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WKBC~sky~ (25)Hivebuzz level badge

428 followers95 posts1604 following0 HP
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Joined April 2018 Active 7 years ago

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  • jeonbyeongchan (25)in #b737 • 7 years ago
    featured

    High Engine Vibration

    P6-2A Transfer Bus2 - 115v ac Condition : Accomplish this NNC only when engine vibrations indicate above 4.0 units and airframe vibrations occur (to exclude a faulty…
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    • jeonbyeongchan (25)in #b737 • 7 years ago
      featured

      FMC FAIL(review) in GUM

      P6-1D 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 or MENU…
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      • jeonbyeongchan (25)in #b737 • 7 years ago
        featured

        Engine Ignition Inoperative

        P6-2D (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. As a result…
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        • jeonbyeongchan (25)in #b737 • 7 years ago
          featured

          Engine Limit or Surge or Stall

          LIMIT 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 illuminates, the…
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          • jeonbyeongchan (25)in #b737 • 7 years ago
            featured

            PACK / PACK TRIP OFF

            P6-4A, 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 /…
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            • jeonbyeongchan (25)in #b737 • 7 years ago
              featured

              ALL Flap Up Landing

              FCTM 8.x [Leading Edge or Trailing Edge Device Malfunctions] Approach Review the approach chart : Published procedure turns and radar vectors that are executed at a speed…
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              • jeonbyeongchan (25)in #b737 • 7 years ago
                featured

                Tail Strike

                Typical 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 takeoff with low gross…
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                • jeonbyeongchan (25)in #b737 • 7 years ago
                  featured

                  MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B

                  FCTM 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 E&E, so these…
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                  • jeonbyeongchan (25)in #b737 • 7 years ago
                    featured

                    LOSS OF BOTH ENGINE DRIVEN GENERATORS

                    Make 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 MCP settings -…
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                    • jeonbyeongchan (25)in #b737 • 7 years ago
                      featured

                      Engine In-Flight Start

                      Note : 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, after engine…
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                      • jeonbyeongchan (25)in #b737 • 7 years ago
                        featured

                        Engine Fuel Leak

                        According 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 that not every…
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                        • jeonbyeongchan (25)in #b737 • 7 years ago
                          featured

                          EMERGENCY DESCENT

                          NNC 0.x [Emergency Descent] PRIOR DESCENT - Advise ATC about rapid descent - Advise cabin crew using company SOP and call-outs DURING DESCENT - confirm heading and altitude…
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                          • jeonbyeongchan (25)in #b737 • 7 years ago
                            featured

                            Engine 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 from the air…
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                            • jeonbyeongchan (25)in #b737 • 7 years ago
                              featured

                              APU FIRE

                              Pulling 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 discharge…
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                              • jeonbyeongchan (25)in #b737 • 7 years ago
                                featured

                                CABIN ALTITUDE WARNING or Rapid Depressurization

                                RAPID DECOMPRESSION outflow valve malfunction door operning structural damage (e.g. bomb explosion) SLOW DECOMPRESSION outflow valve malfunction…
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                                • jeonbyeongchan (25)in #b737 • 7 years ago
                                  featured

                                  AUTO FAIL/UNSCHEDULED-PRESSURIZATION CHANGE

                                  AUTO 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 15,800…
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                                  • jeonbyeongchan (25)in #b737 • 7 years ago
                                    featured

                                    AIRSPEED UNRELIABLE

                                    The following events may cause the air data to become invalid: pitot/static system blocked by protective covers installed for overnight stop pitot/static system taped for…
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                                    • jeonbyeongchan (25)in #b737 • 7 years ago
                                      featured

                                      PARTIAL OR GEAR UP LANDING

                                      FCTM 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 suitable airport…
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                                      • jeonbyeongchan (25)in #b737 • 7 years ago
                                        featured

                                        Engine High Oil Temperature

                                        Thrust lever (affected engine) Retard slowly Decreasing thrust may lower oil temperature by reducing the amount of heat generated by the engine. However, increasing thrust may…
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                                        • jeonbyeongchan (25)in #b737 • 7 years ago
                                          featured

                                          EEC ALTERNATE MODE

                                          Engine %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…
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