SWA MEMORY ITEMSSWA MEMORY ITEMS

What are the two memory items What are the two memory items for resetting tripped circuit for resetting tripped circuit

breakers?breakers?

A tripped circuit breaker may only be reset once. A tripped circuit breaker may only be reset once. Allow approximately Allow approximately 2 minutes2 minutes for cooling before for cooling before resetting. An in-flight reset should only be resetting. An in-flight reset should only be accomplished, if in the judgment of the Captain, accomplished, if in the judgment of the Captain, regaining use of that system is critical to the safe regaining use of that system is critical to the safe conduct of the flight.conduct of the flight.

Flight crews will not reset tripped fuel quantity Flight crews will not reset tripped fuel quantity indicator, fuel pump, or fuel pump control circuit indicator, fuel pump, or fuel pump control circuit breakers. breakers.

With regards to TCAS, what are With regards to TCAS, what are the flight crew responses?the flight crew responses?

Flight crews must immediately respond to Flight crews must immediately respond to TCAS information (both TA’s and RA’s) by TCAS information (both TA’s and RA’s) by using the TCAS (Traffic Avoidance) guidelines using the TCAS (Traffic Avoidance) guidelines located in the located in the “Non-normal Operations: “Non-normal Operations: Maneuvers and Profiles.”Maneuvers and Profiles.”

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

What are the wind component What are the wind component limitations?limitations?

ConditionsConditions Steady Cross WindSteady Cross Wind Peak Gust TailwindPeak Gust Tailwind

TakeoffTakeoff LandingLanding TakeoffTakeoff LandingLanding

DryDry 35 knots35 knots 35 knots35 knots 10 knots10 knots 10 knots10 knots

WetWet 35 knots35 knots 35 knots35 knots 10 knots10 knots 10 knots10 knots

<4000’ RVR or ¾ <4000’ RVR or ¾ mile visibilitymile visibility 35 knots35 knots 10 knots10 knots 10 knots10 knots 10 knots10 knots

<1600’ RVR or ¼ <1600’ RVR or ¼ mile visibilitymile visibility 20 knots20 knots 10 knots10 knots 10 knots10 knots 10 knots10 knots

<600’ RVR<600’ RVR 10 knots10 knots ------ 10 knots10 knots ------

ClutterClutter 20 knots20 knots 20 knots20 knots 10 knots10 knots 10 knots10 knots

Braking FairBraking Fair 15 knots15 knots 15 knots15 knots 10 knots10 knots 10 knots10 knots

Braking PoorBraking Poor 10 knots10 knots 10 knots10 knots 5 knots5 knots 5 knots5 knots

What are the maximum operating What are the maximum operating pressure altitudes?pressure altitudes?

(-700)(-700) 41,000 feet41,000 feet(-300/500)(-300/500) 37,000 feet37,000 feet

What is the Bleed and PACK limitation What is the Bleed and PACK limitation for takeoff, approach, and landing?for takeoff, approach, and landing?

With engine bleed air switches ON; do With engine bleed air switches ON; do not operate the air conditioning packs in not operate the air conditioning packs in HIGH for takeoff, approach, or landing.HIGH for takeoff, approach, or landing.

What are the maximum altitude APU What are the maximum altitude APU limitations?limitations?

-700-700 -300/500-300/500 Max Altitude for OperationMax Altitude for Operation 41,000’ 35,000’41,000’ 35,000’ Max Altitude Electric OnlyMax Altitude Electric Only 41,000’ 35,000’41,000’ 35,000’ Max Altitude Bleed OnlyMax Altitude Bleed Only 17,000’17,000’ Max Altitude Bleed Air & ElectricMax Altitude Bleed Air & Electric 10,000’10,000’

What is the limitation if the cargo bay fire What is the limitation if the cargo bay fire smoke and fire suppression system is smoke and fire suppression system is

utilized?utilized?

Aircraft must land withinAircraft must land within 60 minutes60 minutes of of initial discharge of the fire suppression initial discharge of the fire suppression system.system.

What is the engine driven generator What is the engine driven generator limitation on the ground?limitation on the ground?

Does it apply to the (-300/500)?Does it apply to the (-300/500)?

On the ground, limit one generator On the ground, limit one generator operation (engine driven)operation (engine driven) to a to a maximum ofmaximum of 215 amps.215 amps.

(-300/500) N/A(-300/500) N/A

When can the flight crew remove AC When can the flight crew remove AC power from the aircraft?power from the aircraft?

Do not remove AC power from the Do not remove AC power from the aircraft for at leastaircraft for at least 30 seconds30 seconds after after IRS shutdown.IRS shutdown.

