SWA MEMORY ITEMS

1. SWA MEMORY ITEMS

2. What are the two memory items for resetting tripped circuit breakers? • A tripped circuit breaker may only be reset once. Allow approximately 2 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 the flight. • Flight crews will not reset tripped fuel quantity indicator, fuel pump, or fuel pump control circuit breakers.

3. With regards to TCAS, what are the flight crew responses? • Flight crews must immediately respond to TCAS information (both TA’s and RA’s) by using the TCAS (Traffic Avoidance) guidelines located in the “Non-normal Operations: Maneuvers and Profiles.” • Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS II Resolution Advisory (RA).

4. What are the wind component limitations?

5. What are the maximum operating pressure altitudes? • (-700)41,000 feet • (-300/500)37,000 feet

6. What is the Bleed and PACK limitation for takeoff, approach, and landing? • With engine bleed air switches ON; do not operate the air conditioning packs in HIGH for takeoff, approach, or landing.

7. What are the maximum altitude APU limitations? -700-300/500 • Max Altitude for Operation41,000’ 35,000’ • Max Altitude Electric Only41,000’ 35,000’ • Max Altitude Bleed Only17,000’ • Max Altitude Bleed Air & Electric10,000’

8. What is the limitation if the cargo bay fire smoke and fire suppression system is utilized? • Aircraft must land within60 minutesof initial discharge of the fire suppression system.

9. What is the engine driven generator limitation on the ground?Does it apply to the (-300/500)? • On the ground, limit one generator operation (engine driven)to a maximum of215 amps. • (-300/500) N/A

10. When can the flight crew remove AC power from the aircraft? • Do not remove AC power from the aircraft for at least30 secondsafter IRS shutdown.

11. What are the three in-flight speedbrake limitations? • 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 unless flaps are fully retracted.

12. What is the alternate flap duty cycle limitation in-flight? • Alternate flap duty cycle in-flight is one complete cycle, then25 minutesoff. A complete cycle is movement from position0 to 40 and back to 0. The alternate flaps switch must be in the OFF position for6 secondsbefore reversing the direction of flap movement.

13. What is the flap extension pressure altitude limitation? • Do not extend flaps above20,000 feetpressure altitude.

14. What are the max and min fuel tank temperature limitations? • Max Fuel Tank Temperature+49°C • Min Fuel Tank Temperature-37°C

15. For fuel distribution, when should the main tanks be scheduled to be full? • Fuel Distribution: Main tanks must be full if the center tank quantity is greater than 1000 lbs. • Use center tank to depletion followed by wing tank fuel.

16. When must the fuel crossfeed valve be closed?Does it apply to the (-300/500)? • Fuel crossfeed valve must be closed for takeoff and landing. • (-300/500 N/A)

17. When must the center tank fuel pump switches not be positioned to ON? Unless? • For ground operation, center tank fuel pump switches must not be positioned to ON unless the center tank fuel quantity exceeds 1,000 pounds, except when defueling or transferring fuel. • Center tank fuel pumps must not be ON unless personnel are available on the flight deck to monitor low pressure lights.

18. When must the center tank switches be positioned to OFF? • Center tank fuel pump switches must be positioned to OFF when both center tank fuel pump low pressure lights illuminate. • Note: The limitation does not change the existing normal procedure to turn the center tank fuel pump switches to OFF at the first indication of low pressure from either pump.

19. For the (-700), when must the center tank fuel pumps switches be positioned to OFF at all times? • At all times: The center tank fuel pumps switches must be positioned OFF at the first indication of fuel pump low pressure.

20. For the (-700), when must both center tank fuel pump switches be positioned OFF during takeoff & initial climb? • Takeoff & initial climb: Both center tank fuel pump switches must be positioned OFF for takeoff if center tank fuel quantity is less than 5000 pounds. When center tank fuel quantity is greater than 2000 lbs, turn on both center tank fuel pump switches above 10000’ or after reducing the pitch attitude to accelerate to 250 knots or greater.

