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CQ 2024 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Circle to Land Wx Minimums

A

1000 ft ceiling

3 Miles Visibility

1000/3

1,000-ft ceiling and 3 miles visibility. Both ceiling and visibility criteria are required. Review the Jeppesen approach chart to see if it specifies minimums higher than 1,000/3. If so, then those higher minimums are required

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2
Q

Circle to Land Approach - Minimum descent altitude (MDA)

A

1000 ft above airport elevation unless restricted higher.

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3
Q

Max Operating Pressure Altitude

A

41,000

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4
Q

Engine Bleeds — ON—

Do not operate PACK in what setting?

A

Do no operate PACKS in HIGH for take off 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.

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5
Q

Anti Ice

Holding in icing conditions (flaps?)

A

Holding in icing conditions with flaps extended is prohibited.

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6
Q

Anti Ice and Rain

Above 10ºC

A

Do not operate wing anti-ice on the ground when the OAT is above 10ºC (50ºF).

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7
Q

Anti-Ice and Rain

Can you substitute wing anti-ice for ground de icing/anti-icing and inspection procedures?

A

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

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8
Q

Anti-Ice and Rain

Should you operate weather radar, while fueling, near fuel spills, or near people?

A

Do not operate the weather radar during fueling, near fuel spills, or near people.

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9
Q

Electric Power - Limitations
NG
MAX

A

NG - On the ground, limit one generator operation (engine driven) to maximum 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 30 seconds after IRS shutdown.

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10
Q

Circuit Breakers

Tripped circuit breakers in flight.

A

The in-flight reset of a tripped circuit breaker should only be accomplished when directed by the QRH. Allow approximated two minutes for cooling before resetting.

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11
Q

Circuit breakers

Resetting other than when directed by QRH

A

A tripped circuit breaker may only be reset once. Allow approximately two minutes fro cooling before resetting. An in-flight reset should only be accomplished it, in the judgement of the Captain, regaining use of that system is critical to the safe conduct of the that system is critical to the safe conduct of flight.

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12
Q

Engines and APU
Max EGT temp ground start
NG
MAX

A

NG - 725º
Operate at idle - 2 minutes prior to T/O thrust
Shutdown - idle for 1 minute before shutdown.

MAX - 753º
Operate at idle - 3 minutes prior to T/O thrust.
Shutdown - idle for 3 minutes

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13
Q

Reverse Thrust in flight?

A

Intentional selection of reverse thrust in flight is prohibited.

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14
Q 
APU 
Max altitude for operation. 
Max altitude for electric only 
Max altitude for bleed air only
Max altitude for bleed and electric
A

Operation - 41,000 ft
Electric only - 41,000 ft
Bleed Only - 17,000 ft
Bleed and Electric - 10,000 ft

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15
Q

Flight Controls

Max altitude flap?

A

20,000 ft

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16
Q

Flap duty cycle.

A

A flap duty cycle in flight is one complete cycle, then 5 minutes off. A complete cycle is movement form 0º to 15º and back to 0º.

  • The ALTERNATE FLAP position mist be in the OFF position for 15 second before reversing the direction of flap movement.
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17
Q

Flight Controls

Speed brake

A
  • In flight, do not extend the speed brake lever beyond the FLIGHT DETENTION.
  • Do not use Speed-brakes in flight before 1,000 ft AGL.
  • In flight, do not use speed-brakes with greater than flaps 10.
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18
Q

Flight Controls

-700W speed limitations

A

-700W - do not operate the aircraft at speeds in excess of 320 kts at weights over 143,000 lb if the speed-brake wing lead alleviation system is inoperative.

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19
Q

Fuel
Max fuel tank temp?
Min fuel tank temp?

A

Max fuel tank temp: +49ºC
Min fuel tank temp: -37ºC
*Note: Jet A freeze point is -40ºC, and other listed fuels freeze at lower temperatures.

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20
Q

Fuel systems

When must main tanks be full?

A

Main tanks must be full if the center tank quantity is greater than 1000 lbs.
Note 5: 1000 lbs may be retained in the center tank provided the effects of balance have been considered.
Note 6: Center tank fuel pumps must be ON for all operational with more than 1000 lb of fuel in the center tank.
Note 7: Some MEL items can override this limitation.
!!! * For ground operation, center tank fuel pump switches must NOT be positioned to ON unless the center fuel tank quantity exceeds 1000 lbs, except when de-fueling, or when when transferring fuel.

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21
Q

Fuel Systems:

Transferring fuel / de-fueling

A

Note: Fuel may be transferred from tank to tank or the aircraft may be refueled with Passengers onboard, provided 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 when de-fueling a tank or transferring fuel from a tank that has a fuel quantity below 2000 lb. Until the process has been completed and the respective fuel boost pumps are turned off.

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22
Q

Fuel Systems

LOW PRESSURE light illuminates

A

Corresponding center tank fuel pump switch must be positioned to OFF when a center tank LOW PRESSURE light illuminates.

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23
Q

Fuel Systems;

Note 7: When on the ground fuel LOW PRESSURE light illuminates.

A

Note 7: When on the ground, if the center tank fuel pump LOW PRESSURE light illuminates with useable fuel greater than 1,000 lb in the center tank, refer to 16.12.5 center Tank Fuel Pump LOW PRESSURE Light Illuminated on the ground.

Note: When established in level flight attitude, both center tank pump switches should be positioned ON again if the center tank contains usable fuel.

