Limitations Flashcards
What are the weather minimums to perform a Circle-to-Land Approach Maneuver?
1,000-ft ceiling and 3 miles visibility. Both ceiling and visibility criteria are required.
What is the correct MDA for a Circle-to-Land Approach Maneuver?
1,000 ft AAE unless restricted to a higher altitude in the circle-to-land minimums section on the approach chart.
What is the Maximum Operating Pressure Altitude?
41,000 ft
With engine bleed air switches ON, do not operate the air conditioning packs in HIGH in what phases of flight?
Takeoff, approach, or landing
Note: 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.
Holding in icing conditions with flap extended.
prohibited
Do not operate wing anti-ice on the ground when the OAT is above?
10°C (50°F)
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
Do not operate the _______ _____ during fueling, near fuel spills, or near people.
weather radar
What is the maximum amperage limit during a one generator operation (engine driven)?
Maximum of 215 amps on the ground (NG)
Maximum of 215 amps on the ground or in the air (MAX)
Do not remove AC power from the aircraft for at least ____ seconds after IRS shutdown.
30
Maximum EGT for Ground Start ___°C (NG)
725°C (NG)
Prior to applying takeoff thrust operate engines at or near idle, after rollback, for a minimum of ___ minutes (NG), and _____minutes (MAX).
Two minutes (NG)
Three minutes (MAX)
Prior to applying takeoff thrust
Prior to shutdown, operate engines at or near idle for a minimum of ________ minute (NG) (three desired), ________ minutes (MAX).
one minutes (NG)
three minutes (MAX)
Intentional selection of reverse thrust in flight is ?
prohibited
Max Altitude for APU operation
41,000 ft
Max Altitude for APU operation, Electric only
41,000 ft
Max Altitude for APU operation, Bleed Air only
17,000 ft
Max Altitude for APU operation, Bleed & Electric
10,000 ft
Do not extend flaps above ________ feet pressure altitude.
20,000 ft
Alternate flap duty cycle in flight is one complete cycle, then ____ minutes off.
5 minutes
A complete cycle is movement from position __° to ___° and back to ___°.
0° to 15° and back to 0°
The ALTERNATE FLAP position switch must be in the OFF position for ___ seconds before reversing the direction of flap movement.
15 seconds
In flight, do not extend the speedbrake lever beyond the
FLIGHT DETENT
Do not use speedbrakes in flight below _______ ft AGL.
1,000
In flight, do not use speedbrakes with greater than flaps
10
(7W) If the speed brake wing load alleviation system is inoperative, do not operate the aircraft at speeds in excess of _____ kt at weights over __________ lb.
320 kt at weights over 143,000 lb
What is the Max Fuel Tank Temperature?
+ 49°C
What is the Min Fuel Tank Temperature?
- 37°C
Note: Jet A freeze point is - 40°C, and other listed fuels freeze at lower temperatures.
Main tanks must be full if the center tank quantity is greater than ______________.
1,000 pounds
Note: 1,000 pounds may be retained in the center tank provided the effects of balance have been considered.
Center tank fuel pumps must be ON for all operations with more than this amount of fuel.
1,000 pounds of fuel in the center tank.
Note: Some MEL items can override this limitation.
For ground operation, center tank fuel pump switches must not be positioned to ON unless the center tank fuel quantity exceeds what quantity?
1,000 lb, except when defueling or transferring fuel
Fuel may be transferred from tank to tank or the aircraft may be defueled with Passengers onboard, provided:
the fuel quantity in the tank from which fuel is being taken is maintained at not less than 2,000 lb.
When must the corresponding center tank fuel pump switch be positioned to OFF?
When a center tank LOW PRESSURE light illuminates.
Note: When established in level flight attitude, both center tank pump switches should be positioned ON again if the center tank contains usable fuel.
If the center tank is empty, when must both center tank fuel pump switches must be positioned OFF?
When the first center tank fuel pump LOW PRESSURE light illuminates.
Deplane all Passengers and non-essential Crew Members when defueling a tank or transferring fuel from a tank that has a fuel quantity below what quantity?
2,000 lb until the process has been completed and the respective fuel boost pumps are turned off.
Flight Deck Crews must not reset these 3 tripped fuel circuit breakers:
Fuel quantity indicator
Fuel pump
Fuel pump control
Aircraft must land within _____ minutes (non-ETOPS) or ______ minutes (ETOPS) of initial discharge of the fire suppression system.
60/ 180
Are Pilots authorized to deviate from an ATC clearance when responding to an RA?
YES, to the extent necessary to comply with the TCAS II Resolution Advisory (RA).
What guidelines are used by Flight Crews to immediately respond to TCAS information (both TAs and RAs)?
TCAS (Traffic Avoidance) guidelines located in the AOM Chapter 5.15 Non-Normal Maneuvers.
A tripped circuit breaker may be reset in-flight when ?
directed by the QRH
How many times can a circuit breaker be reset?
Once
How long should you let a circuit breaker cool before resetting when directed by the QRH?
Approximately two minutes.
An in-flight reset should only be accomplished if:
In the judgment of the Captain, regaining use of that system is critical to the safe conduct of flight.
APU FIRE
APU Fire Switch….Confirm….pull, rotate to the stop, and hold for one second.
APU Switch…………………………Off
CABIN ALTITUDE WARNING HORN OR Rapid Depressurization
1.Don oxygen masks and set regulators to 100%.
2. Establish Crew communications.
Aborted Engine Start
1.Engine start level (affected engine)……CUTOFF
Airspeed Unreliable
1.Autopilot (if engaged)……….Disengage
2.Autothrottle (if engaged)….Disengage
3.F/D switches (both)……………Off
4.Set the following gear up pitch attitude and thrust:
Flaps extended…..10° and 80% N1
Flaps up……..4° and 75% N1
Runaway Stabilizer
1.Control column……Hold firmly
2.Autopilot (if engaged)……Disengage
3.Autothrottles (if engaged)….Disengage
4.Control column and thrust levers….control aircraft pitch attitude and airspeed.
5.Main Electric
Stabilizer trim………..Reduce control column forces
6.If the runaway stops after the autopilot is disengaged: Do NOT re-engage the autopilot or autothrottles.
7.If the runaway continues after the autopilot is disengaged: STAB TRIM cutout switches (both)….CUTOUT
IF the runaway continues: stabilizer trim wheel…. Grasp and hold
