Checked Limitations Flashcards by Adam E

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.

1,000, 3

Jeppesen approach chart

it specifies minimums higher than 1,000/3

higher minimums

required

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Circle-to-Land Approach Maneuver

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

1000 ft above airport elevation

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

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Maximum Operating Pressure Altitude

41,000 feet

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Air Systems 1

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

engine bleed air switches

HIGH

takeoff, approach, landing

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Air Systems 1 (alt.)

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

air conditioning packs in HIGH

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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 _______________________________.

fire protection non-normal procedures (QRH)

CARGO FIRE and Smoke or Fumes Removal

increase ventilation for smoke removal

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Anti-Ice and Rain 1

__________ in icing conditions with flaps extended is _______________.

Holding

prohibited

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Anti-Ice and Rain 2

737 MAX -

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

wing anti-ice

above 10°C (50°F)

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Anti-Ice and Rain 2 (alt)

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

Do not operate

ground

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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.

ground deicing/anti-icing and inspection procedures

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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.

wing anti-ice

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Anti-Ice and Rain 4

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

fueling, fuel spills

people

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Anti-Ice and Rain 4 (alt)

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

weather radar

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Fuel System 1

Max Fuel Tank Temperature______

Min Fuel Tank Temperature______

+ 49C

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Fuel System 2

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

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Fuel System 3: Fuel Distribution

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

Main tanks

1000

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Fuel System 3: Fuel Distribution (alt)

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

full

center tank

1000 pounds

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Fuel System 3: Fuel Distribution Note 1

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

the effects of balance

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Fuel System 3: Fuel Distribution Note 1 (alt)

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

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1000 pounds

center tank

Fuel System 3: Fuel Distribution Note 2

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

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Center tank fuel pumps

center tank

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.

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center tank fuel

Fuel System

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

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not be positioned to ON

defueling or transferring fuel

Fuel System (alt)

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

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ground

the center tank fuel quantity exceeds 1000 lbs

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 __________________.

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OFF

defueling

transferring fuel

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 ____________________________________________.

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

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.

may fuel quantity 2,000 defueled deplane all Passengers non-essential Crew Members fuel boost pumps

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

fuel pump OFF LOW PRESSURE

Fuel System Center Tank Note 1 When established in level flight attitude, _______________________ should be positioned ON again if the center tank __________________________.

both center tank pump switches contains usable fuel

Fuel System Center Tank Note 1 (alt) When established in ________________________, both center tank pump switches should be positioned _____ again if the _____________ contains usable fuel.

level flight attitude ON center tank

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.

center tank fuel pump switches OFF LOW PRESSURE

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

215 amps

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

30 seconds IRS

Engines and APU (NG) Maximum EGT for Ground Start ____ (MAX) Maximum EGT for Ground Start ____

725°C 753°C (non-memory item)

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

two minutes three minutes takeoff thrust

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

one minute three minutes

Reverse Thrust Reverse thrust is for _________________ only.

ground use

Auxiliary Power Unit Max Altitude for Operation

41,000 ft

Auxiliary Power Unit Max Altitude for Electric Only

41,000 ft

Auxiliary Power Unit Max Altitude Bleed Air Only

17,000 ft

Auxiliary Power Unit Max Altitude Bleed & Electric

10,000 ft

Flight Controls Do not extend flaps above _________ feet ___________ altitude.

20,000 pressure

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.

one complete cycle 5 0° to 15° 0° OFF 15 seconds reversing

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

FLIGHT DETENT

Flight Controls Do not use speedbrakes in flight below __________________.

1,000 ft AGL

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

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

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

320 143,000 speedbrake wing load alleviation

Checked Limitations Flashcards

(47 cards)