1 FlightSafety international These graphics are coded for security. This program is protected by copyright law and a license agreement between Flight Safety

1

FlightSafety international

These graphics are coded for security. This program is protected by copyright law and a license agreement between Flight Safety and CPaT.

Unauthorized copying of this program will be punished to the maximum extent allowed by law.



BOEING 737-200

2

NEXT >NEXT >

737 AIRCRAFT GENERAL

3

737-200 INTRODUCTION737-200 INTRODUCTION

CABIN INTRODUCTIONCABIN INTRODUCTION

CABIN EMERGENCY EXITSCABIN EMERGENCY EXITS

FLIGHT ATTENDANT STATIONSFLIGHT ATTENDANT STATIONS

GALLEYS and POTABLE WATERGALLEYS and POTABLE WATER

COCKPIT and COCKPIT SEATSCOCKPIT and COCKPIT SEATS

FORWARD AIRSTAIRSFORWARD AIRSTAIRS

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65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER

21 ENTER21 ENTEREXTERIOR WALKAROUNDEXTERIOR WALKAROUND

4

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737INTRODUCTION

5

The 737 is a short to medium range transport jet.

The aircraft range is approximately 1,500 miles.

NEXT >

The 737 is a short to medium range transport jet.

The aircraft range is approximately 1,500 miles.

NEXT >

6

The aircraft is serviced on the right side.

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The aircraft is serviced on the right side.

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Forward Lavatory

Forward GalleyFueling

Aft Lavatory

Aft Galley

Potable Water

7

The Forward and Aft cargo compartments may be accessed through the doors on the right side of the aircraft.

The doors are plug type and open inward, hinged at the top.

NEXT >

The Forward and Aft cargo compartments may be accessed through the doors on the right side of the aircraft.

The doors are plug type and open inward, hinged at the top.

NEXT >

Forward Cargo Compartment Door

Aft Cargo Compartment Door

8

The cargo doors are both open on this frame. The total volume of the Forward bin is 370 cu. ft.; the aft bin total volume is 505 cu. ft.

NEXT >

The cargo doors are both open on this frame. The total volume of the Forward bin is 370 cu. ft.; the aft bin total volume is 505 cu. ft.

NEXT >

Forward Cargo Compartment Door51” X 48”

Aft Cargo Compartment Door 48” X 48”

9

The External Power Receptacle is located on the right side of the aircraft beneath the First Officer’s windows.

NEXT >

The External Power Receptacle is located on the right side of the aircraft beneath the First Officer’s windows.

NEXT >

10

93’ (28.35m)

36’ (10.97m)

17’ 2” (5.23m)

Please note the dimensions on this frame.

NEXT >


NEXT >

11


NEXT >


NEXT >

100’ (30.48m)

12

13’ 0” (3.96m)


NEXT >


NEXT >

37’(11.28m)

13

37’ 4”” (11.37m)

96’ 11”(29.53m)


NEXT >


NEXT >

14

60’ 2” MINIMUMFOR 1800 TURN

AROUNDThe nose wheel steering

maximum turning angle is 780. A 30 tire slip provides a resulting effective turn angle maximum of only 750.

The blue arc displays the nose gear travel during a maximum effort turn

The red arc displays the arc of the aircraft nose during a maximum effort turn.

The white arc displays the arc of the wing during the turn. The wing arc is larger than the nose arc.

If a maximum effort turn is used to turn around from the edge of the taxiway as shown here, a minimum taxiway width of 60’ 2” is required.

NEXT >

The nose wheel steering maximum turning angle is 780. A 30 tire slip provides a resulting effective turn angle maximum of only 750.

The blue arc displays the nose gear travel during a maximum effort turn

The red arc displays the arc of the aircraft nose during a maximum effort turn.

The white arc displays the arc of the wing during the turn. The wing arc is larger than the nose arc.

If a maximum effort turn is used to turn around from the edge of the taxiway as shown here, a minimum taxiway width of 60’ 2” is required.

NEXT >

15

Note how the wings sweep during the turn.

NEXT >

Note how the wings sweep during the turn.

NEXT >

60’ 2” MINIMUMFOR 1800 TURN

AROUND

16

The nose landing gear retracts forward into the nose gear well.

The nose gear extension and retraction is normally operated through hydraulic system pressure.

A red line painted on the nose gear doors indicates the maximum turning angle of the nose gear during tow.

NEXT >

The nose landing gear retracts forward into the nose gear well.

The nose gear extension and retraction is normally operated through hydraulic system pressure.

A red line painted on the nose gear doors indicates the maximum turning angle of the nose gear during tow.

NEXT >

17

The 737-200 aircraft are available in two basic types. The BASIC version is the earlier model, and the ADVANCED version is the later mode.

These two types have slightly different system operations.

We will identify these differences as we progress.

NEXT >

The 737-200 aircraft are available in two basic types. The BASIC version is the earlier model, and the ADVANCED version is the later mode.

These two types have slightly different system operations.

We will identify these differences as we progress.

NEXT >

18

Maximum Takeoff Weight = 109,000 lbs.Maximum Landing Weight = 98,000 lbs.

Max. Zero Fuel Weight = 88,000 lbs.Operating Empty Weight = 62,000lbs.

Fuel Capacity = 25,250 lbs.

Maximum Takeoff Weight = 109,000 lbs.Maximum Landing Weight = 98,000 lbs.

Max. Zero Fuel Weight = 88,000 lbs.Operating Empty Weight = 62,000lbs.

Fuel Capacity = 25,250 lbs.

The weights of the aircraft are shown here.

NEXT >

The weights of the aircraft are shown here.