What are the three in-flight speedbrake What are the three in-flight speedbrake limitations?limitations?

Do not use speedbrakes in flight below Do not use speedbrakes in flight below 1000 feet AGL.1000 feet AGL.

In-flight, do not extend the speedbrake In-flight, do not extend the speedbrake lever beyond the flight detent.lever beyond the flight detent.

In-flight, do not use speedbrakes unless In-flight, do not use speedbrakes unless flaps are fully retracted.flaps are fully retracted.

What is the alternate flap duty cycle What is the alternate flap duty cycle limitation in-flight?limitation in-flight?

Alternate flap duty cycle in-flight is one Alternate flap duty cycle in-flight is one complete cycle, thencomplete cycle, then 25 minutes25 minutes off. A off. A complete cycle is movement from complete cycle is movement from positionposition 0 to 40 and back to 00 to 40 and back to 0. The . The alternate flaps switch must be in the alternate flaps switch must be in the OFF position forOFF position for 6 seconds6 seconds before before reversing the direction of flap reversing the direction of flap movement. movement.

What is the flap extension pressure What is the flap extension pressure altitude limitation?altitude limitation?

Do not extend flaps aboveDo not extend flaps above 20,000 feet20,000 feet pressure altitude.pressure altitude.

What are the max and min fuel tank What are the max and min fuel tank temperature limitations?temperature limitations?

Max Fuel Tank TemperatureMax Fuel Tank Temperature +49°C+49°C

Min Fuel Tank TemperatureMin Fuel Tank Temperature -37°C -37°C

For fuel distribution, when should the For fuel distribution, when should the main tanks be scheduled to be full?main tanks be scheduled to be full?

Fuel Distribution: Main tanks must be Fuel Distribution: Main tanks must be full if the center tank quantity is full if the center tank quantity is greater than greater than 1000 lbs1000 lbs..

Use center tank to depletion followed Use center tank to depletion followed by wing tank fuel.by wing tank fuel.

When must the fuel crossfeed valve be When must the fuel crossfeed valve be closed?closed?

Does it apply to the (-300/500)?Does it apply to the (-300/500)?

Fuel crossfeed valve must be closed for Fuel crossfeed valve must be closed for takeoff and landing.takeoff and landing.

(-300/500 N/A)(-300/500 N/A)

When must the center tank fuel pump When must the center tank fuel pump switches not be positioned to ON? switches not be positioned to ON?

Unless?Unless?

For ground operation, center tank fuel For ground operation, center tank fuel pump switches must not be positioned to pump switches must not be positioned to ON unless the center tank fuel quantity ON unless the center tank fuel quantity exceeds exceeds 1,000 pounds1,000 pounds, except when , except when defueling or transferring fuel.defueling or transferring fuel.

Center tank fuel pumps must not be ON Center tank fuel pumps must not be ON unless personnel are available on the flight unless personnel are available on the flight deck to monitor deck to monitor low pressurelow pressure lights. lights.

When must the center tank switches be When must the center tank switches be positioned to OFF?positioned to OFF?

Center tank fuel pump switches must be Center tank fuel pump switches must be positioned to OFF when both center tank fuel positioned to OFF when both center tank fuel pump pump low pressurelow pressure lights illuminate. lights illuminate.

Note: The limitation does not change the Note: The limitation does not change the existing normal procedure to turn the center existing normal procedure to turn the center tank fuel pump switches to OFF at the first tank fuel pump switches to OFF at the first indication of indication of low pressurelow pressure from either pump. from either pump.

For the (-700), when must the center tank For the (-700), when must the center tank fuel pumps switches be positioned to fuel pumps switches be positioned to

OFF OFF at all timesat all times??

At all timesAt all times: The center tank fuel : The center tank fuel pumps switches must be positioned pumps switches must be positioned OFF at the first indication of fuel pump OFF at the first indication of fuel pump low pressure.low pressure.

For the (-700), when must both center For the (-700), when must both center tank fuel pump switches be positioned tank fuel pump switches be positioned

OFF during OFF during takeoff & initial climbtakeoff & initial climb??

Takeoff & initial climbTakeoff & initial climb: Both center tank fuel : Both center tank fuel pump switches must be positioned OFF for pump switches must be positioned OFF for takeoff if center tank fuel quantity is less takeoff if center tank fuel quantity is less than than 5000 pounds.5000 pounds. When center tank fuel When center tank fuel quantity is greater than quantity is greater than 2000 lbs,2000 lbs, turn on turn on both center tank fuel pump switches above both center tank fuel pump switches above 10000’10000’ or after reducing the pitch attitude to or after reducing the pitch attitude to accelerate to accelerate to 250 knots or greater.250 knots or greater.

