11.13 Landing Gear Flashcards

1
Q

WHICH COMPONENT OF THE LANDING GEAR SUPPORTS MOST OF THE WEIGHT OF THE AIRCRAFT WHEN IT IS ON THE GOUND?

A

THE SHOCK STRUT

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2
Q

HOW IS THE ACTION OF THE SHOCK STRUT CONTROLLED?

A

GAS IN THE STRUT PROVIDES THE SHOCK ABSORBING FUNCTION AND THE OIL PASSING THROUGH VARIOUS PASSAGEWAYS PRODIVES DAMPING

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3
Q

WHAT IS THE PURPOSE OF THE THE LANDING GEAR SHORTENING MECHANISM?

A

TO SHORTEN THE GEAR DURING RETRACTION, TO FIT IN THE WHEEL WELL AND TO INCREASE ENGINE GROUND CLEARANCE.

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4
Q

WHICH SAFETY DEVICE ARE IN PLACE TO PREVENT THE LANDING GEAR FROM BEING MOVED TO THE UP POSITION WHEN ON THE GROUND?

A

THE LANDING GEAR SELECTOR IS PHYSICALLY PREVENTED FROM BEING MOVED TO THE UP POSITION ON THE GROUND,

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5
Q

WHAT IS THE FUNCTION OF THE LANDING GEAR SOLENIOD CONTROL SAFETY VALVE?

A

TO BLOCK THE HUDRAULIC SUPPLY TO THE LANDING GEAR SYSTEM AT HIGH SPEEDS

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6
Q

WHICH COMONENT TRANSFERS THE TYRE PRESSURE INFORMATION FROM THE ROTATING POINT OF THE WHEEL TO THE FIXED PART?

A

TYRE PRESSURE TRANSDUCER.

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7
Q

IF THE AUTO BRAKE SYSTEM IS SET TO AUTO, WHEN DOES IT START TO OPERATE?

A

AS SOON AS THE AUTO SPEEDBRAKE SYSTEM EXTENDS THE SPOILERS

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8
Q

WHAT IS THE PURPOSE OF THE BODY GEAR OR CENTRELINE GEAR?

A

TO SPREAD THE AIRCRAFT WEIGHT OVER A GREATER AREA,

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9
Q

HOW IS THE ACTION OF THE SHOCK STRUT CONTROLLED

A

THE GAS IN THE SHOCK PROVIDES THE SHOCK ABSORBING FUNCTION AND THE OIL PASSING THROUGH THE VAROUS PASSEGEWAYS PROVIDE DAMPENING.

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10
Q

HOW IS ENSURED THAT THE NOSELEG IS CORECTLY POSITIONED BEOFRE RETRACTION?

A

A SET OF CAMS CENTRE THE NOSE WHEELS AS THE LEG EXTENDS,

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11
Q

WHICH COCKPIT INDICATOR IS GIVEN WHEN THE LANDING GEAR IS ALL EXTENDED AND LOCKED?

A

A GREEN LIGHT FOR EACH LEG.

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12
Q

WHICH STATEMENT IS CORRECT REGUARDING THE ONTROL OF THE NOSE WHEEL STEERING

A

THE RUDDER PEDALS GIVE LESS DEFLECTION THAN THE TILLER.

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13
Q

WHAT HAPPENS IF THE BREAK PEDALS ARE MANUALLY DEPRESSED DURING AUTO BREAKING?

A

THE AUTOBRAKE FUNCTION DISENGUAGES AND THE BRAKES ARE CONTROLLED AS NORMAL BY THE CREW.

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14
Q

IF ACCESS TO THE UNDERCARRIGE BAYS OF AN AIRCRAFT IS REQUIRED ON THE GROUND, HOW CAN THE DOORS BE OPENED?

A

THE DOORS CAN BE UNLOCKED MANUALLY BY RELEASING THE UPLOCK SO THEY FALL UNDER GRAVITY

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