NEXT >

19

QUESTION

What is the required minimum distance for a 1800 taxi turn around?

a. 60’ 2”

b. 65’ 0

The correct answer is “a” NEXT >The correct answer is “a” NEXT >

20

QUESTION

The External Power Receptacle is located on which side of the aircraft?

a. Left side

b. Right side

The correct answer is “b” NEXT >The correct answer is “b” NEXT >

21








3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER

NEXTNEXTEXTERIOR WALKAROUNDEXTERIOR WALKAROUND

22

NEXT >NEXT >

737 EXTERIOR WALKAROUND

Two pitot / static probes , one Angle of Attack sensor, and one Rosemond Total Air Temperature probe are located below the windows on the left side of the cockpit.

An Alternate static port is located as shown by the green arrow.

NEXT >

Two pitot / static probes , one Angle of Attack sensor, and one Rosemond Total Air Temperature probe are located below the windows on the left side of the cockpit.


NEXT >

Two pitot / static probes are located below the cockpit windows on the right side.


NEXT >

Two pitot / static probes are located below the cockpit windows on the right side.


NEXT >

A pitot tube is located on both the left and right sides of the Vertical Stabilizer.

These pitot tubes sense airspeed information, and deliver the information to the elevator feel system.

NEXT >

A pitot tube is located on both the left and right sides of the Vertical Stabilizer.

These pitot tubes sense airspeed information, and deliver the information to the elevator feel system.

NEXT >

26

The weather radar antenna is located behind the radome in the nose section of the aircraft.

NEXT to open the radome >

The weather radar antenna is located behind the radome in the nose section of the aircraft.

NEXT to open the radome >

27

The antenna is a flat dish type, typical to those used in a color radar display installation.

NEXT >

The antenna is a flat dish type, typical to those used in a color radar display installation.

NEXT >

28

NosewheelSteeringCylinders

Here, you can see a cut away view of the nose gear in the extended position.

The nosewheel steering is operated by two nose wheel steering cylinders.

One nose gear taxi light is installed.

NEXT >

Here, you can see a cut away view of the nose gear in the extended position.

The nosewheel steering is operated by two nose wheel steering cylinders.

One nose gear taxi light is installed.

NEXT >

29

The snubbers (2) are shown in the top of the nose gear wheel well. When the gear retracts, each tire contacts a snubber to stop wheel spin.

The nose gear doors are mechanically closed when the gear is retracted.

NEXT >

The snubbers (2) are shown in the top of the nose gear wheel well. When the gear retracts, each tire contacts a snubber to stop wheel spin.

The nose gear doors are mechanically closed when the gear is retracted.

NEXT >

30

The snubbers stop the wheels’ spin.

The nose gear is held up by an over center link. No hydraulic pressure is needed to hold the gear up.

The two nose gear doors are retracted mechanically.

NEXT >

The snubbers stop the wheels’ spin.

The nose gear is held up by an over center link. No hydraulic pressure is needed to hold the gear up.

The two nose gear doors are retracted mechanically.

NEXT >

31

The FLIGHT INTERPHONE allows the ground crew to communicate with the pilots through use of the FLIGHT jack on the external power receptacle.

NEXT >

The FLIGHT INTERPHONE allows the ground crew to communicate with the pilots through use of the FLIGHT jack on the external power receptacle.

NEXT > NOSEWHEELWELL

LIGHT

EXTERNALPOWER

CONN

NOTIN USE

INTERPHONE

FLIGHT SERVICE

ON

NORM

PILOT

CALL

32

The Oxygen Blow Out disc is located on the right side of the fuselage. This disc will be described in more detail in the Oxygen section.

The cargo doors are shown open on this frame. The doors are hinged at the top and open inward.

The doors are manually operated and can be operated from either inside or outside the aircraft.

NEXT >

The Oxygen Blow Out disc is located on the right side of the fuselage. This disc will be described in more detail in the Oxygen section.

The cargo doors are shown open on this frame. The doors are hinged at the top and open inward.

The doors are manually operated and can be operated from either inside or outside the aircraft.

NEXT >

33

The cargo compartments comply with the Class “D” FAA category. The Class “D” status indicates that these compartments are not ventilated and will not support a fire.

The compartments are sealed and pressurized. The compartment pressurization is maintained by pressure equalization valves. These valves open intermittently to vent the cargo compartments during climb out and to pressurize the compartments during descent.

Blow out panels are installed in the compartments to protect the aircraft in the event of a rapid decompression.

NEXT >

The cargo compartments comply with the Class “D” FAA category. The Class “D” status indicates that these compartments are not ventilated and will not support a fire.

The compartments are sealed and pressurized. The compartment pressurization is maintained by pressure equalization valves. These valves open intermittently to vent the cargo compartments during climb out and to pressurize the compartments during descent.

Blow out panels are installed in the compartments to protect the aircraft in the event of a rapid decompression.

NEXT >

34

FIREWARN

BELL CUTOUT

FIREWARN

BELL CUTOUT

FIREWARN

BELL CUTOUT

FIREWARN

BELL CUTOUT

If either cargo door is not closed and locked, the MASTER CAUTION lights and the DOOR system annunciator light will be on.

NEXT >

If either cargo door is not closed and locked, the MASTER CAUTION lights and the DOOR system annunciator light will be on.

NEXT >

MASTERCAUTION

PUSH TO RESET

MASTERCAUTION

PUSH TO RESET

MASTERCAUTION

PUSH TO RESET

MASTERCAUTION

PUSH TO RESET

FLT CONT ELEC

APU

FUEL OVHT/DET

ANTI-ICE

HYD OVERHEAD

DOORS AIR COND

35

Shown above in red is the Access door for the Electronics/Electrical compartment.