21. For the (-700), when should the center tank fuel pump switches be positioned ON and back to OFF during climb & cruise? • Climb & cruise: If greater than 2000 lbs of fuel remain in the center tank, both center tank fuel pump switches should be repositioned ON. Turn one center fuel pump OFF during climb or cruise when the center tank fuel quantity reaches approximately 2000 lbs. Open the crossfeed valve to minimize fuel imbalance. • When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining center tank fuel pump switch OFF without delay and close the fuel crossfeed valve.

22. For the (-700), when must the center tank fuel pump switch be turned OFF in the descent? • Descent: Turn one center fuel pump switch OFF at the beginning of the descent if less than 3000 lbs of fuel remain in the center tank. Open the crossfeed valve to minimize fuel imbalance. • When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining center tank fuel pump switch OFF without delay and close the crossfeed valve. • 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 single center tank fuel pump switch may be repositioned ON if both fuel pumps were previously turned OFF. The fuel crossfeed valve should be opened to prevent fuel imbalance. • At the first indication of pump low pressure, the fuel pump must immediately be turned off and the fuel crossfeed valve must be closed. The fuel crossfeed valve must be closed for landing.

23. What is the limitation for holding in icing conditions?Does it apply to the (-300/500)? • Holding in icing conditions with flaps extended is prohibited. • (-300/500 N/A)

24. What is the maximum EGT during ground start? • Ground Start 725°C

25. What is the minimum duct start pressure? Does it apply to the (-700)? • Minimum duct start pressure: 30 psi—reduce 0.5 psi per 1000 feet above sea level. • (-700 N/A)

26. What are the two engine idle time limitations prior to shutdown? • Operate engines at idle for a minimum of one minute prior to shutdown. • When operational conditions permit, engines should idle for 3 minutes before shutdown.

27. When can we use reverse thrust? • Reverse thrust is for ground use only.

28. What is the limitation for operation of the weather radar? • Do not operate the weather radar during fueling, near fuel spills, or people.

29. In all situations • Maintain aircraft control • Analyze the problem • Take appropriate action • Maintain situational awareness

30. Cabin Altitude Warning Horn / Abnormal Pressurization • Oxygen masks & regulators...On/100% • Crew Communications…...…..Establish

31. Aborted Engine Starts • Start Lever Cutoff 725° C

32. Rejected Takeoff • Simultaneously: • Thrust levers………………..…Close • Wheel Brakes…………..….…..Maximum • Without Delay: • Speedbrake Lever………….…UP • Thrust Reversers…..….……...Maximum

33. Warning Horn – Cabin Altitude or Configuration • If an intermittent warning horn sounds in-flight: • Oxygen Masks & Regulators.….ON/100% • Crew Communications………….Establish • Accomplish the Cabin Altitude Warning Horn/Abnormal Pressurization Checklist (QRH Page A-15) • If an intermittent warning horn sounds on the ground: • Assure Proper Takeoff Configuration • If a steady warning horn sounds in-flight: • Assure Proper Landing Configuration

34. Dual Engine Failure • Start Switches………………….FLT • Start Levers…………………….Cutoff • EGT Decreasing • Start Levers…………………….Idle • If EGT Exceeds 950°C (-300/500: 930°C) • Repeat above steps

35. Smoke/Fire/Fumes In the CockpitCabin/Lavatory Fire • Oxygen Masks & Regulators.........ON/100% • Smoke Goggles (if required) ..…...ON

36. Runaway Stabilizer • Control Column……………...……..Hold firmly • Autopilot (if engaged)…..….....…..Disengage • If Runaway Stabilizer Continues: • Stabilizer Trim Cutout Switches...Cutout • If Runaway Stabilizer Continues: • Stabilizer Trim Wheel………..........Grasp & hold

37. Engine Limit/Surge/Stall • Thrust Lever............Retard to maintain limits • If Indications Remain Abnormal Or EGT Continues To Increase: • Start lever…….....…Cutoff • Note: minimum altitude of 400’ AGL, and airspeed are acceptable

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