WKBC~sky~ (@jeonbyeongchan) - Honouree

WKBC~sky~

@jeonbyeongchan 23

about 8 years ago

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

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@jeonbyeongchan 23

about 8 years ago

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) Cond

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@jeonbyeongchan 23

about 8 years ago

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 power

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@jeonbyeongchan 23

about 8 years ago

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

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@jeonbyeongchan 23

about 8 years ago

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

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@jeonbyeongchan 23

about 8 years ago

ALL Flap Up Landing FCTM 8.x Leading Edge or Trailing Edge Device Malfunctions Approach Review the approach chart : Published procedure turns and radar vecto

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@jeonbyeongchan 23

about 8 years ago

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

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@jeonbyeongchan 23

about 8 years ago

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 E

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@jeonbyeongchan 23

about 8 years ago

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

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@jeonbyeongchan 23

about 8 years ago

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-

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@jeonbyeongchan 23

about 8 years ago

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. Howev

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@jeonbyeongchan 23

about 8 years ago

EMERGENCY DESCENT NNC 0.x Emergency Descent PRIOR DESCENT - Advise ATC about rapid descent - Advise cabin crew using compa

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@jeonbyeongchan 23

about 8 years ago

Engine Bird Strike ! typical indications for an engine bird strike are audible thuds on the airframe, increase in engine EGT, engine surge, engine vibrations a

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@jeonbyeongchan 23

about 8 years ago

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 AP

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@jeonbyeongchan 23

about 8 years ago

CABIN ALTITUDE WARNING or Rapid Depressurization RAPID DECOMPRESSION outflow valve malfunction door operning structural damage (e.g. bomb explosion) SLOW DECOMPRESSION

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