Aft of this door is the exhaust port for the equipment cooling air. This opening allows cooling air to flow over the electrical equipment and flow overboard when the aircraft is on the ground and when the cabin differential pressure is low.

The Lower Nose Compartment contains radar equipment.

NEXT >

Shown above in red is the Access door for the Electronics/Electrical compartment.

Aft of this door is the exhaust port for the equipment cooling air. This opening allows cooling air to flow over the electrical equipment and flow overboard when the aircraft is on the ground and when the cabin differential pressure is low.

The Lower Nose Compartment contains radar equipment.

NEXT >

36

Ram Air provides cooling airflow over the air conditioning heat exchangers. Shown above is the inlet for the right pack, and the exhaust from the right pack heat exchanger.

When on the ground, a deflector opens on the front of this inlet door to keep debris from entering into the Ram Air flow system.

The left pack cooling airflow is identical.

NEXT >

Ram Air provides cooling airflow over the air conditioning heat exchangers. Shown above is the inlet for the right pack, and the exhaust from the right pack heat exchanger.

When on the ground, a deflector opens on the front of this inlet door to keep debris from entering into the Ram Air flow system.

The left pack cooling airflow is identical.

NEXT >

37

The pack heat exchanger Inlet Door and the Exhaust Door open and close automatically to regulate the amount of cooling airflow that flows through the pack heat exchangers.

The Inlet and Exhaust doors are mechanically positioned open / closed by a common mechanical linkage.

NEXT >

The pack heat exchanger Inlet Door and the Exhaust Door open and close automatically to regulate the amount of cooling airflow that flows through the pack heat exchangers.

The Inlet and Exhaust doors are mechanically positioned open / closed by a common mechanical linkage.

NEXT >

38

A Runway Turnoff light is installed in the leading edge of each wing. This light shines outward to provide visibility during a taxi turn.

NEXT >

A Runway Turnoff light is installed in the leading edge of each wing. This light shines outward to provide visibility during a taxi turn.

NEXT >

RIGHTRUNWAY TURNOFF LIGHT

39 RIGHT INBOARD LANDING LIGHT

RIGHTRUNWAY TURNOFF LIGHT

An Inboard Landing light is installed in the leading edge of each wing. This light is outboard the Runway Turnoff light.

NEXT >

An Inboard Landing light is installed in the leading edge of each wing. This light is outboard the Runway Turnoff light.

NEXT >

40

The Pratt & Whitney JT8D-9A turbofan engine is shown here.

The two engines are wing mounted and are low enough for “eye level” maintenance.

The engines are mounted forward of the main gear and outboard far enough to not ingest water or slush from the nose gear.

Sea Level rated thrust is 14,500 lbs.

NEXT >

The Pratt & Whitney JT8D-9A turbofan engine is shown here.

The two engines are wing mounted and are low enough for “eye level” maintenance.

The engines are mounted forward of the main gear and outboard far enough to not ingest water or slush from the nose gear.

Sea Level rated thrust is 14,500 lbs.

NEXT >

41

The Pratt & Whitney JT8D-9A engine is equipped with a hydraulically operated “bucket type” thrust reverser system.

NEXT to observe the thrust reverser extend >

The Pratt & Whitney JT8D-9A engine is equipped with a hydraulically operated “bucket type” thrust reverser system.

NEXT to observe the thrust reverser extend >

42

When the Thrust Reverser is fully deployed, the entire engine thrust is deflected forward.

The thrust reversers are normally powered by the “A” hydraulic system, with reserve operation available from accumulator pressure (on the basic aircraft) or the Standby hydraulic system (on the advanced aircraft).

NEXT >

When the Thrust Reverser is fully deployed, the entire engine thrust is deflected forward.

The thrust reversers are normally powered by the “A” hydraulic system, with reserve operation available from accumulator pressure (on the basic aircraft) or the Standby hydraulic system (on the advanced aircraft).

NEXT >

43

The Leading Edge Flaps and Leading Edge Slats are shown here.The under-wing Krueger-type L.E. Flaps have two positions, Retract

and Full Extend. NEXT >

The Leading Edge Flaps and Leading Edge Slats are shown here.The under-wing Krueger-type L.E. Flaps have two positions, Retract

and Full Extend. NEXT >

44

The inboard 2 L.E. Slats on each wing have two positions, Retract and Full Extend.

The outboard L.E. Slats have three positions, Retract, Extend, and Full Extend. All Slat extension is selected by the Flap Handle. NEXT >

The inboard 2 L.E. Slats on each wing have two positions, Retract and Full Extend.

The outboard L.E. Slats have three positions, Retract, Extend, and Full Extend. All Slat extension is selected by the Flap Handle. NEXT >

BasicAircraft

Outboard Outboard

Inboard

Inboard Inboard

Inboard

45

The Inboard and Outboard Trailing Edge Flaps are shown in blue.

The T.E. Flaps normally operate hydraulically. An electric motor is available to provide alternate flap operation.

The Flaps are selected to Flaps 30 or Flaps 40 for a normal landing.

The Takeoff flap range is between Flaps 1and Flaps 25.

NEXT >

The Inboard and Outboard Trailing Edge Flaps are shown in blue.

The T.E. Flaps normally operate hydraulically. An electric motor is available to provide alternate flap operation.

The Flaps are selected to Flaps 30 or Flaps 40 for a normal landing.

The Takeoff flap range is between Flaps 1and Flaps 25.

NEXT >

46

The Ailerons provide lateral control.

The Ailerons normally operate with hydraulic pressure.

NEXT >

The Ailerons provide lateral control.

