Limitations And Memory Items Flashcards
Weather for Circling Approach
1000’ ceiling and 3 SM visibility unless approach chart’s minimums are higher, then use those.
Minimum descent altitude on circling approach
1000’ AFE unless restricted higher by approach plate.
Max operating pressure altitude
41000’
With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for:
Takeoff, approach, or landing
Holding in icing conditions with flaps extended is:
Prohibited
Do not operate the wing anti-ice on the ground when the OAT is above:
10 degrees Celsius
(NG) On the ground, limit one generator operation (engine driven) to a max of:
215 amps
(MAX) Limit one generator operation (engine driven) to a maximum of:
215 amps on the ground or in the air
Do not remove AC power from the aircraft for at least how many seconds after IRS shutdown?
30 seconds
Max EGT for ground start:
725 degrees Celsius (NG)
753 degrees Celsius (MAX)
Operate engines at or near idle, after rollback, for how long prior to applying takeoff thrust?
2 minutes (NG)
3 minutes (MAX)
Operate engines at or near idle for how long before shutdown?
1 minute (NG)
3 minutes (MAX)
Intentional selection of reverse thrust in flight is:
Prohibited
APU max altitude for operation
41000’
APU max altitude for electrics only
41000’
APU max bleed air only
17000’
APU max bleed air and electrics
10,000’
Do not extend flaps above what altitude
20,000’ pressure altitude
Alternate flap duty cycle in flight is one complete cycle then how long off?
5 minutes
A complete flap duty cycle is movement from positions:
0 to 15 degrees and then back to 0 degrees.
In flight, don’t extend the speed brake lever beyond the:
FLIGHT DETENT
Do not use speed brakes with flaps greater than:
10 degrees
Do not use speedbrakes in flight below:
1000’ AGL
Max fuel tank temperature
+49 degrees Celsius
Min Fuel Tank Temperature
-37 degrees Celsius for Jet A
-43° or 3° above fuel’s freezing point
Jet A freeze point is ___ C, and other listed fuels freeze at lower temperatures.
-40 degrees Celsius
Main fuel tanks must be full if the center tank quantity is greater than __ lb.
1000
1000 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 ___ lb of fuel in the center tank.
2000
Fuel may be transferred from tank to tank or the aircraft may be defueled with pax onboard, provided the fuel quantity in the tank from which fuel is being taken is maintained at not less than __ lb.
2000
Deplane all pax and non-essential crew members when refueling a tank or transferring fuel from a tank that has a fuel quantity below __ lb until the process has been completed and the respective fuel boost pumps are turned off.
2000
Corresponding center tank fuel pump switch must be positioned __ when a center tank LOW PRESSURE light illuminates.
OFF
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, 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 deck crews must not reset tripped:
fuel quantity indicator, fuel pump, or fuel pump control circuit breakers.
Aircraft must land within __ minutes (8E and MAX8E: __ minutes) of initial discharge of the fire suppression system.
60, 180
Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the:
TCAS II Resolution Advisory (RA)
Flight crews must immediately respond to TCAS information (both TA’s and RA’s) by using:
The TCAS (traffic avoidance) guidelines located in the QRH Maneuvers Chapter.
CABIN ALTITUDE WARNING or Rapid Depressurization Immediate Action Items
- Don oxygen masks and set regulators to 100%
- Establish crew communications
Runaway Stabilizer Immediate Action Items
- Control column: hold firmly
- Autopilot (if engaged): disengage
- Autothrottle (if engaged): disengage
- Control column and thrust levers: control aircraft pitch attitude and airspeed
- Main electric stabilizer trim: reduce control column forces
- If the runaway STOPS after autopilot is disengaged: Do not re-engage the autopilot or autothrottle.
- 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
Airspeed Unreliable Immediate Action Items
- Autopilot (if engaged): disengage
- Autothrottle (if engaged): disengage
- F/D switches (both): OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended: 10 degrees and 80% N1
Flaps up: 4 degrees and 75% N1
APU FIRE Immediate Action Items
- APU fire switch: Confirm… Pull, rotate to the stop, and hold for 1 second
- APU switch: OFF
Aborted Engine Start Immediate Action Items
- Engine start lever (affected engine): CUTOFF
After turning the APU off, approximately how long should you wait before turning the battery switch off?
(NG) 2 min
(MAX) 5 min
The ALTERNATE FLAP position switch must be in the OFF position for how long before reversing the direction of flap movement?
15 seconds
Do not operate Engine Anti-Ice (EAI) in-flight when
Not in actual or anticipated icing conditions.
The wing anti-ice switch will be turned OFF when?
Prior to beginning the takeoff roll.
To prevent nuisance computer faults when ground power is not available, ensure how many seconds have elapsed between
placing the battery switch ON and starting the APU
30 seconds
