Appendix Flashcards

1
Q

how are altimeter errors corrected? when do they apply and when do they not apply?

A
  • errors are corrected for due to temperature using an altitude correction table. the correction factor is added to the reference altitude eg. DA, MDA etc.
  • applies to any altitude on procedural inst. approach except VNAV approaches
  • does not apply for assigned altitudes given by ATC
  • ATC must be made aware of corrections
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2
Q

what happens to ASDn and ASDn-1 as V1 increases?

A

they both increase

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3
Q

What is ACN

A
  • aircraft classification number

- it’s a measure of stress the aircraft wheels put on the tarmac. more wheels = more stress

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4
Q

What is PCN

A
  • pavement classification number

- a value defining the strength of runways and taxiways

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5
Q

a PCN will have a number followed by 4 letters, what are the different combos of them

A

first letter: (F) flexible (R) rigid

second letter: (A) high (B) medium (C) low (D) ultra low

third letter: (X) pressure limit

fourth letter: (T) measured by technical evaluation (U) measured by usage

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6
Q

how do you know if your aircraft can land or use certain runways and taxiways using ACN and PCN

A

if ACN < PCN, its okay
if PCN < ACN, it’s not okay

found using the table (follow it down)

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7
Q

what is MAC

A
  • mean aerodynamic chord

- the average chord length over the whole wingspan

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8
Q

how to convert CoG location as a % of MAC

A

CoG - (LE)MAC / MAC x 100 = % MAC

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9
Q

when should the decision to reject V1 be made

A

should be made by the captain before V1 so action can be taken AT V1.

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10
Q

What are the memory items for a high and low speed RTO

A
  • close thrust levers
  • speed brake
  • brakes
  • reverse thrust
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11
Q

What should be done for a low speed RTO

A
  • below 80 knots
  • memory items
  • address failures
  • communicate
  • decision to taxi or go back
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12
Q

what should be done for a high speed RTO

A
  • above 80 knots
  • memory items
  • address failures
  • communicate w. fire service and ATC/cabin crew for evacuation
  • stop on runway
  • brake energy calcs if time permits
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13
Q

what are the effects of a continued takeoff 2 seconds before Vef w. engine failure

A
  • reduced safety margins
  • reduced climb gradients
  • increased TOD, TODn-1
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14
Q

what happens following an engine fire

A
  • Vef “fire bell”
  • 400 feet, communicating and confirming failure
  • memory actions
  • shut down engine
  • performance loss after 400 feet.
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15
Q

What happens following en engine failure

A
  • Vef “bang” immediate loss of power

- 50% thrust

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16
Q

how is minimum turnaround time calculated

A
  • add energy from last landing
  • add energy for taxi
  • add energy for RTO
  • subtract energy dissipation during turnaround
17
Q

what happens to efficiency as more fuel is burned

A
  • CoG moves forward as more fuel is burned from wing tanks and main tank which causes less efficiency
18
Q

what is committal height:

A
  • once below a certain height, the aircraft must land
19
Q

What are the implications of a fuel leak

A
  • will a fuel leak cause damage?
  • have enough fuel to divert?
  • some checklists require engine shutdown to find fuel leak.