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SWA New Hire > Checked Limitations > Flashcards

Checked Limitations Flashcards

1
Q

Circle-to-Land Approach Maneuver

Weather minimums are a _____-ft ceiling and ___miles visibility. Both ceiling and visibility criteria are required. Review the ______________ to see if _______________. If so, then those __________ are ______________ to execute the circle-to-land approach maneuver.

A

1,000, 3

Jeppesen approach chart

it specifies minimums higher than 1,000/3

higher minimums

required

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2
Q

Circle-to-Land Approach Maneuver

Use a minimum descent altitude of __________ unless __________________ on the approach chart.

A

1000 ft above airport elevation

restricted to a higher altitude in the circle-to-land minimums section

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3
Q

Maximum Operating Pressure Altitude

A

41,000 feet

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4
Q

Air Systems 1

With ___________ ON, do not operate the air conditioning packs in ______ for ________, _______ or______.

A

engine bleed air switches

HIGH

takeoff, approach, landing

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5
Q

Air Systems 1 (alt.)

With engine bleed air switches ____, do not operate the ___________________ for takeoff, approach, or landing.

A

ON

air conditioning packs in HIGH

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6
Q

Air Systems 2

The ____________________________________ take precedence over the statement regarding no air conditioning pack in HIGH during takeoff, approach, or landing. The __________________________________ checklists require the operating pack switch(es) to be placed in HIGH in order to _______________________________.

A

fire protection non-normal procedures (QRH)

CARGO FIRE and Smoke or Fumes Removal

increase ventilation for smoke removal

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7
Q

Anti-Ice and Rain 1

__________ in icing conditions with flaps extended is _______________.

A

Holding

prohibited

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8
Q

Anti-Ice and Rain 2

737 MAX -

Do not operate ______________ on the ground when the OAT is _______________.

A

wing anti-ice

above 10°C (50°F)

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9
Q

Anti-Ice and Rain 2 (alt)

737 MAX -
_______________ wing anti-ice on the________ when the OAT is above 10°C (50°F).

A

Do not operate

ground

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10
Q

Anti-Ice and Rain 3

737 MAX - Do not use wing anti-ice as a substitute for ______________________________________ which are necessary to comply with operating rules.

A

ground deicing/anti-icing and inspection procedures

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11
Q

Anti-Ice and Rain 3 (alt)

737 MAX - Do not use _____________________ as a substitute for ground deicing/anti-icing and inspection procedures which are necessary to comply with operating rules.

A

wing anti-ice

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12
Q

Anti-Ice and Rain 4

Do not operate the weather radar during _____________, near ___________, or near_______________.

A

fueling, fuel spills

people

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13
Q

Anti-Ice and Rain 4 (alt)

Do not operate the _________________ during fueling, near fuel spills, or near people.

A

weather radar

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14
Q

Fuel System 1

Max Fuel Tank Temperature______

Min Fuel Tank Temperature______

A

+ 49C

  • 37C
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15
Q

Fuel System 2

Note: Jet A freeze point is
______, and other listed fuels freeze at lower temperatures.

A
  • 40C
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16
Q

Fuel System 3: Fuel Distribution

___________ must be full if the center tank quantity is greater than _____ pounds.

A

Main tanks

1000

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17
Q

Fuel System 3: Fuel Distribution (alt)

Main tanks must be ______ if the _______________ quantity is greater than _______________.

A

full

center tank

1000 pounds

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18
Q

Fuel System 3: Fuel Distribution Note 1

1000 pounds may be retained in the center tank provided __________________ have been considered.

A

the effects of balance

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19
Q

Fuel System 3: Fuel Distribution Note 1 (alt)

________________ may be retained in the ____________ provided the effects of balance have been considered.

A

1000 pounds

center tank

20
Q

Fuel System 3: Fuel Distribution Note 2

__________________ must be ON for takeoff with more than 1000 pounds of fuel in the ______________.

A

Center tank fuel pumps

center tank

21
Q

Fuel System 3: Fuel Distribution Note 2 (alt)

If there are more than 1000 pounds of fuel in the center tank, then _________ pumps must be ___ for takeoff.

A

center tank fuel

ON

22
Q

Fuel System

For ground operation, center tank fuel pump switches must __________________ unless the center tank fuel quantity exceeds 1000 lbs, except when _____________________.

A

not be positioned to ON

defueling or transferring fuel

23
Q

Fuel System (alt)

For____________ operation, center tank fuel pump switches must not be positioned to ON unless ___________________, except when defueling or transferring fuel.

