jeonbyeongchan (25)in #b737 • 6 years ago • NoneHigh Engine VibrationP6-2A Transfer Bus2 - 115v ac Condition : Accomplish this NNC only when engine vibrations indicate above 4.0 units…jeonbyeongchan (25)in #b737 • 6 years ago • NoneFMC FAIL(review) in GUMP6-1D P18-2A Transfer Bus 1 Sect 1 - 115v ac Standby Bus Sect 1 - 115v ac (as wired) Transfer Bus 2 Sect 2 - 115v…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine Ignition InoperativeP6-2D (left) P18-2A (right) Transfer Bus 1 Sect 1/2 - 115v ac (left) Standby Bus Sect 1/2 - 115v ac (right) On…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine Limit or Surge or StallLIMIT Condition : LIMIT refers to N1, N2 or EGT approaching or exceeding its respective limits. However, if the ENG…jeonbyeongchan (25)in #b737 • 6 years ago • NonePACK / PACK TRIP OFFP6-4A, Temp at ACM Compressor Oulet > 199 degrees C / 390 degrees F Temp at ACM Turbine Inlet > 99 degrees C…jeonbyeongchan (25)in #b737 • 6 years ago • NoneALL Flap Up LandingFCTM 8.x [Leading Edge or Trailing Edge Device Malfunctions] Approach Review the approach chart : Published…jeonbyeongchan (25)in #b737 • 6 years ago • NoneTail StrikeTypical tail clearance during takeoff is between 50 and 75 cm / 20 and 30 inches. This clearance increases with flap…jeonbyeongchan (25)in #b737 • 6 years ago • NoneMANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM BFCTM 8.x [Hydraulic System(s) Inoperative - Landing] X with one or both hydraulic system fluid quantities not zero…jeonbyeongchan (25)in #b737 • 6 years ago • NoneLOSS OF BOTH ENGINE DRIVEN GENERATORSMake sure you are not dealing with a single or dual engine failure! Advance thrust levers and verify engine response.…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine In-Flight StartNote : An engine in-flight start is not allowed if %N1 or %N2 shows zero rpm There in no minimum oil quantity…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine Fuel LeakAccording to the NNC an increase in fuel imbalance of 230 kg / 500 lbs or more in 30 minutes should be considered an…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEMERGENCY DESCENTNNC 0.x [Emergency Descent] PRIOR DESCENT - Advise ATC about rapid descent - Advise cabin crew using company SOP…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine Bird Strike! typical indications for an engine bird strike are audible thuds on the airframe, increase in engine EGT, engine…jeonbyeongchan (25)in #b737 • 6 years ago • NoneAPU FIREPulling the APU Fire Switch : closes the APU Fuel SOV closes the APU Bleed Air Valve trips the APU GCR and…jeonbyeongchan (25)in #b737 • 6 years ago • NoneCABIN ALTITUDE WARNING or Rapid DepressurizationRAPID DECOMPRESSION outflow valve malfunction door operning structural damage (e.g. bomb explosion)…jeonbyeongchan (25)in #b737 • 6 years ago • NoneAUTO FAIL/UNSCHEDULED-PRESSURIZATION CHANGEAUTO FAIL or Unscheduled Pressurization Change P6-4F Loss of DC power on DC BUS 1/2 for > 3" Rate of cabin…jeonbyeongchan (25)in #b737 • 6 years ago • NoneAIRSPEED UNRELIABLEThe following events may cause the air data to become invalid: pitot/static system blocked by protective covers…jeonbyeongchan (25)in #b737 • 6 years ago • NonePARTIAL OR GEAR UP LANDINGFCTM 8.x [Partial or Gear Up Landing] - Do not spend too much time trying to clear a gear problem and meanwhile…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEngine High Oil TemperatureThrust lever (affected engine) Retard slowly Decreasing thrust may lower oil temperature by reducing the amount of…jeonbyeongchan (25)in #b737 • 6 years ago • NoneEEC ALTERNATE MODEEngine %N2 > 56% AND EEC selected ON AND Loss of signal from either DEU OR AND Invalid Pt signal from ADIRU (*)…