jeonbyeongchan(25)•in #b737•2674 days agoHigh Engine VibrationP6-2A Transfer Bus2 - 115v ac Condition : Accomplish this NNC only when engine vibrations indicate above 4.0 units and airframe vibrations occur (to exclude a f...2$0.00jeonbyeongchan(25)•in b737•2674 days agoHigh Engine VibrationP6-2A Transfer Bus2 - 115v ac Condition : Accomplish this NNC only when engine vibrations indicate above 4.0 units and airframe vibrations occur (to exclude a f...2$0.00
jeonbyeongchan(25)•in #b737•2676 days agoFMC 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 ac (optional FMC 2) Condition : “FMC” message ...20$0.00jeonbyeongchan(25)•in b737•2676 days agoFMC 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 ac (optional FMC 2) Condition : “FMC” message ...20$0.00
jeonbyeongchan(25)•in #b737•2676 days agoEngine 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 GND Left ignition is powered by Transfer Bus 1. A...0$0.00jeonbyeongchan(25)•in b737•2676 days agoEngine 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 GND Left ignition is powered by Transfer Bus 1. A...0$0.00
jeonbyeongchan(25)•in #b737•2677 days agoEngine Limit or Surge or StallLIMIT Condition : LIMIT refers to N1, N2 or EGT approaching or exceeding its respective limits. However, if the ENG OVERHEAT amber light or ENGINE FIRE switch i...0$0.00jeonbyeongchan(25)•in b737•2677 days agoEngine Limit or Surge or StallLIMIT Condition : LIMIT refers to N1, N2 or EGT approaching or exceeding its respective limits. However, if the ENG OVERHEAT amber light or ENGINE FIRE switch i...0$0.00
jeonbyeongchan(25)•in #b737•2685 days agoPACK / PACK TRIP OFFP6-4A, Temp at ACM Compressor Oulet > 199 degrees C / 390 degrees F Temp at ACM Turbine Inlet > 99 degrees C / 210 degrees F Temp in Supply Duct > 121 degrees C...0$0.00jeonbyeongchan(25)•in b737•2685 days agoPACK / PACK TRIP OFFP6-4A, Temp at ACM Compressor Oulet > 199 degrees C / 390 degrees F Temp at ACM Turbine Inlet > 99 degrees C / 210 degrees F Temp in Supply Duct > 121 degrees C...0$0.00
jeonbyeongchan(25)•in #b737•2690 days agoALL Flap Up LandingFCTM 8.x [Leading Edge or Trailing Edge Device Malfunctions] Approach Review the approach chart : Published procedure turns and radar vectors that are executed ...2$0.00jeonbyeongchan(25)•in b737•2690 days agoALL Flap Up LandingFCTM 8.x [Leading Edge or Trailing Edge Device Malfunctions] Approach Review the approach chart : Published procedure turns and radar vectors that are executed ...2$0.00
jeonbyeongchan(25)•in #b737•2691 days agoTail StrikeTypical tail clearance during takeoff is between 50 and 75 cm / 20 and 30 inches. This clearance increases with flap setting. Consider using Flaps 15 for takeof...0$0.00jeonbyeongchan(25)•in b737•2691 days agoTail StrikeTypical tail clearance during takeoff is between 50 and 75 cm / 20 and 30 inches. This clearance increases with flap setting. Consider using Flaps 15 for takeof...0$0.00
jeonbyeongchan(25)•in #b737•2691 days agoMANUAL 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, verify the EDP. The EMDP are located in the ...0$0.00jeonbyeongchan(25)•in b737•2691 days agoMANUAL 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, verify the EDP. The EMDP are located in the ...0$0.00
jeonbyeongchan(25)•in #b737•2692 days agoLOSS OF BOTH ENGINE DRIVEN GENERATORSMake sure you are not dealing with a single or dual engine failure! Advance thrust levers and verify engine response. ENG FAIL should not be displayed. Verify M...10$0.00jeonbyeongchan(25)•in b737•2692 days agoLOSS OF BOTH ENGINE DRIVEN GENERATORSMake sure you are not dealing with a single or dual engine failure! Advance thrust levers and verify engine response. ENG FAIL should not be displayed. Verify M...10$0.00
jeonbyeongchan(25)•in #b737•2699 days agoEngine In-Flight StartNote : An engine in-flight start is not allowed if %N1 or %N2 shows zero rpm There in no minimum oil quantity requirement for an engine in-flight start. However...10$0.00jeonbyeongchan(25)•in b737•2699 days agoEngine In-Flight StartNote : An engine in-flight start is not allowed if %N1 or %N2 shows zero rpm There in no minimum oil quantity requirement for an engine in-flight start. However...10$0.00