The Ailerons normally operate with hydraulic pressure.

NEXT >

47

The Flight Spoilers can be extended inflight as speedbrakes. As speedbrakes, they decelerate the aircraft and increase descent rates.

The Flight Spoilers will augment the Aileron operation when the control wheel is rotated more than 10 degrees.

The Flight Spoilers will extend further when used on the Ground as Ground Spoilers.

NEXT >

The Flight Spoilers can be extended inflight as speedbrakes. As speedbrakes, they decelerate the aircraft and increase descent rates.

The Flight Spoilers will augment the Aileron operation when the control wheel is rotated more than 10 degrees.

The Flight Spoilers will extend further when used on the Ground as Ground Spoilers.

NEXT >

48

The Ground Spoilers can only extend when there is weight on the main gear.

These Ground Spoilers aid in the deceleration during rejected takeoffs or during landings.

When the Ground Spoilers are extended,the Flight Spoilers also extend.

NEXT >

The Ground Spoilers can only extend when there is weight on the main gear.

These Ground Spoilers aid in the deceleration during rejected takeoffs or during landings.

When the Ground Spoilers are extended,the Flight Spoilers also extend.

NEXT >

49

Here we show the aircraft in flight with the Landing Gear retracted.

NEXT to extend the Landing Gear >

Here we show the aircraft in flight with the Landing Gear retracted.

NEXT to extend the Landing Gear >

50

Each of the Landing Gear is equipped with two wheels.

The Main Gear wheels have brakes, with Anti-skid protection.

NEXT >

Each of the Landing Gear is equipped with two wheels.

The Main Gear wheels have brakes, with Anti-skid protection.

NEXT >

51

Tire screens provide protection for the hydraulic components and the flight control components that are located in the main gear well area.

Should a tire fail while the gear are retracted, these screens should contain the tire failure. Locking Pins hold the screens in place.

NEXT >

Tire screens provide protection for the hydraulic components and the flight control components that are located in the main gear well area.

Should a tire fail while the gear are retracted, these screens should contain the tire failure. Locking Pins hold the screens in place.

NEXT >

screenlocking

pins

52

The hydraulic reservoirs for the “A” , “B”, and “STANDBY” hydraulic systems are all located in the main gear well.

NEXT >

The hydraulic reservoirs for the “A” , “B”, and “STANDBY” hydraulic systems are all located in the main gear well.

NEXT >

53

In the main gear well, there two electric pumps that provide pressure to the B hydraulic system.

There is also one electric pump that provides the hydraulic pressure to the Standby system.

NEXT >

In the main gear well, there two electric pumps that provide pressure to the B hydraulic system.

There is also one electric pump that provides the hydraulic pressure to the Standby system.

NEXT >

54

The APU has a Ground Control Panel and Fire Warning Horn in aft portion of the right main wheel well close to the edge of the fuselage.

An APU Fire Control Handle, Bottle Discharge switch, Horn Cutout button, Red light, and Horn are all installed on this panel.

NEXT >

The APU has a Ground Control Panel and Fire Warning Horn in aft portion of the right main wheel well close to the edge of the fuselage.

An APU Fire Control Handle, Bottle Discharge switch, Horn Cutout button, Red light, and Horn are all installed on this panel.

NEXT >

BOTTLEDISCHARGE

APUFIRE

CONTROL1. PULL HANDLE DOWN2. DISCHARGE BOTTLE

BOTTLE DISCHARGE

HORNCUTOUT

horn

55

APU Fire Protection is provided from one Freon bottle located on the AFT right side of the aircraft.

Engine Fire Protection is provided by two freon bottles located in the left main gear well.

NEXT >

APU Fire Protection is provided from one Freon bottle located on the AFT right side of the aircraft.

Engine Fire Protection is provided by two freon bottles located in the left main gear well.

NEXT >

56

Far below the Aft Galley Service Door is the Negative Pressure Relief Valve, the Main Outflow Valve and the two Positive Pressure Relief Valves.

NEXT >

Far below the Aft Galley Service Door is the Negative Pressure Relief Valve, the Main Outflow Valve and the two Positive Pressure Relief Valves.

NEXT >

57

The APU is located in the tail section of the aircraft.

The inlet door for APU combustion air is located aft of the Aft Galley Service Door.

APU Exhaust exits the aircraft as shown above.

NEXT >

The APU is located in the tail section of the aircraft.

The inlet door for APU combustion air is located aft of the Aft Galley Service Door.

APU Exhaust exits the aircraft as shown above.

NEXT >

58

Inlet Air for combustion and cooling enters the APU compartment from the aircraft right side. This inlet air enters the compartment through an automatic door.

APU Exhaust is delivered straight out the aft end of the aircraft.

NEXT >

Inlet Air for combustion and cooling enters the APU compartment from the aircraft right side. This inlet air enters the compartment through an automatic door.

APU Exhaust is delivered straight out the aft end of the aircraft.

NEXT >

59

The inlet door for APU combustion air provides airflow as shown above.

Fuel is normally provided to the APU from the #1 fuel tank.

Bleed air is delivered from the APU as shown in red.

Combustion gases from the APU exit the aircraft behind the APU.

NEXT >

The inlet door for APU combustion air provides airflow as shown above.

Fuel is normally provided to the APU from the #1 fuel tank.

Bleed air is delivered from the APU as shown in red.

Combustion gases from the APU exit the aircraft behind the APU.

NEXT >

60

The Forward Outflow Valve for the pressurization system is shown on this frame.

This Valve will close when the Main Outflow Valve on the right side of the fuselage, is almost fully closed.

NEXT >

The Forward Outflow Valve for the pressurization system is shown on this frame.