For the (-700), when should the center tank For the (-700), when should the center tank fuel pump switches be positioned ON and fuel pump switches be positioned ON and

back to OFF during back to OFF during climb & cruiseclimb & cruise??

Climb & cruiseClimb & cruise: If greater than : If greater than 2000 lbs2000 lbs of fuel of fuel remain in the center tank, both center tank fuel remain in the center tank, both center tank fuel pump switches should be repositioned ON. Turn pump switches should be repositioned ON. Turn one center fuel pump OFF during one center fuel pump OFF during climb or cruiseclimb or cruise when the center tank fuel quantity reaches when the center tank fuel quantity reaches approximately approximately 2000 lbs.2000 lbs. Open the crossfeed valve Open the crossfeed valve to minimize fuel imbalance.to minimize fuel imbalance.

When the MASTER CAUTION and FUEL system When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining annunciator lights illuminate, turn the remaining center tank fuel pump switch OFF without delay center tank fuel pump switch OFF without delay and close the fuel crossfeed valve.and close the fuel crossfeed valve.

For the (-700), when must the center tank For the (-700), when must the center tank fuel pump switch be turned OFF in the fuel pump switch be turned OFF in the

descentdescent?? DescentDescent: Turn one center fuel pump switch OFF at the beginning : Turn one center fuel pump switch OFF at the beginning

of the descent if less than of the descent if less than 3000 lbs3000 lbs of fuel remain in the center of fuel remain in the center tank. Open the crossfeed valve to minimize fuel imbalance.tank. Open the crossfeed valve to minimize fuel imbalance.

When the MASTER CAUTION and FUEL system annunciator When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining center tank fuel pump switch lights illuminate, turn the remaining center tank fuel pump switch OFF without delay and close the crossfeed valve.OFF without delay and close the crossfeed valve.

If an extended period of level flight is required prior to approach If an extended period of level flight is required prior to approach and landing, i.e., holding, and fuel remains in the center tank, a and landing, i.e., holding, and fuel remains in the center tank, a single center tank fuel pump switch may be repositioned ON if single center tank fuel pump switch may be repositioned ON if both fuel pumps were previously turned OFF. The fuel crossfeed both fuel pumps were previously turned OFF. The fuel crossfeed valve should be opened to prevent fuel imbalance.valve should be opened to prevent fuel imbalance.

At the first indication of pump low pressure, the fuel pump must At the first indication of pump low pressure, the fuel pump must immediately be turned off and the fuel crossfeed valve must be immediately be turned off and the fuel crossfeed valve must be closed. The fuel crossfeed valve must be closed for landing.closed. The fuel crossfeed valve must be closed for landing.

What is the limitation for holding in icing What is the limitation for holding in icing conditions?conditions?

Does it apply to the (-300/500)?Does it apply to the (-300/500)?

Holding in icing conditions with Holding in icing conditions with flaps extended is prohibited.flaps extended is prohibited.

(-300/500 N/A)(-300/500 N/A)

What is the maximum EGT during ground What is the maximum EGT during ground start?start?

Ground Start Ground Start 725°C725°C

What is the minimum duct start pressure? What is the minimum duct start pressure? Does it apply to the (-700)?Does it apply to the (-700)?

Minimum duct start pressure: Minimum duct start pressure:

30 psi—reduce 0.5 psi per 1000 30 psi—reduce 0.5 psi per 1000 feetfeet above sea level. above sea level.

(-700 N/A) (-700 N/A)

What are the two engine idle time What are the two engine idle time limitations prior to shutdown?limitations prior to shutdown?

Operate engines at idle for a Operate engines at idle for a minimum of minimum of one minuteone minute prior to prior to shutdown. shutdown.

When operational conditions permit, When operational conditions permit, engines should idle for engines should idle for 3 minutes3 minutes before shutdown. before shutdown.

When can we use reverse thrust?When can we use reverse thrust?

Reverse thrust is for ground use only.Reverse thrust is for ground use only.

What is the limitation for operation of the What is the limitation for operation of the weather radar?weather radar?

