B737NG Aircraft general

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Pilot Type Rating Overview.

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B737NG Aircraft general

  1. 1. B 737 NG Ground School. See the aircraft study guide at www.theorycentre.comThe information contained here is for training purposes only. It is of a general nature it isunamended and does not relate to any individual aircraft. The FCOM must be consulted forup to date information on any particular aircraft.
  2. 2. B737NGAircraft General
  3. 3. COCKPIT DOOR.As seen From the Passenger cabin
  4. 4. Flight Deck DoorThe flight deck door meets requirements forresistance to ballistic penetration andintruder entrance. The door opens into thepassenger cabin. When closed, the doorlocks when electrical power is available andunlocks when electrical power is removed. Aviewing lens in the door allows observationof the passenger cabin.The door can be manually opened from theflight deck by turning the door handle.The door incorporates a deadbolt with a keylock on the passenger cabin side.Rotating both concentric deadbolt levers tothe locked (horizontal) positionprevents the passenger cabin key fromunlocking the door. Rotating only theforward deadbolt lever to locked allows thekey to unlock the door.
  5. 5. The flight deck access system consists of anemergency access panel, chime module, threeposition Door Lock selector, two indicator lights,and an Access System switch. The emergencyaccess panel includes a six button keypad forentering the numeric emergency access codealong with red, amber, and green lights. The redlight illuminates to indicate the door is locked.When the correct emergency access code isentered, the amber light illuminates. The greenlight illuminates to indicate the door is unlocked.
  6. 6. Two indicator lights and a three position Door Lock selector arelocated on the aisle stand. Illumination of the amber LOCK FAIL lightindicates the door lock has failed or the Access System switch is in theOFF position.The emergency access code is used to gain access to the flight deckin case of pilot incapacitation. A flight deck chime and illumination ofthe amber AUTO UNLK light indicates the correct emergency accesscode has been entered and the door is programmed to unlock after atime delay. Selecting the DENY position on the Door Lock selectordenies entry and prevents further keypad entry for several minutes. Toallow entry, the selector is turned to the UNLKD position which unlocksthe door while held in that position. If the emergency access code isentered and the pilot takes no action, the door unlocks after expirationof the time delay. Before the door unlocks, the chime soundscontinuously and the AUTO UNLK light flashes.
  7. 7. The door incorporates two pressuresensors that unlock the decompressionpanels in the event pressurization is lost.The decompression panels have manualrelease pins. Pulling the pins frees thepanels allowing egress in the event thedoor is jammed. Decompression panels manually unlocked.
  8. 8. WELCOME TO THE OFFICE!
  9. 9. AFT Overhead PanelSpend a few minutes finding your way around.The first thing you will notice is how small and crowded it is!
  10. 10. Forward Overhead Panel
  11. 11. Glare shield Mode control panel and EFS control panels.
  12. 12. Looking aft the circuit breaker panels.
  13. 13. Windows 4 and 5 are now normally not fitted on the NG.
  14. 14. Window number 2 L and R can be opened.
  15. 15. Window 2 L shown open. Only window 2R can be opened from outside the aircraft.
  16. 16. LOGO Light SwitchOFF – logo lights on each side of vertical finextinguished.ON – logo lights illuminated. ANTI–COLLISION LightPOSITION Light Switch SwitchSTROBE & STEADY – red and green wing–tip position lights, white trailing OFF – red strobe/rotatingedge wing–tip lights and wing–tip and tail strobe lights illuminated. beacon lights on upperOFF – red and green wing–tip position lights, white trailing edge wing–tip lights and lower fuselageand wing–tip and tail strobe lights extinguished. extinguished.STEADY – red and green wing–tip position lights and white trailing edge ON – red strobe/rotatingwing–tip lights illuminated. beacon lights illuminated.WING Illumination SwitchOFF – wing leading edge lights on fuselage forward of wing extinguished.ON – wing leading edge lights illuminated.WHEEL WELL Light SwitchOFF – three wheel well lights extinguished.ON – wheel well lights illuminated.