This Valve will close when the Main Outflow Valve on the right side of the fuselage, is almost fully closed.

NEXT >

61

QUESTION

Where is the APU located?

a. Right main gear well

b. Tail section


62

QUESTION

Where is the APU Fire Control Panel located?

a. Right Main Gear Well

b. Tail section


63

QUESTION

What is the purpose of the pitot tubes that are located on both sides of the vertical stabilizer?

a. Rudder Travel limiting

b. Elevator Feel


64

QUESTION

Is there any ventilation provided to the two cargo compartments?

a. Yes, but only during flight

b. No, these are classified as Class “D” containers.


65








3 ENTER3 ENTER

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83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER


66

NEXT >NEXT >

737 CABIN

INTRODUCTION

67

We will now show an example of the cabin service, and seating configurations.

On this frame you can see the four exit doors and two overwing escape hatches from the cabin.

NEXT >

We will now show an example of the cabin service, and seating configurations.

On this frame you can see the four exit doors and two overwing escape hatches from the cabin.

NEXT >

68

On this frame we show the galley areas. The galleys are equipped with high speed ovens, hot beverage containers, hot cup receptacles, refrigeration, and storage compartment.

Galley power is controlled from the cockpit, and is 115 VAC.

NEXT >

On this frame we show the galley areas. The galleys are equipped with high speed ovens, hot beverage containers, hot cup receptacles, refrigeration, and storage compartment.

Galley power is controlled from the cockpit, and is 115 VAC.

NEXT >

69

Water is supplied to the galleys from the airplane’s pressurized water system and, in an emergency, may be shut off at the galleys.

NEXT >

Water is supplied to the galleys from the airplane’s pressurized water system and, in an emergency, may be shut off at the galleys.

NEXT >

70

The 2 Lavatories have now been added. . .

NEXT >

The 2 Lavatories have now been added. . .

NEXT >

71

The Flight Attendant Seats have now been added to the area by the Main Cabin Entry Door and by the Left Aft Service Door.

NEXT >

The Flight Attendant Seats have now been added to the area by the Main Cabin Entry Door and by the Left Aft Service Door.

NEXT >

72

The One Class passenger seats are shown on this frame.

There are 6 seats per row.

NEXT >

The One Class passenger seats are shown on this frame.

There are 6 seats per row.

NEXT >

73

Forward Stairs are installed, and on some aircraft, Aft Stairs are installed.

The AFT Stairs are only used as an emergency exit.

NEXT >

Forward Stairs are installed, and on some aircraft, Aft Stairs are installed.


NEXT >

74

On this frame , you can see the aft cabin area.

NEXT to remove the passenger seats >

On this frame , you can see the aft cabin area.

NEXT to remove the passenger seats >

EXITEXIT

75

Behind these walls are the aft galley and Flight Attendant seating areas.

NEXT to remove these walls and the galley equipment >

Behind these walls are the aft galley and Flight Attendant seating areas.

NEXT to remove these walls and the galley equipment >

EXITEXIT

76

The two aft service doors and the aft Flight Attendant station can be seen on this frame. Up to two Flight Attendants can sit on this seat.

The Aft Lavatory door is closed.

NEXT >

The two aft service doors and the aft Flight Attendant station can be seen on this frame. Up to two Flight Attendants can sit on this seat.

The Aft Lavatory door is closed.

NEXT >

EXITEXIT

77

NEXT to open the aircraft Aft lavatory door >NEXT to open the aircraft Aft lavatory door >

EXITEXIT

78

NEXT to see a cut-away view of the lavatories >NEXT to see a cut-away view of the lavatories >

EXITEXIT

79

Here is the aft lavatory.

Chemical water is recirculated by an electric pump to flush the toilet.

Potable water is provided to the wash basin.

NEXT >

Here is the aft lavatory.

Chemical water is recirculated by an electric pump to flush the toilet.

Potable water is provided to the wash basin.

NEXT >

80

Smoke detectors are installed in the lavatory ceilings. NEXT >

Smoke detectors are installed in the lavatory ceilings. NEXT >

81

A small fire extinguisher is installed beneath the wash basin in each lavatory.

This extinguisher can put out a fire in the trash container.

NEXT >

A small fire extinguisher is installed beneath the wash basin in each lavatory.

This extinguisher can put out a fire in the trash container.

NEXT >

82

QUESTION

What is the purpose of the fire extinguishers that are located below the wash basins in the lavatories?

a. Fire protection for the entire lavatory

b. Fire protection for the lavatory trash container


83








3 ENTER3 ENTER

65 ENTER65 ENTER

NEXTNEXT

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER


84

NEXT >NEXT >

737CABIN

EMERGENCY EXITS

85

For evacuation, these 4 doors can be opened and the evacuation slides may be inflated.

NEXT to show the evacuation slides deployed and inflated >

For evacuation, these 4 doors can be opened and the evacuation slides may be inflated.

NEXT to show the evacuation slides deployed and inflated >

86

The 4 evacuation slides are now inflated. A red “PULL TO INFLATE” handle is installed by the girt bar of all four slides.

The Forward Service Door slide normally inflates automatically.

NEXT to see the overwing exits opened >

The 4 evacuation slides are now inflated. A red “PULL TO INFLATE” handle is installed by the girt bar of all four slides.

The Forward Service Door slide normally inflates automatically.

NEXT to see the overwing exits opened >

87

The Overwing Exit doors are plug type.

These doors are pulled inward and placed on a seat row during evacuation. The passengers will normally exit off the wing trailing edge.

NEXT >

The Overwing Exit doors are plug type.

These doors are pulled inward and placed on a seat row during evacuation. The passengers will normally exit off the wing trailing edge.

