Perf Feedback Flashcards

1
Q

Screen height Class B

A

50ft (Wet or dry)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Screen height Class A dry runway

A

35ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Screen height Class A wet runway

A

15ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

When carrying out inceased v2 what is effect on screen height

A

remains constant

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

v2 increased, what happens to CLTOm and climb angle

A

both increase

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

if mass increases what happens to ROD, Gradient of Des and desc angle

A

ROD increase
Gradient of Desc no affect
descent angle no affect

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Why would you decrease the flap settings? If you have a long runway + close obstacles

A

How do you calculate ASDR with OEI?

ASDR is the distance from break release point to V1 + the distance from (V1 +2sec) to a complete stop

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Is v2 affected by tyre speed

A

no

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Quick Turnaround affected by

A
Slope
Temp
Flaps
Wind
Pressure Alt
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

On Contaminated Runway, what happens to the CLTOM

FLTOM

A

CLTOM UNCHANGES

FLTOM decrease

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

If Dry V1 used on wet runway,

A

ASDR increases and becomes unbalanced confirmed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

What is SFC?

A

Fuel flow per unit of thrust

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

two aircraft with the same mass and different altitude

A

Higher Aircraft has a reduced ROC

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Factores affecting Driftdown flight path with OEI?

A

Mass Start of Drifdown
PA
Temperature

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Factors affecting level off altitude? Pick 2

A

OAT yes

Power (N1) yes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

How does an increase in mass affect Vy and Vx?

A

Increase VY

Increase VX

17
Q

What is the regulated TOM?

A

The lowest of PLTOM and maxiumum structural TOM

18
Q

If flaps setting is increased - what happens to glide angle, rod and speed for in glide angle.

A

Glide angle SLIGHTLY increase.

ROD increase

Speed for min angle and min ROD decrease

19
Q

Why do we have a crossover altitude?

A

not exceed MMO

20
Q

On Landing Graphs

A

If upslope given, do not apply any factor

21
Q

What is the procedure to follow after a quick turnaround?

A

Waiting a certain amount of time before T/O

22
Q

Wet paved runway (on take off) factorisation?

A

Do not factorise. (1.0x)

23
Q

What is the effect of decreasing density on flight path angle, rate of climb, and climb angle?

A

all decrease

24
Q

What is the effect of wind on ROC and Gradient of climb?

A

No effect on ROC

No effect on Air gradient

A headwind increase ground gradient

A tailwind decrease ground gradient

25
Q

On the speed versus Thrust required curve, what is the point of contact with the tangent of the curve?

A

1.32VMD because speed is proportional to power required?

26
Q

When TOM is limited by VMBE, an increase in the uphill slope will:

A

allow an increase in mass

27
Q

The use of reduced Thrust for T/O is permitted

A

If the TOM is less than the field length and climb limited take

28
Q

Maximum quick turnaround mass

A

decrease with increasing OAT and pressure

altitude .

29
Q

What is the climb requirement at the 3rd take off segment ?

A

there is no climb req

30
Q

When does the pilot take the first action to abort the take off?

A

At V1

31
Q

Take off with compacted snow on runway.

A

ASDR increases TODR stays the same.

32
Q

in the thrust vs speed, the speed at the minimum of the curve (reworded):

A

Vmd

33
Q

Specific Range

A

NM/KG

34
Q

On an uphill runway the ASDR

A

increases

35
Q

increased v2 procedure

A

to achieve optimum alt as soon as possible