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SWA B737 > SWA B737 - Checked Limitations/Immediate Action Items > Flashcards

SWA B737 - Checked Limitations/Immediate Action Items Flashcards

1
Q

(Checked Limitations) What is the limitation for the Cargo Bay Fire Suppression System?

A

Aircraft must land within 60 minutes of initial discharge of the Fire Suppression System (180 minutes for the MAX)

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2
Q

(Checked Limitations) What is the maximum altitude for operating the APU BLEED AIR and ELECTRIC?

A

10,000 feet

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3
Q

(Checked Limitations) You are ready for takeoff, you have 900 pounds of fuel in the center tank, what position should your center fuel pump switches be in?

A

They should both be OFF

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4
Q

(Checked Limitations) What is the maximum fuel tank Temperature?

A

+49 degrees C

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5
Q

(Checked Limitations) How long after IRS Shutdown do you have to wait before removing AC power?

A

Do not remove AC Power from the aircraft for at least 30 seconds after IRS shutdown.

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6
Q

(Checked Limitations) What is the checked limitation on Thrust Reversers?

A

Reverse Thrust is for ground use ONLY

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7
Q

(Checked Limitations) What is the maximum altitude for operating the APU?

A

FL410

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8
Q

(Checked Limitations) What is the limitation on PACK operation for Takeoff, Approach, and Landing?

A

With the Engine Bleed Air Switches ON, do not operate the air conditioning PACKS in HIGH for takeoff, approach, or landing.

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9
Q

(Checked Limitations) What is the limitation for holding in icing conditions?

A

Holding in Icing Conditions with Flaps Extended is PROHIBITED

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10
Q

(Checked Limitations) What are some fuel limitations (4 of them) while on the ground at the gate?

A
  • Main (wing) tanks must be full if the center fuel tank quantity is greater than 1000 pounds.
  • For ground operation, center tank fuel pump switches must NOT be positioned to ON unless the center tank fuel quantity exceeds 1000 pounds, except when defueling or transferring fuel.
  • Center Tank Fuel Pumps must not be selected ON unless personnel are available on the flight deck to monitor the low pressure lights.
  • Flight Crews must not reset tripped fuel quantity, fuel pump, or fuel pump control circuit breakers.
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11
Q

(Checked Limitations) What are the Speedbrake Limitations?

A
  • Do not use speedbrakes in flight below 1000 feet AGL.
  • In flight, do not extend the Speedbrake Lever beyond the Flight Detent.
  • In flight, do not use speedbrakes with Flaps greater than 10.
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12
Q

(Checked Limitations) What is the minimum fuel tank Temperature?

A

-37 degrees C

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13
Q

(Checked Limitations) What are the TCAS limitations?

A
  • 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
  • Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS II Resolution Advisory (RA)
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14
Q

(Checked Limitations) What is the maximum altitude for operating the APU BLEED AIR ONLY?

A

17,000 feet

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15
Q

(Checked Limitations) What is the Maximum Operating Pressure Altitude for the NG and MAX?

A

FL410

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16
Q

(Checked Limitations) When MUST the Center Tank Fuel Pumps be turned OFF.

A

• Corresponding Center Fuel Pump Switch must be positioned to OFF when a Center Tank LOW PRESSURE light illuminates.

(For Ground Operation, Center Tank Fuel Pump Switches must not be positioned to ON unless the center tank fuel quantity exceeds 1000 pounds, except when defueling or transferring fuel.)

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17
Q

(Checked Limitations) What are the limitations for tripped circuit breakers?

A
  • A tripped circuit breaker may only be reset once. Allow approximately two minutes for cooling before resetting. 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.
  • Flight Crews MUST NOT reset tripped fuel quantity, fuel pump, or fuel pump control circuit breakers.
  • The Flight Deck Crew should not cycle (pull and reset) a circuit breaker at any time unless the cycle meets one or more of the following criteria (• directed by the QRH, • directed by a procedure listed in the B737 AOM, FOM, MEL or Operations Binder, • coordinated and approved by MX)
  • IN FLIGHT - The in-flight reset if a tripped circuit breaker should only be accomplished when directed by the QRH. Allow approximately 2 minutes for cooling before resetting.
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18
Q

(Checked Limitations) Other than speed limitations, what is the limitation on the use of normal flaps?

A

Do not extend flaps above 20,000 feet

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19
Q

(Checked Limitations) What is the limitation on operating the radar?

A

Do not operate the WX Radar during fueling, near fuel spills, or near people.

20
Q

(Checked Limitations) What are the Engine limitations for cool down after landing?

A

NG - Operate Engines at or near idle for a MINIMUM of ONE minute prior to shutdown (recommend THREE minutes prior to shutdown)

MAX - Operate Engines at or near idle for a MINIMUM of THREE minutes prior to shutdown.

21
Q

(Checked Limitations) What Is the limitation for operating on one generator on the ground?

A

NG - Limit one Generator Operation (Engine Driven) to a Maximum of 215 Amps.

