Checked Limitations Flashcards
Circle to Land Approach Maneuver
Wx Minimums 1000/3 unless Jeppesen specifies minimums higher than 1000/3.
Use a MDA of 1000’ AFE, unless restricted to a higher altitude in the circle-to-land minimums.
Tripped CB
Only reset once. (2 minutes for cooling before resetting)
In flight - only if CA decides it is critical to the safe conduct of the flight.
TCAS
Pilots must immediately respond to TCAS information using the guidelines located in the QRH Maneuvers chapter.
Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS-II RA.
Maximum Operating Pressure Altitude
41,000
Maximum Altitudes for APU
Operation: 41,000
Electrics: 41,000
Bleed Air 17,000
Elec + Bleed Air 10,000
Cargo Bay
Aircraft must land within 60 minutes (180 ETOPS) of initial discharge of the fire protection system
Electrical Power: On the ground limit one generator operation (engine driven) to a maximum of:
215 amps
MAX: Air and Ground 215 amps max
Electrical Power: Do not remove AC power form the aircraft for at least:
30 sec after IRS shutdown
Flight Controls: Do not use the speedbrakes in flight: (3)
- Below 1000’ AGL
- Beyond the FLIGHT detent
- Greater than Flaps 10
Alternate Flap Duty Cycle Limit
One complete cycle then 5 min off.
One complete cycle is 0 to 15 to 0
The Alternate Flap Switch must be OFF for 15 seconds before reversing direction.
Max Flap Extension altitude
20,000’
Max / Min Fuel tank temp
+49° C / -37° C
Main tanks must be full if the center tank quantity is greater than:
1,000 lbs
Center tank fuel pumps must be ON for all operations with more than:
1,000 lbs in the center tank
For Ground Operations, center tank fuel pump must not be positioned ON unless the center tank quantity indicates:
More than 1,000 lbs. (Except when defueling or transferring fuel)
Fuel may be transferred from tank to tank or defueled with passengers on board provided:
The tank from which fuel is being taken is maintained at not less than 2,000 lbs.
Deplane all passengers and non-essential crew members if transferring from a tank with less than 2,000 lbs until the process has been completed and the respective fuel boost pumps are turned off.
Corresponding center tank fuel pump switch must be positioned OFF when:
A center tank LOW PRESSURE light illuminates.
When established in level flight, both center tank fuel switches should be positioned ON if:
The center tank contains usable fuel.
If the center tank is empty, both center tank fuel pump switches must be positioned OFF when:
The first center tank fuel pump LOW PRESSURE light illuminates.
Center tank fuel pumps must not be ON unless:
Personnel are available on the flight deck to monitor the low pressure lights.
Flight Crews must not reset a tripped: (3)
Fuel Quantity Indicator,
Fuel Pump, or
Fuel Pump Control
CBs
Holding in Icing Conditions with flaps extended is
Prohibited
Engines and APU Max EGT for ground start:
725° C
Operate engines at or near idle, after rollback, for a minimum of:
2 minutes prior to applying takeoff thrust.
MAX - 3 minutes
Operate engines at or near idle for a minimum of
1 minute prior to shutdown
MAX - 3 minutes
Reverse Thrust limitation:
Intentional selection of reverse thrust in flight is prohibited.
Do not operate the weather radar
During fueling,
Near fuel spills, or
Near people
The in flight reset of a tripped CB should only be accomplished:
At the direction of the QRH
Allow approx. 2 minutes for cooling prior to resetting
Resetting a tripped CB other than directed by the QRH should only be accomplished if:
in the Judgement of the Captain, regaining use of that system is critical to the safe conduct of the flight.
CABIN ALTITUDE WARNING or
Rapid Depressurization
- Don oxygen masks and set regulators to 100%
2. Establish Crew Communications.
APU FIRE
- APU fire switch - CONFIRM - Pull, rotate to the stop, and hold for 1 second.
- APU switch - OFF
Aborted Engine Start
- Engine start lever (affected engine) - CUTOFF
Do not operate the wing anti-ice on the ground when the OAT is above:
10°C or 50°F
Do not use wing anti-ice as a substitute for
ground deicing/anti-icing and inspection procedures which are necessary to comply with operating rules.
-700: Do not operate at speeds in excess of ____ at weights over _______ with the speedbrake wing load alleviation system is inoperative.
320 kt
143,000 lbs
With Engine Bleed Air switches ON…
… do not operate the Packs in HIGH for takeoff, approach, or landing.
The fire protection non-normal procedures (QRH) take precedence over the statement regarding no air conditioning pack in HIGH during takeoff, approach, or landing. The CARGO FIRE and Smoke or Fumes Removal checklists require the operating pack switch(es) to be placed in HIGH in order to increase ventilation for smoke removal.
