Perf Flashcards

(42 cards)

1
Q

The EOL is derived from what three distances subtracting 45m

A

ASDA
TODA
STODA 1.9

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2
Q

V2 mustn’t be less than

A

1.1 VmCa or 1.2 vs

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3
Q

What does v2 overspeed achieve

A

On climb weight limited take offs you can use the extra remaining runway to get more speed resulting in increasing Vr and improving climb performance. The cost of this is increased torr and todr

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4
Q

What correction to add for slope on landing distance available

A

Specified in 4-2 if the runway slope exceeds 1% down, reduce LDA by 10% for each 0.5% in excess of 1%

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5
Q

What happens to asda and todr with a higher v1

A

ASDA increas
Todr decrease

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6
Q

What happens to asda and todr with a higher v1

A

ASDA increase
Todr decrease

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7
Q

Why is it good to use a balanced field length where possible

A

Maximise brw on a runway that has no stopway or clear way beyond the TORA. It is when ASDA =toda

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8
Q

What does a low v1 do

A

Results in short accelerate stop distance but a long 1 inop takeoff distance, useful when there is a clear way

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9
Q

What does having a high v1 (close to Vr) do

A

Results in long ASDA but short 1 inop take off distance. Useful when there’s a stopway

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10
Q

What do you interpolate to on average eprs for take off graph limitations

A

Nearest 1000ft PA and 5C

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11
Q

40 flap max structural landing weight is

A

64650kg

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12
Q

How long must you wait if quick turn around is not permitted

A

44mins

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13
Q

What are the considerations for reference field length

A

Casr 121 6.02 abc
Level, dry, still air, isa at sea level, mtow

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14
Q

Mzfw is related to what ,limitation

A

Wing structure

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15
Q

Minimum v1 speed is

A

Vmcg

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16
Q

You have an ldr of 1000m but the runway is wet.what is your new LDr

A

1150m
1000+15%

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17
Q

What wind components corrections are made to normal p charts

A

Not greater than 50% hwc and no less than 150% twc

18
Q

On a 3 degree profile and you cross the threshold at 100ft.
How much longer will your ldr be

19
Q

ATC requires you to maintain a particular altitude so how would you preserve maximum range

A

Fly aT optimum design speed and that speed will reduces as weight decreases

20
Q

Which is higher mrc or mlrc

21
Q

Max range speed is

A

Vimd 1.32 best tas/drag

22
Q

Correct rotation at the right Vr will ensure proper acceleration to

23
Q

What happens to stall speed in forward c of g

24
Q

Clear way is 400m and stopway 100m
If the stopway became 400mt what happens to v1 and mbrw

A

They both increase

25
Changes in oat effect sfc at a particular weight speed and altitude is
Increase in oat results in increased sfc
26
Do changes in oat have significant effect on sgr
No
27
Max range tas for a turbojet aircraft is
Determined by angle of attack for best gs/drag
28
Max range tas for a turbojet aircraft is
Determined by angle of attack for best gs/drag
29
The angle of attack for max endurance in a turbojet is
Independent of wind and weight
30
In order to maintain profile for a given ias
You need more power in hedwind than nil or tail
31
The angle of attack required for minimum thrust in level flight
Doesn’t vary with changes in weight
32
Vr mustn’t be less than
V1 or 1.05 vmca
33
Average tas in a climb formula
Anm/eti x 60
34
What cg position results in lower vmca
Forward
35
727 cg datum is located
Just in front of main landing gear
36
What happens to tas with oat increase
TAS increases
37
If asked best sgr without given a cruise schedule
Use lrc first then check faster speeds to see if there’s a faster one if headwind is strong
38
Balanced field length occurs
When distance require Oei to 35ft is equal to asda
39
Minim v1 is
Vmcg plus recognition time
40
MLRC differs from MRC
MLRC is faster than MRC and involves a reduction in thrust as fuel is burnt and weight reduces
41
Characteristics of fwd cg
Bad Increase stall speed due tail down force Increased drag Thrust required increase Range reduced Good Reduced vmca due longer arm to rudder Increased longitudinal stability
42
Approach attitudes with flaps Leading Trailing
Leading edge flaps are high attitude Trailing flaps are low attitude