22
Q

(Checked Limitations) You are ready for takeoff, you have 1500 pounds of fuel in the center tank, what position should your center fuel pump switches be in?

A

They should both be ON.

23
Q

(Checked Limitations) What is the limitation on the Alternate Flaps?

A

Alternate Flap duty cycle in flight is one complete cycle, then 5 minutes OFF (a complete duty cycle is movement from position 0 to 15 and back to 0). The alternate flap switch MUST be in the OFF position for 15 seconds before reversing the direction of flap movement.

24
Q

(Checked Limitations) What is the maximum altitude for operating the APU ELECTRIC ONLY?

A

FL 410

25
Q

(Checked Limitations) What is the EGT limitation for Ground Start?

A

NG - 725 degrees C
MAX - Redline

(The EEC does not supply RED LINE protection, but will shut the engine down if it senses an impending hot start)

26
Q

(Checked Limitations) After starting, what are the limitations for Engine stabilization?

A

Operate Engines at or near IDLE, after rollback for a MINIMUM of TWO minutes (NG) or THREE minutes (MAX) prior to applying takeoff thrust.

(RECOMMENDATION: On the First Flight of the Day; operate engines at or near idle, after rollback, for minimum of FIVE minutes prior to applying takeoff thrust)

27
Q

(Checked Limitations) What are the Fuel Distribution limitations?

A
  • Main (wing) tanks must be full if the Center Tank quantity is greater than 1000 pounds.
  • Use Center Tank to depletion followed by wing tank fuel.
  • 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 1000 pounds of fuel in the center tank (Some MEL items can override this limitation).
28
Q

(Checked Limitations) What is the limitation for a Circle to Land Approach Maneuver?

A

WX minimums are 1000 ft. ceiling and 3 miles visibility. BOTH ceiling and visibility criteria are required. If the Jeppesen approach chart specifies minimums higher than 1000/3, now those higher minimums are required to execute the circle to land approach maneuver.

(Use a Minimum Descent Altitude (MDA) of 1000 ft. above airport elevation unless restricted to a higher altitude in the Circle to Land minimums section on the approach chart)

29
Q

(Checked Limitations) What us the Maximum Operating Pressure Altitude of the B-737?

A

FL410

30
Q

(Checked Limitations) Do not operate Wing Anti-Ice on the Ground when the OAT is above _____?

A

10 Degrees C (50 F)

31
Q

(Checked Limitations) 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

32
Q

(Checked Limitations) Do NOT operate the _____ _____ during fueling, near fuel spills, or near people.

A

Weather Radar

33
Q

(Checked Limitations) When can you reset a tripped circuit breaker?

A

When directed by the QRH or if in the judgement of the Captain, regaining use of that system is critical to the safe conduct of flight

NOTE: A tripped circuit breaker may only be reset once & allow approximately two minutes for cooling before resetting.

34
Q

(Checked Limitations) What is the Max Altitude for APU BLEED & ELECTRIC?

A

10,000 feet

35
Q

(Checked Limitations) In Flight, do NOT extend the Speedbrake Lever beyond the _____ _____.

A

FLIGHT DETENT.

36
Q

(Checked Limitations) What is authorized in relation the ATC Clearances and TCAS RA alerts?

A

Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS RA.

37
Q

(Checked Limitations) Do not use Speedbrakes in flight below _____ ft. AGL.

A

1000 ft

38
Q

(Checked Limitations) In flight, do NOT use Speedbrakes with greater than flaps _____.

A

Flaps 10

39
Q

(Checked Limitations) If the Speedbrake Wing Load Alleviation System is Inoperative, do NOT operate the aircraft at speeds in excess of _____ kts. at weights over ______ lbs.

A

320 kts. & 143,000 lbs.

40
Q

(Checked Limitations) 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 2000 lbs.

41
Q

(Immediate Action Items) APU FIRE

A

• APU Fire Switch - Confirm; Pull,
Rotate to the stop, & Hold for
one second.
• APU Switch - OFF

42
Q

(Immediate Action Items) CABIN ALTITUDE WARNING or Rapid Depressurization

A

• Don oxygen masks and set
regulators to 100%
• Establish Crew Communications

43
Q

(Immediate Action Items) Aborted Engine Start

A

• Engine Start Lever (Affected Engine)

- CUTOFF

44
Q

(Immediate Action Items) Airspeed Unreliable

A 
• Autopilot (if engaged) - Disengage
• Autothrottle (if engaged) - Disengage
• F/D Switches - OFF
• Set the following gear up pitch attitude and thrust:
    -Flaps Extended (10* & 80% N1)
    -Flaps Up (4* & 75% N1)
45
Q

(Immediate Action Items) Runaway Stabilizer

A 
• 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 Stabalizer Trim - 
     Reduce Control Column Forces

IF THE RUNAWAY STOPS AFTER THE
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) -
OFF

IF THE RUNAWAY CONTINUES:
• Stabalizer Trim Wheel - Grasp & Hold

SWA B737 (18 decks)

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