Landing 323 Flashcards

1
Q

What are the two parts of landing?

A

Descending Approach

Ground Roll

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2
Q

Descending Approach:

A

• L/D is an angle attack remember

• Minimum Safe Approach Speed
o 1.3 X Vso
o Transition to Vso at touchdown (NOT BEFORE)

• Steepest approach angle for your approach as possible.
o Reduce flare distance, minimize horizontal component of inertia

  • Large increase in drag as aircraft pitches up
  • As wing tip stalls on a swept wing, burbling flow misses the tail surfaces. There is no buffet.
  • Airfoil center of lift moves inward and forward.
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3
Q

Newton’s Second Law:

A

• Newton’s Second Law : The direction of the force is the same as that of the acceleration.

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4
Q

After Touchdown:

Thrust

Drag

A

o Thrust = 0
♣ Throttle at idle after touchown
♣ Reverser makes thrust value = negative thrust

o Drag
♣ Induced and parasite at touchdown
♣ Parasite at end of roll

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5
Q

F =

A

F = MA

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6
Q

Aerodynamic drag decreases as _______ decreases.

Friction _______ as _____ decreases.

A

Aerodynamic drag decreases as velocity decreases.

Friction increases as velocity decreases.

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7
Q

• Acceleration and Deceleration

Proportional to

Inversely proportional to

A

o Proportional to the sum of all forces

o Inversely proportional to Mass of object

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8
Q

Friction

Depends on:

Characteristics of :

_________ ability
Product of _____ - _____

A
Friction:
•	Depends on forces acting normal to runway 
•	Characteristics of landing surface
•	Braking ability
•	Product of Weight - Lift
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9
Q

How can you minimize landing distance:

A

Minimize stall speed

Maximize deceleration

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10
Q

How can you minimize Vso (4)

A

Minimize Weight
Maximize Air Density
Maximize surface Area & Cl
Flaps

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11
Q

Minimizing Vso in depth.

A

• Minimize weight –
o gives you a slower landing speed
o shorter distance to decelerate

• Maximize air density (not very easy to control)
o Low altitude
o Low temperature
♣ Slower airspeed.

• Maximize surface area & CL
o Maximize surface area (really only way is fowler flaps)
o Maximize Clmax
♣ Flaps
♣ Maximize flaps regardless of wind conditions

• Flaps
o High Lift Device
o Same amount of lift at slower speed
o Reduces horizontal component of inertia
o Increases angle of descent without increasing airspeed

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12
Q

How can you Maximize Deceleration?

Negative THRUST: WHAT DOES IT DO

A

o Provides approx. 40% of forward thrust
o Thrust reversers
o Reversible pitch props

Increases drag
♣ Aerodynamic Drag

Increases friction
♣ Max Wheel Braking
♣ Decrease Lift – spoilers, flaps up, etc.
♣ Anti-skid brakes

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13
Q

Other factors with Maximum Deceleration?

Wind
Runway Slope
Pilot Technique

A

o Wind
♣ Headwind component reduces groundspeed

o Runway slope
♣ Weight component

o Pilot Technique
♣ Approach Speed
♣ Use of flaps
♣ Use of Brakes

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14
Q

Landing Errors (4)

What happens and whY?

A

• Wheel Barrowing

o Excessive speed, full flaps. Touchdown too fast hold the airplane down with forward pressure.

• Balloons

o Thinks ground coming up too fast, pulls back

• Bounces

o Too fast, or too great descent rate. Gains altitude as airspeed slows

• Porpoise

o Touch nose gear, then mains, then nose gear.

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15
Q

Wind Shear:

Define it

How can you tell on final if there’s a shear layer?

Describe Horizontal Gusts

Describe Vertical Gusts

Falling air ______ angle of attack

Decrease in lift causes _______ to increase

A
  • Any sudden change in the direction or speed of wind
  • Watch wind sock and winds aloft if it’s drastic there’ll be shear

o Horizontal gusts (side to side gusts not crosswinds)
♣ Change in airspeed
♣ Induces a pitching moment to return to the airplane to trimmed speed
♣ Induces new drag and lift values for new airspeed

o	Vertical Gusts
♣	Change Angle of attack
♣	May introduce damaging flight loads
♣	Rising gust increases angle of attack 
•	Too many G’s
•	Stall
♣	Falling air decreases angle of attack
•	Decrease in lift - recovery altitude increases.
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16
Q

Beware during thunderstorms of _________.

Preventative measure?

A

Updrafts

Heat things up in case your air gets cold soaked especially since there’s liquid.

17
Q

Problems with Ice

A

• Disturbs smooth airflow
• Adds weight
• Changes the shape of the airfoil
• Changes shape of control surfaces – flutter
• Increases stall speed
• Ice over air intake
o Both carbureted and fuel injected
• Any 90° bend in air intake plumbing
o Ice will form and build
• Windshield usually the first to notice ice
o Loss of visibility
o Probably indicates there’s developed ice elsewhere much greater
• Water seeps into wing or tail crevices and freezes at higher altitudes
o Loss of control

18
Q

Carb Icing

How does it happen
Reduces what?

How do you fix it? (hopefully)

A

Carburetor Icing
• Air expands cools temperature
• Evaporation occurs cools temperature
• Reduces amount of airflow into the engine

Full carb heat always
• Partial heat may thaw moisture crystals, but not warm carb walls above freezing
• Carb air temp gauge

19
Q

Snow

is it a problem? Why or why not?

What does it do to the aircraft?

What might you need to do while taxiing.

What does snow do?

A
SNOW
•	Generally not a problem
o	Already frozen moisture
•	Changes airfoil shape while sitting
•	May need to taxi with more power
•	Reduces visibility
20
Q

Rain

Explain it all.

A
RAIN
•	Impact force
o	Pressure (density of air) + Force
o	Water is 1,000 x more dense than air
o	Wet airplane adds weight
o	Water rippling on wing surface increases rag up to 30%
o	Water logged – saturated air filter
♣	Power loss
21
Q

Three types of hydroplaning.

A

Dynamic
Viscous
Reverted Rubber

22
Q

Dynamic Hydroplaning

A
  • (high speeds and a puddle of water)
  • (water molecules can’t get out of the way fast enough and they don’t due to surface tension)
  • high speeds +Standing water
23
Q

Viscous Hydroplaning

A

• wet, painted surface of runway

24
Q

Reverted Rubber Hydroplaning

A

Reverted Rubber
• locked brakes
• tire skidding generates enough heat to cause rubber in contact with runway to revert to it’s uncured state ( think of it as melting). Reverted rubber acts like a seal between tire and runway, delaying water exiting front eh tire footprint area. The water heats and is converted into steam which supports the tire off the runway.

25
Q

Average deceleration on a dry runway using brakes and reversers is _____ kts per second.

A

7 knots per second

26
Q

If you’re hydroplaning your deceleration is ______

With reversers it’s_____

A

1 knot per second or .05gs

3.8 knots per second

27
Q

How can you shorten your ground roll after landing?

A
Brakes
Aerodynamic Braking
Thrust reversers
Increase friction
Speed Brakes