  17. 17. The Nose wheel well light may be turned on at theExternal power panel. The ON position of this switchwill override the cockpit switch.
  18. 18. The Nose wheel well light may be turned on at theExternal power panel. The ON position of this switchwill override the cockpit switch. The main wheel well lights may be turned ON by a switch in the left main wheel well. This switch should be left in the Normal position as the ON position overrides the Cockpit switch.
  19. 19. EMERGENCY LIGHTS
  20. 20. EMERGENCY LIGHTS3 rechargeable Battery packs.
  21. 21. EMERGENCY LIGHTSCharged from DC BUS 1.
  22. 22. EMERGENCY LIGHTS Battery packs will fully charge in 90 minutes.
  23. 23. EMERGENCY LIGHTSEmergency light come on if DC BUS 1 falls below 12 Volts.
  24. 24. EMERGENCY LIGHTSThe emergency light batteries will supply emergency lightingfor more than 10 minutes.
  25. 25. Emergency Light SwitchForward Overhead panel.
  26. 26. In the guarded armed position theemergency lights will illuminate When;DC BUS 1 is unpowered.Or when AC power is removed.
  27. 27. Emergency light switch must be OFF beforepower is removed from the aircraftIn the guarded armed position theemergency lights will illuminate When; DC BUS 1 is unpowered. Or when AC power is removed.
  28. 28. Emergency light switch must be OFF beforepower is removed from the aircraft There is a second location that the emergency lights can be switched ON.In the guarded armed position theemergency lights will illuminate When; DC BUS 1 is unpowered. Or when AC power is removed.
  29. 29. Emergency light switch must be OFF beforepower is removed from the aircraft There is a second location that the emergency lights can be switched ON.In the guarded armed position the Aft attendants panel.emergency lights will illuminate When; Flight deck switch must be ARMED. This switch must be in Normal to allow DC BUS 1 is unpowered. emergency light battery charging Or when AC power is removed.
  30. 30. Door Annunciator Lights
  31. 31. Door Annunciator LightsLower Nosecompartmentdoor Electronic Equipment door.
  32. 32. Over wing Emergency Escape DoorsThere are either 2 or 4 Type III emergency exits. These are canopy or gullwing type doors that open out and up. The doors are held closed bymechanical locks and cabin pressure.The doors can be opened from either inside or outside of the aircraft.The door is opened by a counterbalance spring assembly. The rate ofopening is controlled by a hydraulic snubber unit.
  33. 33. Basic Aircraft Dimensions
  34. 34. What is the minimum pavement width to perform a 180° turn in a B737-800? a. 61 feet or 18.6 meters. b. 66 feet or 20.1 meters. c. 69 feet or 21.0 meters. d. 79 feet or 24.0 meters.
  35. 35. What is the minimum pavement width to perform a 180° turn in a B737-800? a. 61 feet or 18.6 meters. b. 66 feet or 20.1 meters. c. 69 feet or 21.0 meters. d. 79 feet or 24.0 meters.
  36. 36. Maximum Runway Slope. +/- 2%
  37. 37. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.
  38. 38. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.
  39. 39. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets.
  40. 40. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets. Maximum Flight Operating 82° North & South Latitude.
  41. 41. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets. Maximum Flight Operating 82° North & South Latitude. 737-800 Max T/O Weight. 75,976 kg.
  42. 42. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets. Maximum Flight Operating 82° North & South Latitude. 737-800 Max T/O Weight. 75,976 kg. 737-800 Max Landing 65,317 kg. Weight.
  43. 43. Maximum Runway Slope. +/- 2%Maximum Operating Altitude. 41,000 Ft.Maximum Takeoff & 8,400 Ft.Landing Altitude.Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets. Maximum Flight Operating 82° North & South Latitude. 737-800 Max T/O Weight. 75,976 kg. These weights vary depending on airline certification 737-800 Max Landing 65,317 kg. requirements. Weight. Aircraft FCOM applies!
  44. 44. The minimum wing tip turning radius of a B737-800 with wingletsis?
