Limitations Flashcards

1
Q

What are the weather minimums to perform a Circle-to-Land Approach Maneuver?

A

1,000-ft ceiling and 3 miles visibility. Both ceiling and visibility criteria are required.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What is the correct MDA for a Circle-to-Land Approach Maneuver?

A

1,000 ft AAE unless restricted to a higher altitude in the circle-to-land minimums section on the approach chart.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What is the Maximum Operating Pressure Altitude?

A

41,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

With engine bleed air switches ON, do not operate the air conditioning packs in HIGH in what phases of flight?

A

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.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Holding in icing conditions with flap extended.

A

prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Do not operate wing anti-ice on the ground when the OAT is above?

A

10°C (50°F)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Do not use ______ ______ as a substitute for ground deicing/anti-icing and inspection procedures which are necessary to comply with operating rules.

A

wing anti-ice

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

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

A

weather radar

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What is the maximum amperage limit during a one generator operation (engine driven)?

A

Maximum of 215 amps on the ground (NG)
Maximum of 215 amps on the ground or in the air (MAX)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Do not remove AC power from the aircraft for at least ____ seconds after IRS shutdown.

A

30

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Maximum EGT for Ground Start ___°C (NG)

A

725°C (NG)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Prior to applying takeoff thrust operate engines at or near idle, after rollback, for a minimum of ___ minutes (NG), and _____minutes (MAX).

A

Two minutes (NG)
Three minutes (MAX)
Prior to applying takeoff thrust

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Prior to shutdown, operate engines at or near idle for a minimum of ________ minute (NG) (three desired), ________ minutes (MAX).

A

one minutes (NG)
three minutes (MAX)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Intentional selection of reverse thrust in flight is ?

A

prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Max Altitude for APU operation

A

41,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Max Altitude for APU operation, Electric only

A

41,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Max Altitude for APU operation, Bleed Air only

A

17,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Max Altitude for APU operation, Bleed & Electric

A

10,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Do not extend flaps above ________ feet pressure altitude.

A

20,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Alternate flap duty cycle in flight is one complete cycle, then ____ minutes off.

A

5 minutes

21
Q

A complete cycle is movement from position __° to ___° and back to ___°.

A

0° to 15° and back to 0°

22
Q

The ALTERNATE FLAP position switch must be in the OFF position for ___ seconds before reversing the direction of flap movement.

A

15 seconds

23
Q

In flight, do not extend the speedbrake lever beyond the

A

FLIGHT DETENT

24
Q

Do not use speedbrakes in flight below _______ ft AGL.

A

1,000

25
Q

In flight, do not use speedbrakes with greater than flaps

A

10

26
Q

(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.

A

320 kt at weights over 143,000 lb

27
Q

What is the Max Fuel Tank Temperature?

A

+ 49°C

28
Q

What is the Min Fuel Tank Temperature?

A
  • 37°C
    Note: Jet A freeze point is - 40°C, and other listed fuels freeze at lower temperatures.
29
Q

Main tanks must be full if the center tank quantity is greater than ______________.

A

1,000 pounds
Note: 1,000 pounds may be retained in the center tank provided the effects of balance have been considered.

30
Q

Center tank fuel pumps must be ON for all operations with more than this amount of fuel.

A

1,000 pounds of fuel in the center tank.
Note: Some MEL items can override this limitation.

31
Q

For ground operation, center tank fuel pump switches must not be positioned to ON unless the center tank fuel quantity exceeds what quantity?

A

1,000 lb, except when defueling or transferring fuel

32
Q

Fuel may be transferred from tank to tank or the aircraft may be defueled with Passengers onboard, provided:

A

the fuel quantity in the tank from which fuel is being taken is maintained at not less than 2,000 lb.

33
Q

When must the corresponding center tank fuel pump switch be positioned to OFF?

A

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.

34
Q

If the center tank is empty, when must both center tank fuel pump switches must be positioned OFF?

A

When the first center tank fuel pump LOW PRESSURE light illuminates.

35
Q

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?

A

2,000 lb until the process has been completed and the respective fuel boost pumps are turned off.

36
Q

Flight Deck Crews must not reset these 3 tripped fuel circuit breakers:

A

Fuel quantity indicator
Fuel pump
Fuel pump control

37
Q

Aircraft must land within _____ minutes (non-ETOPS) or ______ minutes (ETOPS) of initial discharge of the fire suppression system.

A

60/ 180

38
Q

Are Pilots authorized to deviate from an ATC clearance when responding to an RA?

A

YES, to the extent necessary to comply with the TCAS II Resolution Advisory (RA).

39
Q

What guidelines are used by Flight Crews to immediately respond to TCAS information (both TAs and RAs)?

A

TCAS (Traffic Avoidance) guidelines located in the AOM Chapter 5.15 Non-Normal Maneuvers.

40
Q

A tripped circuit breaker may be reset in-flight when ?

A

directed by the QRH

41
Q

How many times can a circuit breaker be reset?

A

Once

42
Q

How long should you let a circuit breaker cool before resetting when directed by the QRH?

A

Approximately two minutes.

43
Q

An in-flight reset should only be accomplished if:

A

In the judgment of the Captain, regaining use of that system is critical to the safe conduct of flight.

44
Q

APU FIRE

A

APU Fire Switch….Confirm….pull, rotate to the stop, and hold for one second.
APU Switch…………………………Off

45
Q

CABIN ALTITUDE WARNING HORN OR Rapid Depressurization

A

1.Don oxygen masks and set regulators to 100%.
2. Establish Crew communications.

46
Q

Aborted Engine Start

A

1.Engine start level (affected engine)……CUTOFF

47
Q

Airspeed Unreliable

A

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

48
Q

Runaway Stabilizer

A

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