A

ground

the center tank fuel quantity exceeds 1000 lbs

24
Q

Fuel System (alt 2)

IF ground ops AND center tank fuel quantity is less than 1000 lbs, THEN center tank fuel pump switches must be positioned to ____ , UNLESS ____________ or __________________.

A

OFF

defueling

transferring fuel

25
Q

Fuel System Transfers

Fuel may be transferred from tank to tank or the aircraft may be defueled with Passengers onboard, provided ______________________________________.

________________________ when defueling a tank or transferring fuel from a tank that has a fuel quantity below 2000 lb. until the process has been completed and ____________________________________________.

A

the fuel quantity in the tank from which fuel is being taken is maintained at not less than 2000 lb

Deplane all Passengers and non-essential Crew Members

the respective fuel boost pumps are turned off

26
Q

Fuel System Transfers (alt)

During defueling or while fuel is being transferred from tank to tank, Passengers ___ remain onboard provided the ____________ in the tank that’s being reduced is maintained above _____ lbs.

If the fuel quantity in the tank being reduced is less than 2,000 lbs, ____________ and ____________________ until the process has been completed and the respective _____________________ are turned off.

A

may

fuel quantity

2,000

defueled

deplane all Passengers

non-essential Crew Members

fuel boost pumps

27
Q

Fuel System Center Tank

Corresponding center tank __________________ switch must be positioned to ____ when a center tank _____________________ light illuminates.

A

fuel pump

OFF

LOW PRESSURE

28
Q

Fuel System Center Tank Note 1

When established in level flight attitude, _______________________ should be positioned ON again if the center tank __________________________.

A

both center tank pump switches

contains usable fuel

29
Q

Fuel System Center Tank Note 1 (alt)

When established in ________________________, both center tank pump switches should be positioned _____ again if the _____________ contains usable fuel.

A

level flight attitude

ON

center tank

30
Q

Fuel System Center Tank Note 1

If the center tank is empty, both ____________________ must be positioned ______ when the first center tank fuel pump _______________________ light illuminates.

A

center tank fuel pump switches

OFF

LOW PRESSURE

31
Q

Electrical Power

On the ground, limit one generator operation (engine driven) to a maximum of ______ .

A

215 amps

32
Q

Electrical Power

Do not remove AC power from the aircraft for at least __________ after ____ shutdown.

A

30 seconds

IRS

33
Q

Engines and APU

(NG) Maximum EGT for Ground Start ____

(MAX) Maximum EGT for Ground Start ____

A

725°C

753°C (non-memory item)

34
Q

Engines and APU

Operate engines at or near idle, after rollback, for a minimum of __________ (NG), __________ (MAX), prior to applying ________________ .

A

two minutes

three minutes

takeoff thrust

35
Q

Engines and APU

Operate engines at or near idle for a minimum of _____________ (NG), ______________ (MAX), prior to shutdown.

A

one minute

three minutes

36
Q

Reverse Thrust

Reverse thrust is for _________________ only.

A

ground use

37
Q

Auxiliary Power Unit

Max Altitude for Operation

A

41,000 ft

38
Q

Auxiliary Power Unit

Max Altitude for Electric Only

A

41,000 ft

39
Q

Auxiliary Power Unit

Max Altitude Bleed Air Only

A

17,000 ft

40
Q

Auxiliary Power Unit

Max Altitude Bleed & Electric

A

10,000 ft

41
Q

Flight Controls

Do not extend flaps above _________ feet ___________ altitude.

A

20,000

pressure

42
Q

Flight Controls

Alternate flap duty cycle in flight is _____________, then ____ minutes off.

A complete cycle is movement from position ______________ and back to ____. The ALTERNATE FLAP position switch must be in the _____ position for __________ before ______________ the direction of flap movement.

A

one complete cycle

5

0° to 15°

0°

OFF

15 seconds

reversing

43
Q

Flight Controls

In flight, do not extend the speedbrake lever beyond the _________________

A

FLIGHT DETENT

44
Q

Flight Controls

Do not use speedbrakes in flight below __________________.

A

1,000 ft AGL

45
Q

Flight Controls

NG - In flight, do not use speedbrakes with greater than flaps ___.

A

10

46
Q

Flight Controls

MAX - In flight, do not use speedbrakes with greater than flaps ___.

A

10

47
Q

Flight Controls

7W - Do not operate the aircraft at speeds in excess of ____ kt at weights over ___________ lb if the ________________ system is inoperative.

A

320

143,000

speedbrake wing load alleviation

SWA New Hire (2 decks)

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