  45. 45. The minimum wing tip turning radius of a B737-800 with wingletsis? 75’ 2” Feet or 22.9 Metres.
  46. 46. The minimum wing tip turning radius of a B737-800 with wingletsis? 75’ 2” Feet or 22.9 Metres.The retractable landing light may be extended up to what maximumspeed?
  47. 47. The minimum wing tip turning radius of a B737-800 with wingletsis? 75’ 2” Feet or 22.9 Metres.The retractable landing light may be extended up to what maximumspeed? At ANY SPEED
  48. 48. The minimum wing tip turning radius of a B737-800 with wingletsis? 75’ 2” Feet or 22.9 Metres.The retractable landing light may be extended up to what maximumspeed? At ANY SPEEDWith the EMERG LIGHTS SWITCH in the guarded ARMposition. All Emergency lights will illuminate automatically if.
  49. 49. The minimum wing tip turning radius of a B737-800 with wingletsis? 75’ 2” Feet or 22.9 Metres.The retractable landing light may be extended up to what maximumspeed? At ANY SPEEDWith the EMERG LIGHTS SWITCH in the guarded ARMposition. All Emergency lights will illuminate automatically if.DC BUS 1 is Unpowered. (less than 12 Volts DC)DC BUS 1 is only powered when AC Transfer bus1 or 2 are powered. (See Electrical power)
  50. 50. Which door is open?
  51. 51. Which door is open?Either the lower nose compartment doorOr Electronic equipment door.
  52. 52. Lower Nose Compartment Electronic Equipment DoorDoor Aft of the nose wheel well.Forward of the Nose wheelwell
  53. 53. Lower Nose Compartment Electronic Equipment DoorDoor Aft of the nose wheel well.Forward of the Nose wheelwell Two doors but only 1 annunciator light.
  54. 54. OXYGEN SYSTEMAft Overhead Panel
  55. 55. OXYGEN SYSTEMSTypes of mask vary by aircraft tail number. This information is only general.
  56. 56. The thermal discharge port locatedon the right forward fuselage isclosed by a green disk. If missingthere may have been an overpressure discharge of Oxygen.
  57. 57. Typical Oxygen Mask Stowage Left side. Right is similar.
  58. 58. Some aircraft are equipped with a gaseous oxygen system.This is airline route dependent and the Passenger systemremains independent of the crew oxygen system.
  59. 59. Some aircraft are equipped with a gaseous oxygen system.This is airline route dependent and the Passenger systemremains independent of the crew oxygen system.Automatic activation varies on different aircraft and maybe from 14,000 to 15,650 feet.
  60. 60. Potable water system.
  61. 61. Vacuum Waste SystemThe aircraft is equipped with a vacuum waste system which uses cabindifferential pressure to move human waste from the toilet to a wasteholding tank. If differential pressure is too low there is a vacuum pumpwhich will operate automatically. The vacuum pump normally operateswhen the aircraft is on the ground or in flight below 16,000 feet.
  62. 62. Vacuum Waste SystemThe aircraft is equipped with a vacuum waste system which uses cabindifferential pressure to move human waste from the toilet to a wasteholding tank. If differential pressure is too low there is a vacuum pumpwhich will operate automatically. The vacuum pump normally operateswhen the aircraft is on the ground or in flight below 16,000 feet.The waste tank level indicator continuously indicates the level in thewaste tank.
  63. 63. Vacuum Waste SystemThe aircraft is equipped with a vacuum waste system which uses cabindifferential pressure to move human waste from the toilet to a wasteholding tank. If differential pressure is too low there is a vacuum pumpwhich will operate automatically. The vacuum pump normally operateswhen the aircraft is on the ground or in flight below 16,000 feet.The waste tank level indicator continuously indicates the level in thewaste tank.When the waste tank is full the LAV INOP light illuminates and thevacuum flushing system is disabled.
  64. 64. The toilet tank service panel is located on the left side of the aft fuselage
  65. 65. What is the wing span of the B737-800 with blendedwinglets?
  66. 66. What is the wing span of the B737-800 with blendedwinglets?
