3 DL QUIZLET CARDS Flashcards

1
Q

Which runway should you use if your right engine where to fail given winds are 360 at 15kts and the runway choices are 27/090?

A

090, good engine into the wind to counteract weather vane tendency

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2
Q

Safety

A
  • always paramount to operational priorities

- operation must be stopped if safety is in question of: passengers, crew, or assets

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3
Q

5 Operational Priorities (so all passengers see exit):

A
1-safety*
2-CFR/ATC/company policy compliance (CAP)
3-passenger comfort
4-schedule
5-economy
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4
Q

Flight Operations

A

1-promotes corporate goal by providing qualified pilots in support of global operation
2-function: support pilots through standardized programs, procedures, and manuals which meet or exceed all regulatory requirements
3-efforts:
a-safety policy) discourage unsafe practices, carelessness, complacency and development of individual procedures
b-safety promotion) promote operational flexibility, good judgment, and professionalism

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5
Q

5 Delta’s Core Values (HIRPS)

A

1-Honesty - Always tell the truth
2-Integrity - Always keep your deals
3-Respect - Don’t hurt anyone
4-Perseverance - Try harder than all our competitors—never give up
5-Servant leadership - Care for our customers, our community and each other

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6
Q

What are Delta’s priorities?

A

1-provide safe transportation,

2-exceed customer expectations, 3-make Delta the worldwide airline of choice

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7
Q

What are the main elements of a turbine engine?

A

Air inlet, Compressor, diffuser, combustion chamber, turbines, exhaust

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8
Q

You takeoff out of Atlanta and set 29.92 and land in Bogota Colombia which has a field elevation of 8300 ft and the current altimeter in bogota is 30.02. You noticed you forgot to reset your altimeter setting. What is your current altitude state? Higher/lower?

A

8200 ft., if you change from 29.92 to 30.02, your indicated alitiude would go up 100ft to 8300ft. if you leave the altimeter at 29.92 when you land in bogota, if would read 8200 ft. 0.1 inches per 10 feet. Thus, 0.1 times 10 per 0.1 equals 100 feet.

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9
Q

Where can you find VY and VX on a lift to drag chart compared to LD Max.

A

Vx is at L/D Max or slightly higher than L/D for turbine aircraft. VY is then at a higher speed than Vx

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10
Q

What type of wing design produces a higher critical mach number? More chambered or less chambered wing?

A

Swept, less camber

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11
Q

Why must GS increase in order to maintain a constant IAS in a climb?

A

TAS must increase so GS must also increase

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12
Q

Why does TAS increase at a constant IAS while in a climb?

A

Air is becoming less dense therefore more TAS required to maintain IAS

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13
Q

What are the service limits for a VASI?

A

3-5 miles day, 20 miles night. +/-10° centerline

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14
Q

If ATC clears your to descend to a specific altitude what is the minimum descent rate you must obtain or ATC expecting?

A

500 fpm

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15
Q

What happens to drag while in drag affect? What happens to as you leave ground affect and why?

A

Induced drag Increases as you leave ground affect. Not familiar with the term drag effect. AOA must increase as you leave ground effect to create the same lift that was being created with the assistance of ground effect.drag effect
drag effect The resistance to a projectile’s (i.e., a bullet’s) forward motion imparted by a tissue, which results in a loss of kinetic energy.

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16
Q

Define True Airspeed.

A

Calibrated A/S corrected for non-standard temp and pressure. I always used ICE T was a G. Indicated, Calibrated, Equivalent, True, and Ground

17
Q

What are the service limits of a papi? They are accurate from how many miles out? How many degrees side to side?

A

5 miles day, 20 night, +/-10°. 4 NM fro runway threshold. 4/10 degrees on test.

18
Q

What is the purpose of a hydraulic accumulator?

A

To store hydraulic pressure and to prevent system pressure surges

19
Q

Can you start the takeoff roll before a displaced threshold?

A

Yes, you cannot land before displaced threshold

20
Q

What happens to forces of an aircraft when established in a constant climb?

A

Lift must exceed weight for an aircraft to climb, so in a constant climb, lift exceeds weight and thrust equals drag, otherwise the aircraft would accelerate or decelerate. all opposing forces are in equilibrium in a steady state climb

21
Q

Which type of runway lights turn yellow on the last 2,000 feet?

A

Runway edge lights

22
Q

After you engage the starter you notice there is no N2 indication. What is most likely the issue?

A

The air turbine started does not supply any air for N2 rotation

23
Q

What happens to wing tip vortices in ground affect?

A

They are greatly reduced

24
Q

What causes a hung start?

A

Insufficient starting source, i.e. too little air from the starter

25
Q

What are the advantages of axial flow compressor over centrifugal flow compressors?

A

Axial flow compressors are highly efficient at high speeds, smaller frontal area for a given airflow, straight through flow allowing ram efficiency and increased pressure rise with increased number of stages with little losses

26
Q

When oil pressure drops what are some of the other indications within the cockpit that you can expect?

A

Higher oil temperatures, maybe higher fuel temps because of the fuel/oil heat exchanger experiences higher than normal oil temps, which in turn heats the fuel more

27
Q

What are the characteristics of an aircraft with a forward CG?

A

FWD CG means more stable, higher stall speed, lower cruise speed
“I love her Good”
Increased Longitudinal Stability, Lower Cruise speed, Higher Stall Speed, Good Stall/Spin Characteristics

28
Q

What causes an airplane to skid in a turn?

A

Rate of turn is too high

29
Q

Why does your TAS and GS increase for a given constant IAS at a high density airport?

A

Any given IAS requires the same amount of air molecules, and at a lower density of the air (higher density altitude) the only way to achieve this is with a higher actual speed through the air (TAS), which then means a higher GS.

30
Q

You’re in manual pressurization mode and your cabin starts to climb when you decrease power for the descent. What can you do with your out flow valves and power?

A

Close outflow valve or increase power for more airflow into pressure vessel

31
Q

What are the takeoff/landing wake turbulence techniques behind an arriving and departing heavy?

A

Rotate prior to heavy’s rotation point, land past it’s touchdown point