Landing Flashcards

1
Q

What is LDA, what are the LDA parameters

A
  • landing distance available

- is the runway length (TORA) with no obstacle in path

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2
Q

what are the LDA parameters with obstacles

A

at a distance 60m back from threshold, a minimum 300m width extending outwards by 15%

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3
Q

what is Vls

A
  • lowest selectable speed
  • Vls = 1.23Vs1g
  • speed no less than Vls to 50ft above rwy.
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4
Q

what is Vapp

A
  • Final approach speed
  • speed during landing at 50ft above runway
  • Vapp must be greater than/equal to Vls
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5
Q

how is Vapp determined

A

= Vls + wind correction (minimum 5kts, max 15kts)

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6
Q

what is Vref

A
  • reference speed (incase of emergency/abnormal config)
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7
Q

what is Vref

A
  • reference speed (incase of emergency/abnormal config)
  • Vref = Vls in CONF FULL
  • for non-normal, Vapp = Vref + delta Vinop
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8
Q

What is ALD

A
  • Accelerate landing distance
  • the distance from 50ft above runway to where the aircraft comes to a complete stop.
  • correction of no more than 50% HW and 150% TW
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9
Q

what effect does an automatic landing have on ALD

A
  • it increases ALD on the ground and in air phase compared to a manual landing
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10
Q

What is an approach climb? what are the speeds for each config and climb gradients

A
  • it is the aircraft’s ability to climb with 1 engine inoperative

CONFIGS:

  • 1 engine inop, slats and flaps in apprch
  • TOGA thrust, 1.23 vs1g less than v less than 1.41 vs1g.
  • Gear up, V greater than/equal to Vmcl.
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11
Q

what are the minimum gradients for a landing climb

A

twin - 2.1%

Quad - 2.7%

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12
Q

What is a landing climb? what are the configs for a landing climb

A
  • a landing climb is a constraint to ensure climb capability for te MAP with all engines running

(configs)

  • N engines
  • from idle to TOGA, thrust avbl 8 seconds later
  • gear down
  • flaps and slats in LDG config
  • 1.13Vs1g < V < 1.23Vs1g
  • V > Vmcl
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13
Q

what is the min gradient for a landing climb?

A

3.2% for all aircraft types

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14
Q

What is RLD

A
  • Required landing distance

- used to assist operations in defining minimum distance required at destination

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15
Q

what are the RLD considerations

A
  • slope must be considered if greater than +/- 2%
  • available runway length must be at least equal to RLD with failure
  • LDA must be greater than or equal to LDA
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16
Q

what are the RLD considerations on a dry runway

A
  • aircraft landing weight must permit landing within 60% of LDA at destination and any alternate
  • RLD = 1.667 x ALD
17
Q

what are the RLD considerations on a wet runway

A
  • LDA must be greater than or equal to 1.15RLDdry

- required landing distance must be 115% of dry surface

18
Q

what are the RLD considerations on a contaminated runway

A
  • RLDcontaminated is the greatest of:
  • ALDcontaminated x 1.15 OR
  • RLDwet
19
Q

what are the RLD considerations with auto landing

A
  • RLDauto is the greatest of:
  • ALDauto x 1.15 OR
  • RLDmanual
20
Q

What are the go-around requirements for normal approach

A
  1. 1% for twin

2. 7% for quad

21
Q

What are the go-around requirements for CAT II and III approach

A
  1. 5% for all aircraft types OR

- the published gradient (whichever’s higher)

22
Q

what is max regulatory landing weight (MLW) the sum of

A
  • max structural weight

- ma performance weight

23
Q

what are the fuel jettisoning conditions

A
  • after flying for 15mins at MTOW, if the aircraft can’t maintain a 2.1, 2.7% (most restrictive) climb gradient on the go-around then a fuel jettison system is required