
b737 Tag Posts Index
Explore on-chain topics from the Hive blockchain.
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3 great photos in a day:)
Hi everybody who loves planes:)Started with Qantas for takeoff picture. And here is the De Havilland Canada approacing for landing! and the last is B737-800 landing
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The Royal Boeing Business Jet - Worth $100 Million
The Most Luxurious Boeing Business Jet - B737, Royal Jet owns this. The range of this BBJ can fly up to 10 1/2 hours. So from Abu Dhabi it can go all the way to
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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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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
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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
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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
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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
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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
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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
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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,
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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
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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,
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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
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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
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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
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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 squib
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CABIN ALTITUDE WARNING or Rapid Depressurization
RAPID DECOMPRESSION outflow valve malfunction door operning structural damage (e.g. bomb explosion) SLOW DECOMPRESSION outflow valve malfunction presurization controller
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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
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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
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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
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