Note: If the center tank is empty, both center tank fuel pump switches must be positioned OFF when the the first center tank fuel pump LOW PRESSURE light illuminates.

24
Q

Fuel Systems

Center Fuel pumps not ON unless personnel available to monitor LOW PRESSURE lights.

A

!!! * 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.

25
Q

Cargo Bay Fire Suppression:

A

!!! * Aircraft must land within 60 minutes (8E) and (MAX8E - 180 - minutes) of initial discharge of the fire suppression system.

26
Q

TCAS

A

!!! * 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.

27
Q

All situations

A
  • Maintain Aircraft Control
  • Analyze the Problem
  • Take Appropriate Action
  • Maintain Situational Awareness
28
Q

QRC NG

CABIN ALTITUDE WARNING or Rapid Depressurization

A
  1. Don oxygen masks and set regulators to 100%

2. Establish Crew Communications.

29
Q

QRC NG

Runaway Stabilizer

A
  1. Control column ——————————— Hold Firmly
  2. Autopilot (if engaged) —————————Disengage
  3. Auto throttle (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 auto throttle.
    ***
  7. If the runaway continues after the autopilot is disengaged:
    STAB TRIM cutout switches (both)——-CUTOUT
    If the runaway continues:
  8. Stabilizer trim wheel ——————————Grasp and Hold.
    —————————————————————————————-
    - Go to QRH ch.9 Runaway Stabilizer checklist.
30
Q

Airspeed Unreliable

A
  1. Autopilot ——————————Disengage
  2. Auto throttle ————————- Disengage
  3. F/D switches————————- OFF
  4. Set the following gear up pitch attitude and thrust:
    Flaps extended—————- 10º and 80% N1
    Flaps up————————— 4º and 75% N1
    ————————————————————————
    - Go to QRH Ch. 10 Airspeed Unreliable checklist.
31
Q

QRC NG

APU FIRE

A
  1. APU Fire fire switch ——-confirm —— Pull, rotate to the stop, and hold, and hold for 1 second
  2. APU switch ————————————-OFF
    ———————————————————————————————————-
    - Go to QRH Ch. * APU FIRE checklist
32
Q

QRC NG

Aborted Engine Start

A
  1. Engine Start lever (affected engine)—————- CUTOFF
    ——————————————————————————-
    Go to QRH Ch.7 Aborted Engine Start Checklist.
33
Q

QRC MAX

CABIN ALTITUDE WARNING or Rapid Depressurization

A
  1. Don oxygen masks and set regulators to 100%

2. Establish Crew communications.

34
Q

QRC Max

Runaway Stabilizer

A
  1. Control column ——————————— Hold Firmly
  2. Autopilot ————————— —————Disengage
  3. Auto-throttle —————————————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 Auto pilot or Auto Throttle
  7. STAB TRIM cutout switches (both) ———Cutout
  8. If runaway continues
    Trim wheel —————————————Grasp and hold
    ——————————————————————
    Go to QRH Ch. 9 Runaway Stabilizer checklist.
35
Q

QRC
Airspeed Unreliable
MAX

A 
Airspeed Unreliable
1. Autopilot ———————————— Disengage
2. Auto-throttle ——————————-Disengage
3. F/D switches ——————————OFF
4. Set the following gear up pitch attitude and thrust:
	Flaps extended ———————-10º and 80% N1
	Flaps up———————————-4º and 75% N1
————————————————————————-
- Go to QRH Ch. 10 Airspeed Unreliable Checklist
36
Q

QRC MAX

APU FIRE

A
  1. APU Fire Switch ———- Confirm———-Pull, rotate to the stop, and hold for 1 second
  2. APU switch —————————————OFF
    ———————————————————————————-
    - Go to QRH Ch. 8 APU FIRE checklist.
37
Q

QRC MAX

Aborted Engine Start

A
  1. Engine start lever (affected engine)—————— CUTOFF
    ————————————————————————————-
    - Go to QRH Ch. 7 Aborted Engine Start checklist.
38
Q

Q.2.2. Do not remove AC power from the aircraft for at least ____ seconds after IRS shutdown.

A

30

39
Q

Q.2.4. 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

40
Q

Q.2.5. 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)

41
Q

Q.3.3. A complete cycle is movement from position __° to ___° and back to ___°.

A

0° to 15° and back to 0°

42
Q

Q.3.4. The ALTERNATE FLAP position switch must be in the OFF position for ___ seconds before reversing the direction of flap movement.

A

15 seconds

43
Q

Q.3.6. Do not use speedbrakes in flight below _______ ft AGL.

A

1,000

44
Q

Q.3.7. In flight, do not use speedbrakes with greater than flaps ______.

A

10

45
Q

Q.3.12. 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.

46
Q

Q.3.13. 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.

47
Q

Q.3.15. 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.

48
Q

Q.3.16. 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

49
Q

Q.3.17. 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.

50
Q

Q.3.18. Flight Deck Crews must not reset these 3 tripped fuel circuit breakers

A

Fuel quantity indicator
Fuel pump
Fuel pump control

51
Q

Q.4.2. 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).

52
Q

Q.4.3. 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

53
Q

Q.4.4. A tripped circuit breaker may be reset in-flight when ___________________ ?

A

directed by the QRH

54
Q

Q.4.5. How many times can a circuit breaker be reset?

A

Once.

55
Q

Q.4.6. How long should you let a circuit breaker cool before resetting when directed by the QRH?

A

Approximately two minutes.

56
Q

Q.4.7. 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.

CQ 2024 Limitations (3 decks)

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