NEXT >

88

If the aircraft is equipped with Aft Stairs, the stair is used as an emergency exit.

NEXT >

If the aircraft is equipped with Aft Stairs, the stair is used as an emergency exit.

NEXT >

89

On some aircraft, Aft Stairs are installed.


When the Aft Stairs is retracted, it completely occupies the doorway, making the door unusable for galley servicing.

NEXT >

On some aircraft, Aft Stairs are installed.


When the Aft Stairs is retracted, it completely occupies the doorway, making the door unusable for galley servicing.

NEXT >

90

The Aft Stairs normally remain in the retracted position.

NEXT >

The Aft Stairs normally remain in the retracted position.

NEXT >

91

The Aft stairway interior door control handle is shown in the “latched position”.

NEXT to unlatch the door >

The Aft stairway interior door control handle is shown in the “latched position”.

NEXT to unlatch the door >

LEFT AFT CABIN SERVICE DOOR

AftLavatory

92


AftLavatory

93


AftLavatory

94


AftLavatory

95

The Extend / Retract Switch may be used to operate an electric motor to open or close the door.

NEXT to animate >

The Extend / Retract Switch may be used to operate an electric motor to open or close the door.

NEXT to animate >


AftLavatory

96


AftLavatory

97


AftLavatory

98


AftLavatory

99


AftLavatory

100


AftLavatory

101


AftLavatory

102

The Door folds outward from the aircraft and deploys the stairway.

This is an emergency exit, no slide is installed on this door if the stair system is installed.

NEXT >

The Door folds outward from the aircraft and deploys the stairway.

This is an emergency exit, no slide is installed on this door if the stair system is installed.

NEXT >


AftLavatory

To Replay - 92 ENTERTo Replay - 92 ENTER

103

The door may also be opened by moving the control handle to the emergency position.

This action requires about 80 lbs. of force to move the handle down, and the door will then freefall. The freefall of the stair/door is described in detail in your Flight Manual.

NEXT >

The door may also be opened by moving the control handle to the emergency position.

This action requires about 80 lbs. of force to move the handle down, and the door will then freefall. The freefall of the stair/door is described in detail in your Flight Manual.

NEXT >


AftLavatory

104

The door may also be opened by use of the Exterior Stair control handle.

The exterior controls also allow for normal electric operation and for emergency operation.

NEXT >

The door may also be opened by use of the Exterior Stair control handle.

The exterior controls also allow for normal electric operation and for emergency operation.

NEXT >

105

The cockpit escape strap is shown here.

Escape straps are also available at the overwing exits.

NEXT >

The cockpit escape strap is shown here.

Escape straps are also available at the overwing exits.

NEXT >

106

QUESTION

How many cabin emergency exits are available?

a. 6

b. 7


107

QUESTION

How many evacuation slides are installed?

a. 4 (on aircraft without Aft stairs)

b. 6 (on aircraft without Aft stairs)


108








3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

NEXTNEXT

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER


109

NEXT >NEXT >

737FLIGHT ATTENDANT

STATIONS

110

Controls for the cabin lighting, Call system, Passenger Address, and Service Interphone are installed at the forward and aft Attendant stations.

NEXT >

Controls for the cabin lighting, Call system, Passenger Address, and Service Interphone are installed at the forward and aft Attendant stations.

NEXT >

111

ON

OFF

BRT

OFF

BRT

OFF

ON

OFF

ENTRY WORK GROUNDSERVICE

WINDOW CEILING

DIM DIM

LIGHTS

CALL SYSTEM MUSIC

CAPTAIN ATTENDANT RESET

This is the forward Flight Attendant control panel.

Controls for the cabin lights and cabin music are installed on this panel.

The Flight Attendants can call the cockpit or other attendants from this station.

The hand held mike allows the attendants to make a P.A. announcement.

The handset allows the attendants to talk over the service interphone with the cockpit or the other attendant station.

NEXT >

This is the forward Flight Attendant control panel.

Controls for the cabin lights and cabin music are installed on this panel.




NEXT >

112

ON

OFF

BRT

OFF

ENTRY WORK EMER EXIT

DIM

CALL SYSTEM

CAPTAIN A ATTENDANT RESET

LIGHTS

This is the AFT Flight Attendant control panel.

Controls for the work lights and entry lights are installed on this panel.

An EMER EXIT light control switch is installed on this panel.




NEXT >

This is the AFT Flight Attendant control panel.

Controls for the work lights and entry lights are installed on this panel.

An EMER EXIT light control switch is installed on this panel.




NEXT >

113

QUESTION

Which Flight Attendant panel has an Emergency Light control switch?

a. Forward

b. Aft


114

QUESTION

Both Flight Attendant panels have provisions to make P.A. announcements and to communicate over the Service Interphone system.

a. True

b. False


115








3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

NEXTNEXT

132 ENTER132 ENTER

183 ENTER183 ENTER


116

NEXT >NEXT >

737GALLEYS

117

The galleys are installed on the aircraft right side. The galleys are serviced by the forward and aft galley service doors on aircraft right.

The galleys provide ovens, hot beverage, refrigeration, and storage.

Galley electrical power is 115 VAC at 400 Hz. supplied by the APU, engine generators or ground power.

Water is provided to the galleys from the pressurized potable water system and may be shut off at each galley area.

NEXT >

The galleys are installed on the aircraft right side. The galleys are serviced by the forward and aft galley service doors on aircraft right.

The galleys provide ovens, hot beverage, refrigeration, and storage.

Galley electrical power is 115 VAC at 400 Hz. supplied by the APU, engine generators or ground power.