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

In all situationsIn all situations

Maintain aircraft control Maintain aircraft control

Analyze the problem Analyze the problem

Take appropriate action Take appropriate action

Maintain situational awarenessMaintain situational awareness

Cabin Altitude Warning Horn / Cabin Altitude Warning Horn / Abnormal PressurizationAbnormal Pressurization

Oxygen masks & regulators...On/Oxygen masks & regulators...On/100%100%

Crew Communications…...…..Establish Crew Communications…...…..Establish

Aborted Engine StartsAborted Engine Starts

Start Lever Start Lever CutoffCutoff

725° C

Rejected TakeoffRejected Takeoff

Simultaneously:Simultaneously:

Thrust levers………………..…Close Thrust levers………………..…Close

Wheel Brakes…………..….…..Maximum Wheel Brakes…………..….…..Maximum

Without Delay:Without Delay:

Speedbrake Lever………….…UP Speedbrake Lever………….…UP

Thrust Reversers…..….……...MaximumThrust Reversers…..….……...Maximum

Warning Horn – Cabin Altitude or Warning Horn – Cabin Altitude or ConfigurationConfiguration

If an intermittent warning horn sounds in-flight:If an intermittent warning horn sounds in-flight:

Oxygen Masks & Regulators.….ON/Oxygen Masks & Regulators.….ON/100%100%Crew Communications………….EstablishCrew Communications………….EstablishAccomplish the Cabin Altitude Warning Accomplish the Cabin Altitude Warning Horn/Abnormal Pressurization Checklist Horn/Abnormal Pressurization Checklist (QRH Page A-15)(QRH Page A-15)If an intermittent warning horn sounds on the ground:If an intermittent warning horn sounds on the ground:

Assure Proper Takeoff ConfigurationAssure Proper Takeoff ConfigurationIf a steady warning horn sounds in-flight:If a steady warning horn sounds in-flight:

Assure Proper Landing ConfigurationAssure Proper Landing Configuration

Dual Engine FailureDual Engine Failure

Start Switches………………….FLT Start Switches………………….FLT

Start Levers…………………….Cutoff Start Levers…………………….Cutoff

EGT DecreasingEGT Decreasing

Start Levers…………………….IdleStart Levers…………………….IdleIf EGT Exceeds If EGT Exceeds 950°C (-300/500: 930°C)950°C (-300/500: 930°C)

Repeat above stepsRepeat above steps

Smoke/Fire/Fumes In the CockpitSmoke/Fire/Fumes In the CockpitCabin/Lavatory FireCabin/Lavatory Fire

Oxygen Masks & Regulators.........ON/Oxygen Masks & Regulators.........ON/100%100%

Smoke Goggles (if required) ..…...ONSmoke Goggles (if required) ..…...ON

Runaway StabilizerRunaway Stabilizer

Control Column……………...……..Hold firmly Control Column……………...……..Hold firmly

Autopilot (if engaged)…..….....…..Disengage Autopilot (if engaged)…..….....…..Disengage

If Runaway Stabilizer Continues:If Runaway Stabilizer Continues:

Stabilizer Trim Cutout Switches...Cutout Stabilizer Trim Cutout Switches...Cutout

If Runaway Stabilizer Continues:If Runaway Stabilizer Continues:

Stabilizer Trim Wheel………..........Grasp & holdStabilizer Trim Wheel………..........Grasp & hold

Engine Limit/Surge/StallEngine Limit/Surge/Stall

Thrust Lever............Retard to maintain limitsThrust Lever............Retard to maintain limits

If Indications Remain Abnormal Or EGT Continues To Increase:If Indications Remain Abnormal Or EGT Continues To Increase:

Start lever…….....…CutoffStart lever…….....…Cutoff

Note: minimum altitude of 400’ AGL, and airspeed are acceptableNote: minimum altitude of 400’ AGL, and airspeed are acceptable

Uncommanded Rudder/Yaw/RollUncommanded Rudder/Yaw/Rollor (-300/500) Spindle Failureor (-300/500) Spindle Failure

Autopilot (if engaged)….....DisengageAutopilot (if engaged)….....DisengageMaintain control of the aircraft with all available Maintain control of the aircraft with all available flight controls. If roll is uncontrollable, flight controls. If roll is uncontrollable, immediately reduce pitch/AOA and increase immediately reduce pitch/AOA and increase airspeed. Do not attempt to maintain altitude airspeed. Do not attempt to maintain altitude until control is recovered. until control is recovered. Thrust……………………Verify symmetricalThrust……………………Verify symmetrical(-300/500) If spindle failure (flaps are extended, (-300/500) If spindle failure (flaps are extended, no asymmetry indicated on the flap gauge, no asymmetry indicated on the flap gauge, rudder pedals are normal, may be accompanied rudder pedals are normal, may be accompanied by a loud bang): Go-Around...............Initiateby a loud bang): Go-Around...............Initiate