Landing Flashcards

1
Q

Performance values take into account the threshold is crossed at ______ft at VREF.

A

50

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2
Q

At 90 kt, the PM calls “90 KNOTS.” The PF smoothly reduces thrust reversers to idle by ______ kt (not above 30% N1).

A

60

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3
Q

How to use reverse thrust should be used when landing on wet, slippery, and contaminated runways.

A

Maximum

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4
Q

Rudder control is effective to approximately______ kt. Nose wheel steering is sufficient for maintaining directional control during the rollout.

A

60

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5
Q
A
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6
Q

Idle reverse thrust will be used for landing on runways with ______ ft or more of actual landing distance available, as runway

A

7,500

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7
Q

IRTL must not be used when any of the following conditions apply:

A

1) Wet or contaminated runways

2) condition code (RCC) of 5 or less

3) Overweight landings

4) Any tailwind component exists

5) Braking action less than GOOD

6) Aborted/rejected takeoff

7) With a deferral or abnormality that may affect landing distances. (Anti-skid, spoiler caution message, etc.)

8) less than 7,500 ft of runway is available

9) ACARS or dispatch release landing distance data exceeds 7,500 ft without reverser credit

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8
Q

LANDING ON WET OR CONTAMINATED RUNWAYS

A
  • Use Maximum Performance Landing techniques
  • Make a firm touchdown
  • Apply maximum reverse thrust.
  • Apply firm and symmetrical brake pedal pressure; do not pump the brakes
  • Maintain runway centerline with rudder
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9
Q

(LAHSO) PILOT AUTHORITY

A

The PIC has the final authority

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10
Q

(LAHSO) WEATHER

A

1,000 ft and 3 miles (PAPI or VASI available and working),

otherwise 1,500 ft and 5 miles are required.

No windshear reported in the last 20 minutes

The tail wind must be less than 3 kt.

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11
Q

(LAHSO) APPROACH

A

Approach must be stabilized by:
* 1,000 ft HAT for straight-in visual approaches
* MDA or 500 ft HAT, whichever is lower, when a circling maneuver is to be accomplished after completing an instrument approach

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12
Q

(LAHSO) RUNWAY

A

Dry runway is required

landing distance must be at least the distance shown on the TLR.

Touchdown must be in the first one-third of the available landing distance or in the first 3,000 ft, whichever is less.

Night an FAA-approved LAHSO night lighting system is installed and operating.

No MEL item may exist that affects the stopping capability of the aircraft.

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13
Q

(LAHSO) CLEARANCE

A

A LAHSO clearance shall not be accepted below 1,000 ft AGL on final approach.

A LAHSO clearance, once accepted, must be adhered to just as any other ATC clearance, unless an amended clearance is obtained or an emergency occurs. A LAHSO clearance does not preclude a rejected landing (go-around).

When the computation of LAHSO data interferes with other flight deck safety of flight duties, do not accept a LAHSO.

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14
Q

REJECTED LANDING

A

A rejected landing (go-around) is performed when:
* Unable to land in the first one-third of the available landing distance or first 3,000 ft, whichever is less
* Any condition exists in which the PIC determines a safe LAHSO cannot be completed within the confines of the hold short point (e.g., emergency situation, unsafe condition on the runway, not properly configured)

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15
Q

MAXIMUM PERFORMANCE LANDING

A
  • Use full flaps
  • Cross the threshold at 50 ft and VREF
  • Avoid extended flare
  • Apply maximum reverse thrust
  • After the main landing gear wheels have touched down, lower nosewheel immediately
  • Apply firm and steady maximum brakes, and hold pedal pressure until the airplane decelerates to a safe taxi speed
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16
Q

Required landing distance is calculated for what value

A

airplane crossing the runway threshold at 50 ft and at VREF using maximum manual braking.

17
Q

When the airplane crosses the threshold at 10 kt above VREF, the landing distance increases by approximately ________

A

20%.

18
Q

What are the reasons for bounce landing?

A
  • Windshear
  • Low-level turbulence
  • Excessive airspeed
  • Thrust not at idle on touchdown
  • Incorrect flare technique
19
Q

LANDING FLAPS OTHER THAN 45°

A

QRH procedure and compute the required runway length before landing. A straight-in coupled approach recommend

20
Q

The decision to land overweight is a function of several factors:

A
  • Runway and performance landing weight limits
  • Approach weather and runway conditions
  • Tire speed limit
  • Status of aircraft (e.g., anti-skid, brakes, spoilers)
  • Time and altitude needed to burn off fuel versus weather, traffic, and/or need to land
21
Q

Who does the landing during overweight landing

A

Captain

22
Q

Do you need to declare emergency doing overweight landing

A

no

23
Q

REJECTED / BOUNCED LANDING
When the airspeed has dropped below VREF, how to initiate the miss approach

A

retract flaps only when the airspeed becomes greater than VREF.

24
Q

REJECTED / BOUNCED LANDING

ACTIONS AND CALLOUTS

A
25
Q

Do not use asymmetric reverse thrust on slippery or icy runways.

A