped?

A

By gravity

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8
Q

What does emergency operation provide?

A

Landing gear extension by means of a hydraulic accumulator which discharges oil in the above mentioned jacks

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9
Q

Where is the hydraulic oil contained?

How is it pressurized?

How does the electric pump work?

A

In an integrated reservoir located inside the Hydraulic Power Pack

By a reversible electric pump:

As the LG control knob is placed in either the UP or DOWN position, the pump directs the fluid through the related pressure line toward each hydraulic jack

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10
Q

What do we do in order to prevent inadvertent LG retraction?

A

The control knob must be pulled before being pushed upward for UP command

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11
Q

For what is the emergency hydraulic accumulator used?

A

Used for the landing gear extension:

normal extension line and emergency extension line converge in correspondence of the shuttle valves

Two valves:
- The first one for NLG and
- Second one for MLG emergency operation

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12
Q

Where is the emergency accumulator pressure indicator located?

A

On the tail cone, left side

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13
Q

How is the nitrogen pressure recharged?

A

On ground, a red push-button located beneath the pressure indicator allows the electrical pump for charging the accumulator should the nitrogen pressure be below the lower limit indicated on the placard

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14
Q

How is emergency extension controlled?

A

By two distributors located on the cabin floor, under a removable cover in correspondance of the pilot seat

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15
Q

How is the LG indication system?

A

Electrical

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16
Q

What are the main components of which the LG indication system is composed?

A

UP/DN limit micro-switches (6 couples, for each leg)
Leg position, 3 lights (turned ON when the pertinent leg is extended and locked and located on the LH instrument panel)
Transmition light, 1 red (turned ON during transition phases)
Pump light, 1 amber (GEAR PUMP ON caution amber light turned ON when the pump is electrically supplied )
Push to test (if installed) (for landing gear and green lights operational check)

17
Q

What does each light indicate?

A

Three greens: illuminate only when the respective gear is down-locked

Red light: extinguishes only when all three gear legs are down-locked or they are up

Amber light: extinguishes only when the electrical pump is off

18
Q

What do the Up/Down limit switches control?

A

LG lights lighting and pump operation on the basis of LG configuration set by the pilot through the LG control knob

19
Q

What’s the push to test button?

A

Used to check that the landing gear position lights are operating

20
Q

What is the warning horn for?

A

Alerts the pilot when the LG contorl knob is in UP position and at least one of the two throttle levers and/or flaps are respectively set to idle and to LAND position

21
Q

What happens to LG lights during emergency extension?

A

LG position lights work as per normal extension mode. For this reason LG control knob must be set on DOWN position before starting the emergency procedure

22
Q

IMPORTANT

What must you do after each emergency landing gear extension?

A

Apply the restoration procedure described in the AMM