Perf Flashcards

1
Q

Class B AEO Gross to Net Obstacle Clearance distance

A

x 1.3

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2
Q

Jet Max Range (VMR) =

A

VMR = 1.32 x VMD

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3
Q

Class B Take-off FLL Regulatory Factors - TORA/ASDA/TODA

A

TORA 1.0 ASDA 1.3 TODA 1.15

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4
Q

Gradient of climb knowing Rate of Climb and TAS

A

Gradient (%) = ROC x 6000
TAS x 6080

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5
Q

What needs to be checked for Quick Turnaround Limits?

A

OAT
Flaps
Runway Slope
Wind component
Pressure Altitude

See 4.30 in CAP

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6
Q

Specific (Air) Range?

A

Specific Air Range = TAS / Fuel Flow

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7
Q

Class B / Turbo-Prop Landing Distance Safety Factor

A

Most stop in 70% of LDA

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8
Q

Class A Jet Aircraft Landing Distance Safety Factor

A

Most stop in 60% of LDA

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9
Q

Safety factor landing on wet or contaminated runway

A

15% (x1.15)

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10
Q

VREF Class A and Class B

A

Class A
VREF = 1.23 VSR0

Class B
VREF = 1.30 VS0

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11
Q

Long-Range Cruise LRC Speed is selected because…

A

It achieves 99% of maximum still-air range with 4% higher speed

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12
Q

Aerodynamic Ceiling is _______

A

VY = VMD = VX

ROC = 0

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13
Q

Service ceiling is ______

A

Rate of climb falls to determined level - 100ft/min PROP - Jet - Specific ROC achieved?!

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14
Q

Typical Clean VMD value vs. Vs

A

Jet = 1.6VS

Prop = 1.3VS

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15
Q

Jet and Prop Maximum Range Speed is

A

Jet Max Range Speed = 1.32 VMD

Prop Max Range Speed = VMD

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16
Q

Clearway min width and max slope, controlled by

A

Max semi-width 75m
Max upward slope 1.25%
Controlled by airport authority

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17
Q

Balanced Field is when…

A

Balanced Field
TODA = ASDA

However, Balanced Field Takeoff
OEI TODR = OEI ASDR

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18
Q

Screen Height (Class A and B) Wet Runway

A

Class A - 15ft
Class B - 50ft

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19
Q

Runway Upslope effect on ASDR

A

Increases

(Gradient much greater effect on acceleration than braking)

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20
Q

Class B - No stopway/clearway - TODR safety factor relating to TORA

A

TODR x1.25 must not exceed TORA

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21
Q

Take-off Class B - Factor for Paved Wet

A

x1.0

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22
Q

Take-off Class B - Factor for Grass Wet

A

x1.3

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23
Q

Take-off Class B - Factor for Grass Dry

A

x1.2

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24
Q

Max TODA compared to TORA

A

Max TODA is 1.5x TORA

(EU OPS Limit)

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25
Q

VX for Prop

A

1.1VS

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26
Q

VX for Jet

A

VMD

27
Q

VY for Prop

A

Between VMP and VMD

28
Q

VY for Jet

A

1.32 VMD

29
Q

Power available line for Jet on Power Curves Graph

A

Straight-line - diagonal starting at origin

30
Q

Power available line for Prop on Power Curves Graph

A

Inverted Curve - Due to reducing thurst available at higher TAS

31
Q

Speed at Screen Height - Class B (V2)

A
  1. 2VS1 / “Safe Speed” - Single Engine
  2. 1VMCA / 1.2VS1 - Two Engine

50ft Screen Height

32
Q

Landing Factor for Wet

A

x1.15

33
Q

Landing Factor for Grass

A

x1.15

34
Q

Take-Off Flight Min Climb Gradient - Segment 2

A
  1. 4% - 2 Engines
  2. 7% - 3 Engines
  3. 0% - 4 Engines
35
Q

Above 400ft - Gradient of Climb

A

1.2% Two Enngines

36
Q

Max Bank Angle Segment 1 and 2 NTOFP

A

15º

37
Q

Max Bank Angle Segment 3

A

25º

38
Q

All Engines Operating FLL Factor

A

x1.15

39
Q

Balanced V1 on Graph

A

ASD - TOD(n-1)

40
Q

V2 Speed - Class A - Must be

A

1.13V<span>SR (2/3 engine turboprop and jet)</span>

1.1 VMCA

41
Q

LRC is

A

1.37VMD

42
Q

Maximum Obstacle Domain Semi-Width - 0-15º change of track

A

Able to maintain visual guidance or same accuracy
300m

All other conditions
600m

43
Q

Maximum Obstacle Domain Semi-Width - Over 15º change of track

A

Able to maintain visual guidance or same accuracy
600m

All other conditions
​900m

44
Q

VR Speed limitations

A

Above VS1 (single) or

  • *1.1VS1 (Multi)**
  • *1.05 VMCA**

Class A above speeds + above VMU (tailstrike prevention)

45
Q

Exceed Quick Turnaround Limit… How long to wait for reinspection of wheels?

A

53 minutes

46
Q

Best Range Speed with Tailwind

A

Lower than normal 1.32VMD

47
Q

Best Range Speed with Headwind

A

Faster than normal 1.32VMD

48
Q

Performance Ceiling is when ROC is reduced to ____

A

Performance Ceiling: 300ft/min

49
Q

Short Landing Ops - Maximum Declared Safe Area length

A

90m

50
Q

Missed Approach Min Climb Gradient and Config - Class A and B

A

OEI at or above DH
Gear Retracted
Approach Flaps

Class A

Twin - 2.1%
Three Engine - 2.4%
Four or More - 2.7%

  • *Class B**
    0. 75%
51
Q

Baulked Landing Min Climb Gradient and Config - Class A and Class B

A

Gear Down
Landing Flap

3.2% Class A - 2.5% Class B

52
Q

VSR0 =

A

1.06 VS0

53
Q

VMCA - Maintain course of ___ degrees of track, with a maximum bank angle of ___ degrees

A

VMCA - Maintain course of 20 degrees of track, with a maximum bank angle of 5 degrees

54
Q

Minimum Clearway width

A

500ft

55
Q

When is VMCA usually a limiting factor?

A

Low weight
Low PA
High Density
Large Flap Setting

56
Q

Clearway Reduces - What happens to V1

A

V1 Increases with reduced clearway

57
Q

Stopway Reduces - What happens to V1?

A

V1 Decreases with reduced stopway

58
Q

How many foot pounds to add per taxi mile on Brake Cooling Schedule?

A

1 million per taxi mile

59
Q

Runway Gradient to be ignored (%) on Landing

A

+/- 2%

60
Q

Missed Approach vs. Baulked Landing Config Name

A

Missed Approach: Approach Climb

Baulked Landing: Landing Climb

61
Q

Upslope effect on ASD and V1

A

ASD Increased
V1 Increased

(Longer to accelerate to V1)

62
Q

Downslope effect on ASD and V1

A

ASD Decreased
V1 Decreased

Lower V1 due to reduced braking effectiveness downslope

63
Q

Aerodynamic Ceiling =

A

Coffin Corner

64
Q

Class B Slope Factor on Landing and Takeoff

A

Landing - x1.05 on downslope only

Take-off - x1.05 on upslope only