Water is provided to the galleys from the pressurized potable water system and may be shut off at each galley area.

NEXT >

GALLEYSGALLEYS

118

The Galley Power switch is located on the overhead panel in the center of the Electrical System Control Panel.

NEXT >

The Galley Power switch is located on the overhead panel in the center of the Electrical System Control Panel.

NEXT >

DRIVE TEMP

RISE

IN

TR 1TR 2

TR 3

TESTSTBYPWR

BATBUS

BATAPU GEN

GEN 2

INV

TESTSTBYPWR

GRDPWR

GEN 1

LOW OILPRESSURE

LOW OILPRESSURE

HIGH OILTEMP

HIGH OILTEMP

LOW OILPRESSURE

LOW OILPRESSURE

HIGH OILTEMP

HIGH OILTEMP

STANDBYPWR OFF

STANDBYPWR OFF

STANDBY POWER

BAT OFF AUTO

DISCONNECT DISCONNECT

1 2

OFF

BAT

ON

ACDC

GALLEYOFF

ON

RESIDVOLTS

119

View of cockpit looking AFT


Circuit Breakers for the Galley Power are located on the electrical circuit breaker panels behind the pilots.

The P6-11 and P6-12 panels are behind the copilot.

NEXT >

Circuit Breakers for the Galley Power are located on the electrical circuit breaker panels behind the pilots.

The P6-11 and P6-12 panels are behind the copilot.

NEXT >

P6-1

P6-2

P6-3

P18-1

P18-2

P18-3P6-4

P6-11

P6-12

120

QUESTION

Where is the Galley Power switch located?

a. On the electrical control panel - Overhead Cockpit panel.

b. On the forward galley.


121

QUESTION

Water supply to each galley can be shut off at the respective galley.

a. True

b. False


122

NEXT >NEXT >

737POTABLE WATER

123

The 30 gallon Potable water tank is located behind the aft cargo compartment. Some aircraft may only have a 20 gallon tank.

The tank is pressurized when the APU or the left engine is running.

The water lines supply fresh water to the galleys as shown above.

NEXT >

The 30 gallon Potable water tank is located behind the aft cargo compartment. Some aircraft may only have a 20 gallon tank.

The tank is pressurized when the APU or the left engine is running.

The water lines supply fresh water to the galleys as shown above.

NEXT >

124

The Potable water tank also supplies fresh water to wash basins in the lavatories.

A shut-off / drain valve is located in the cabinet below each lavatory sink.

NEXT >

The Potable water tank also supplies fresh water to wash basins in the lavatories.

A shut-off / drain valve is located in the cabinet below each lavatory sink.

NEXT >

125

WATER

QUANTITY

WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2

EXTERNAL SERVICE

PANEL

The External Water Service panel is located on the lower right side of the aft fuselage.

The Potable Water tank Quantity Indicator is located inside the cabin directly over the right Aft Galley Service Door.

NEXT to view this indicator >

The External Water Service panel is located on the lower right side of the aft fuselage.

The Potable Water tank Quantity Indicator is located inside the cabin directly over the right Aft Galley Service Door.

NEXT to view this indicator >

126

The lights on the Potable Water Tank Quantity Indicator will illuminate when the TEST button is depressed.

When the tank is full, all lights will illuminate.

NEXT to animate a test >

The lights on the Potable Water Tank Quantity Indicator will illuminate when the TEST button is depressed.

When the tank is full, all lights will illuminate.

NEXT to animate a test >

-

WATER

QUANTITY

WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2

127

-

WATER

QUANTITY

WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2

128

-

WATER

QUANTITY

WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2

129

-

WATER

QUANTITY

WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2WATER

QUANTITY

WATER

PUSH

1/4 3/4

E F

1/2

You can see that the 30 gallon potable water tank is half full in this example.

If the tank is FULL, all lights will come on.

NEXT >

You can see that the 30 gallon potable water tank is half full in this example.

If the tank is FULL, all lights will come on.

NEXT >To Replay - 127 ENTERTo Replay - 127 ENTER

130

QUESTION

Where is the panel that allows the crew to determine the quantity of potable water?

a. Over the Aft Right Service Door

b. Over the Forward Right Service Door


131

QUESTION

What may be used to pressurize the potable water supply?

a. APU or Right engine

b. APU or Left engine


132








3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

NEXTNEXT

183 ENTER183 ENTER


133

NEXT >NEXT >

737COCKPIT

134

The Cockpit speakers are shown above in red.

NEXT >

The Cockpit speakers are shown above in red.

NEXT >

135

The Escape Strap storage areas are shown above in red.

NEXT >

The Escape Strap storage areas are shown above in red.

NEXT >

136

The Map lights are shown above in red.

NEXT >

The Map lights are shown above in red.

NEXT >

137

The Aft Overhead panel holds the Crew and Passenger Oxygen controls, Thrust Reverse indications, an Audio Selector Panel, and various other items.

NEXT >

The Aft Overhead panel holds the Crew and Passenger Oxygen controls, Thrust Reverse indications, an Audio Selector Panel, and various other items.

NEXT >

138

The Forward Overhead panel holds the control panels for most of the aircraft systems.

NEXT >

The Forward Overhead panel holds the control panels for most of the aircraft systems.

NEXT >

139

The Exterior aircraft lighting control switches, Engine Ignition/Start Panel, and APU Start Switch are located in this area.

NEXT >

The Exterior aircraft lighting control switches, Engine Ignition/Start Panel, and APU Start Switch are located in this area.

NEXT >

140

The Lightshield, Autopilot Control Panel, and Flight Director Control Panels are shown here.

NEXT >

The Lightshield, Autopilot Control Panel, and Flight Director Control Panels are shown here.