jeonbyeongchan(25)•in #b737•2700 days agoEngine Fuel LeakAccording to the NNC an increase in fuel imbalance of 230 kg / 500 lbs or more in 30 minutes should be considered an engine fuel leak. However, bear in mind tha...0$0.00jeonbyeongchan(25)•in b737•2700 days agoEngine Fuel LeakAccording to the NNC an increase in fuel imbalance of 230 kg / 500 lbs or more in 30 minutes should be considered an engine fuel leak. However, bear in mind tha...0$0.00
jeonbyeongchan(25)•in #b737•2700 days agoEMERGENCY DESCENTNNC 0.x [Emergency Descent] PRIOR DESCENT - Advise ATC about rapid descent - Advise cabin crew using company SOP and call-outs DURING DESCENT - confirm heading ...0$0.00jeonbyeongchan(25)•in b737•2700 days agoEMERGENCY DESCENTNNC 0.x [Emergency Descent] PRIOR DESCENT - Advise ATC about rapid descent - Advise cabin crew using company SOP and call-outs DURING DESCENT - confirm heading ...0$0.00
jeonbyeongchan(25)•in #b737•2703 days agoEngine Bird Strike! typical indications for an engine bird strike are audible thuds on the airframe, increase in engine EGT, engine surge, engine vibrations and unpleasant odors ...0$0.00jeonbyeongchan(25)•in b737•2703 days agoEngine Bird Strike! typical indications for an engine bird strike are audible thuds on the airframe, increase in engine EGT, engine surge, engine vibrations and unpleasant odors ...0$0.00
jeonbyeongchan(25)•in #b737•2703 days agoAPU FIREPulling the APU Fire Switch : - closes the APU Fuel SOV - closes the APU Bleed Air Valve - trips the APU GCR and GCB - closes the APU inlet Door - arms the disc...0$0.00jeonbyeongchan(25)•in b737•2703 days agoAPU FIREPulling the APU Fire Switch : - closes the APU Fuel SOV - closes the APU Bleed Air Valve - trips the APU GCR and GCB - closes the APU inlet Door - arms the disc...0$0.00
jeonbyeongchan(25)•in #b737•2703 days agoCABIN ALTITUDE WARNING or Rapid DepressurizationRAPID DECOMPRESSION - outflow valve malfunction - door operning - structural damage (e.g. bomb explosion) SLOW DECOMPRESSION - outflow valve malfunction - presu...12$0.00jeonbyeongchan(25)•in b737•2703 days agoCABIN ALTITUDE WARNING or Rapid DepressurizationRAPID DECOMPRESSION - outflow valve malfunction - door operning - structural damage (e.g. bomb explosion) SLOW DECOMPRESSION - outflow valve malfunction - presu...12$0.00
jeonbyeongchan(25)•in #b737•2705 days agoAUTO 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 pressure change > 2,00 fpm SLE Cabin altitude above 1...0$0.00jeonbyeongchan(25)•in b737•2705 days agoAUTO 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 pressure change > 2,00 fpm SLE Cabin altitude above 1...0$0.00
jeonbyeongchan(25)•in #b737•2706 days agoAIRSPEED UNRELIABLEThe following events may cause the air data to become invalid: - pitot/static system blocked by protective covers installed for overnight stop - pitot/static sy...10$0.00jeonbyeongchan(25)•in b737•2706 days agoAIRSPEED UNRELIABLEThe following events may cause the air data to become invalid: - pitot/static system blocked by protective covers installed for overnight stop - pitot/static sy...10$0.00
jeonbyeongchan(25)•in #b737•2708 days agoPARTIAL 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 reducing the possibility of diverting to a more ...0$0.00jeonbyeongchan(25)•in b737•2708 days agoPARTIAL 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 reducing the possibility of diverting to a more ...0$0.00
jeonbyeongchan(25)•in #b737•2739 days agoEngine High Oil TemperatureThrust lever (affected engine) Retard slowly Decreasing thrust may lower oil temperature by reducing the amount of heat generated by the engine. However, increa...0$0.00jeonbyeongchan(25)•in b737•2739 days agoEngine High Oil TemperatureThrust lever (affected engine) Retard slowly Decreasing thrust may lower oil temperature by reducing the amount of heat generated by the engine. However, increa...0$0.00
jeonbyeongchan(25)•in #b737•2744 days agoEEC ALTERNATE MODEEngine %N2 > 56% AND EEC selected ON AND Loss of signal from either DEU OR AND Invalid Pt signal from ADIRU () -> soft 15" delay. Engine %N2 > 56 % AND EEC not ...0$0.00jeonbyeongchan(25)•in b737•2744 days agoEEC ALTERNATE MODEEngine %N2 > 56% AND EEC selected ON AND Loss of signal from either DEU OR AND Invalid Pt signal from ADIRU () -> soft 15" delay. Engine %N2 > 56 % AND EEC not ...0$0.00