  67. 67. What is the overall length of the B737-800?
  68. 68. What is the overall length of the B737-800?
  69. 69. Under which condition will the OVERWING annunciator lightilluminate?
  70. 70. Under which condition will the OVERWING annunciator lightilluminate?When any over wing door is not full closed and locked.When any flight lock fails to engage when commanded tolock during take off or in flight.
  71. 71. Under which condition will the OVERWING annunciator lightilluminate?When any over wing door is not full closed and locked.When any flight lock fails to engage when commanded tolock during take off or in flight.What conditions are required to cause the flight locks toengage on the over wing emergency exits.
  72. 72. Under which condition will the OVERWING annunciator lightilluminate?When any over wing door is not full closed and locked.When any flight lock fails to engage when commanded tolock during take off or in flight.What conditions are required to cause the flight locks toengage on the over wing emergency exits.3 of the 4 main doors closed.Either engine running.BOTH thrust levers more than 53° ( Take off thrust range)Or Air mode.
  73. 73. Where is this located?
  74. 74. Where is this located?
  75. 75. In the guarded armed position theemergency lights will illuminate When?
  76. 76. In the guarded armed position theemergency lights will illuminate When?When DC BUS 1 is unpowered.Or when AC power is removed.
  77. 77. There is a second location that the emergency lights can be switched ON. Where is this?In the guarded armed position theemergency lights will illuminate When?When DC BUS 1 is unpowered.Or when AC power is removed.
  78. 78. Emergency light switch must be OFF beforepower is removed from the aircraft There is a second location that the emergency lights can be switched ON. Where is this?In the guarded armed position theemergency lights will illuminate When? Aft attendants panel. When DC BUS 1 is unpowered. Flight deck switch must be ARMED. Or when AC power is removed. This switch must be in Normal to allow emergency light battery charging
  79. 79. Maximum Runway Slope?
  80. 80. Maximum Runway Slope? +/- 2%
  81. 81. Maximum Runway Slope? +/- 2%Maximum OperatingAltitude?
  82. 82. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?
  83. 83. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff &Landing Altitude?
  84. 84. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?
  85. 85. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross windLimits with Winglets?
  86. 86. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?
  87. 87. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight OperatingLatitude?
  88. 88. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude?
  89. 89. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude? 737-800 Max T/O Weight?
  90. 90. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude? 737-800 Max T/O Weight? 75,976 kg.
  91. 91. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude? 737-800 Max T/O Weight? 75,976 kg. 737-800 Max Landing Weight?
  92. 92. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude? 737-800 Max T/O Weight? 75,976 kg. 737-800 Max Landing 65,317 kg. Weight?
  93. 93. Maximum Runway Slope? +/- 2%Maximum Operating 41,000 Ft.Altitude?Maximum Takeoff & 8,400 Ft.Landing Altitude?Maximum Cross wind 33 knots. 36 Knots without winglets.Limits with Winglets?Maximum Flight Operating 82° North & SouthLatitude? 737-800 Max T/O Weight? 75,976 kg. These weights vary depending 737-800 Max Landing 65,317 kg. on airline certification Weight? requirements. Aircraft FCOM applies!
  94. 94. Where can the wheel well lights be controlled?
  95. 95. Where can the wheel well lights be controlled?Forward overhead panel Main switch.
  96. 96. Where can the wheel well lights be controlled?Forward overhead panel Main switch.External electrical power panel Nose wheel welllight.
  97. 97. Where can the wheel well lights be controlled?Forward overhead panel Main switch.External electrical power panel Nose wheel welllight.Left hand Main wheel well Main wheel well light.
  98. 98. Where can the wheel well lights be controlled?Forward overhead panel Main switch.External electrical power panel Nose wheel welllight.Left hand Main wheel well Main wheel well light.External switches labelled as ON and NormalLeave in Normal to allow control from the flightdeck.
  99. 99. The END of Aircraft GeneralNow Take the test at www.theorycentre.comFor more information info@theorycentre.com

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