Checked Limitations Flashcards
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
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
Maximum Operating Pressure Altitude
41,000 feet
Air Systems 1
With ___________ ON, do not operate the air conditioning packs in ______ for ________, _______ or______.
engine bleed air switches
HIGH
takeoff, approach, landing
Air Systems 1 (alt.)
With engine bleed air switches ____, do not operate the ___________________ for takeoff, approach, or landing.
ON
air conditioning packs in HIGH
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
Anti-Ice and Rain 1
__________ in icing conditions with flaps extended is _______________.
Holding
prohibited
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)
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
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
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
Anti-Ice and Rain 4
Do not operate the weather radar during _____________, near ___________, or near_______________.
fueling, fuel spills
people
Anti-Ice and Rain 4 (alt)
Do not operate the _________________ during fueling, near fuel spills, or near people.
weather radar
Fuel System 1
Max Fuel Tank Temperature______
Min Fuel Tank Temperature______
+ 49C
- 37C
Fuel System 2
Note: Jet A freeze point is
______, and other listed fuels freeze at lower temperatures.
- 40C
Fuel System 3: Fuel Distribution
___________ must be full if the center tank quantity is greater than _____ pounds.
Main tanks
1000
Fuel System 3: Fuel Distribution (alt)
Main tanks must be ______ if the _______________ quantity is greater than _______________.
full
center tank
1000 pounds
Fuel System 3: Fuel Distribution Note 1
1000 pounds may be retained in the center tank provided __________________ have been considered.
the effects of balance
Fuel System 3: Fuel Distribution Note 1 (alt)
________________ may be retained in the ____________ provided the effects of balance have been considered.
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 ______________.
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.
center tank fuel
ON
Fuel System
For ground operation, center tank fuel pump switches must __________________ unless the center tank fuel quantity exceeds 1000 lbs, except when _____________________.
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.
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 __________________.
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 ___.
10
Flight Controls
MAX - In flight, do not use speedbrakes with greater than flaps ___.
10
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
