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20 Cards in this Set
- Front
- Back
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APU FIRE |
1 APU fire switch … Confirm … Pull, rotate to the stop and hold for 1 second 2 APU switch … OFF
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ABORTED ENGINE START |
1 Engine start lever (affected engine) … CUTOFF |
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TAKEOFF CONFIGURATION |
1 Assure correct airplane takeoff configurarion |
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AIRSPEED UNRELIABLE |
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* 80% N1 Flaps up … 4* 75% N1 |
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CABIN ALTITUDE WARNING |
1 Don oxygen masks and set regulators to 100% 2 Establish crew communications 3 Pressurization mode selector … MAN 4 Outflow valve switch … Hold in CLOSE until the outflow VALVE indication shows fully closed 5 If cabin altitud is uncontrollable: Passengers signs … ON PASS OXYGEN switch … ON Go to the Emergency Descent Checklist |
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EMERGENCY DESCENT |
1 Announce the emergency descent 2 Passengers signs … ON 3 Without delay descend to the lowest safe altitude or 10.000ft, whichever is higher 4 Thrust levers (both) … Reduce thrust to minimum or as needed for anti-ice 6 Speedbrake … FLIGHT DETENT 7 Set taget speed to Mmo/Vmo |
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ENGINE FIRE or Engine Severe Damage or Separation |
1 Autothrottle (if engaged) … disengage 2 Thrust lever (affected engine) … Confirm … Close 3 Engine start lever (affected engine) … Confirm … CUTOFF 4 Engine fire switch (affected engine) … Confirm … Pull 5 If the engine fire switch or ENG OVERHEAT light is illuminated: Engine fire switch (affected engine) … Rotate to the stop and hold for 1 second (verify bottle discharged illuminated) |
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ENGINE LIMIT or SURGE or STALL |
1 Autothrottle (if engaged) … Disengage 2 Thrust lever (affected engine) … Confirm … Retard until engine indications stay within limits or the thrust lever is closed |
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ENGINE OVERHEAT |
1 Autothrottle (if engaged) … Disengage 2 Thrust lever (affected engine) … Confirm … Close 3 If the ENG OVERHEAT light stays illuminated: Go to the ENGINE FIRE NNC |
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LANDING CONFIGURATION |
1 Assure correct airplane landing configuration |
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TAKEOFF CONFIGURATION |
1 Assure correct airplane takeoff configuration |
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LOSS OF THRUST ON BOTH ENGINES |
1 ENGINE START switches (both) … FLT 2 Engine start levers (both) … CUTOFF 3 When EGT decreases: Engine start levers (both) … IDLE detent 4 If EGT reaches a redline or there is no increase in EGT within 30 seconds: Engine start lever (affected engine) … Confirm … CUTOFF, then IDLE detent If EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed |
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RUNAWAY STABILIZER |
1 Control column … Hold firmly 2 Autopilot (if engaged) …Disengage 3 Autothrottle (if engaged) … disengage 4 Control column and thrust levers … Control airplane 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 AUTOTHROTTLE 7 Ig the runaway continues after the autopilot is disengaged: STAB TRIM cutout swtiches (both) … CUTOUT If the runaway continues: Stabilizer trim wheel … Grasp and hold |
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MLW B737-800 |
66.360 Kgs |
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MLW B737-700 |
58.059 Kgs |
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MLW LV-CTC LV-CTB LV-FQB LV-FQC |
65.317 Kgs |
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MAXIMUM CABIN DIFFERENTIAL PRESSURE (relief valves) |
9.1psi |
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SELECTED FLT ALT / DIFFERENTIAL PRESSURE LIMIT |
At or below 28000ft = 7.45psid 28000ft to 37000ft = 7.80psid Above 37000ft = 8.35psid |
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ENGINE OUT DRIFTDOWN PROCEDURE |
1 Rudder trim ... Controlar 2 Autothrottle ... Disconnect 3 MCT ... Set 4 Altitud hold ... Set 5 Driftdown Altitud ... Set 6 Driftdown Speed ... Set 7 When approaching driftdown speed ... LVL CHG Set |
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SEVERE TURBULENCE PROCEDURE |
1 Yaw damper ... ON 2 Autothrottle ... Disengage 3 Autopilot ... CWS (Check CWS pitch & roll) 4 ENG Start Swtiches ... FLT 5 Thrust ... Set Climb: 280knots / .76M whichever is lower Cruise: FMC recommended thrust settings. Descent: .76M / 280knots / 250knots whichever is lower. If sev turb is encountered below 15.000ft and the airplane gross weight is less than the MLW, the airplane may be slowed to 250knots. *If an approach must be made into an area of severe turbulence, delay flap extension as long as possible. |