NEXT >

141

The FIRE WARN, and MASTER CAUTION lights are located on the lightshield. System Annunciator panels are also located here.

NEXT >

The FIRE WARN, and MASTER CAUTION lights are located on the lightshield. System Annunciator panels are also located here.

NEXT >

142

The Captain’s, First Officer’s, and Center Instrument panels are located as shown above. Sun visors are stowed on each side.

NEXT >

The Captain’s, First Officer’s, and Center Instrument panels are located as shown above. Sun visors are stowed on each side.

NEXT >

143

The Alternate Static source selectors locations are shown above in red.

Oxygen panel locations are shown above in green.

NEXT >

The Alternate Static source selectors locations are shown above in red.

Oxygen panel locations are shown above in green.

NEXT >

144

The Control Stand is located between the two pilots.

NEXT >

The Control Stand is located between the two pilots.

NEXT >

145

The Forward Electronics Panel, Thrust Lever Quadrant, and Aft Electronics Panel are located on the Control Stand.

NEXT >

The Forward Electronics Panel, Thrust Lever Quadrant, and Aft Electronics Panel are located on the Control Stand.

NEXT >

Forward

Electronics

Panel

Thrust

Lever

Quadrant

Aft

Electronics

Panel

146



The cockpit door opens outward from the cockpit.

The door has 4 blow out panels that allow pressure equalization between the cabin and cockpit, in the event of a cockpit DEPRESSURIZATION.

Notice a mirror is installed at the top of the door.

NEXT >

The cockpit door opens outward from the cockpit.

The door has 4 blow out panels that allow pressure equalization between the cabin and cockpit, in the event of a cockpit DEPRESSURIZATION.

Notice a mirror is installed at the top of the door.

NEXT >

147



An Emergency Exit Handle allows the pilots to pull the handle to pull the two top blowout panels into the cockpit.

This Handle allows the pilots to exit in the event of an emergency when the door cannot be opened.

The cockpit door can normally be opened, closed, and locked from either side of the door.

NEXT >

An Emergency Exit Handle allows the pilots to pull the handle to pull the two top blowout panels into the cockpit.

This Handle allows the pilots to exit in the event of an emergency when the door cannot be opened.

The cockpit door can normally be opened, closed, and locked from either side of the door.

NEXT >

148

The cockpit door may be locked electrically using a switch on the Control Stand.

On this frame the door is locked (the switch light is extinguished).

When the door is locked with this switch, entry from the cabin requires the use of a door key.

The cockpit door cannot be locked without normal DC power.

NEXT >

The cockpit door may be locked electrically using a switch on the Control Stand.

On this frame the door is locked (the switch light is extinguished).

When the door is locked with this switch, entry from the cabin requires the use of a door key.

The cockpit door cannot be locked without normal DC power.

NEXT >

CAB DOORLOCK

CAB DOORUNLOCKEDCAB DOORUNLOCKED

149

When this switch is illuminated as shown here, the cockpit door is unlocked.

To lock the cockpit door, press the switch to extinguish the light.

NEXT >

When this switch is illuminated as shown here, the cockpit door is unlocked.

To lock the cockpit door, press the switch to extinguish the light.

NEXT >

CAB DOORLOCK

CAB DOORUNLOCKEDCAB DOORUNLOCKED

150



There are two observer seats in this cockpit.

The First Observer seat can be folded down after the observer is inside the cockpit.

NEXT to lower the First observer’s seat >

There are two observer seats in this cockpit.

The First Observer seat can be folded down after the observer is inside the cockpit.

NEXT to lower the First observer’s seat >

151



The seat back must be raised and locked into position.

The First observers seat is now lowered for use.

NEXT >

The seat back must be raised and locked into position.

The First observers seat is now lowered for use.

NEXT >

152



The second observers seat is located adjacent to the coat stowage closet behind the Captain.

NEXT >

The second observers seat is located adjacent to the coat stowage closet behind the Captain.

NEXT >

153



The nose gear viewer is located beneath a cover plate on the cockpit floor aft and between the two pilot’s seats.

NEXT >

The nose gear viewer is located beneath a cover plate on the cockpit floor aft and between the two pilot’s seats.

NEXT >

154



The Manual Gear Extension Handles are located below a door on the floor. The door is inboard and aft of the First Officer’s seat.

There is one handle for each of the landing gear.

NEXT to see the handles close up >

The Manual Gear Extension Handles are located below a door on the floor. The door is inboard and aft of the First Officer’s seat.

There is one handle for each of the landing gear.

NEXT to see the handles close up >

155

This frame shows that the handles for each gear are on the respective side of the floor panel.

NEXT >

This frame shows that the handles for each gear are on the respective side of the floor panel.

NEXT >

right main gearhandle

nose gearhandle

left main gearhandle

156

The right main gear handle is pulled up on this frame.

Remember that each handle releases the uplocks for only the respective landing gear.

NEXT >

The right main gear handle is pulled up on this frame.

Remember that each handle releases the uplocks for only the respective landing gear.

NEXT >

157



The Manual Passenger Oxygen Control Handle is located below this cover plate.

NEXT for a close-up view >

The Manual Passenger Oxygen Control Handle is located below this cover plate.

NEXT for a close-up view >

158

This handle can be pulled to manually activate the passenger oxygen system.

Pushing the handle for five seconds when the cabin altitude is below 14,000’ will shut-off the passenger oxygen supply.

This handle is not used frequently, because the passenger oxygen system is designed to operate automatically.

NEXT >

This handle can be pulled to manually activate the passenger oxygen system.

Pushing the handle for five seconds when the cabin altitude is below 14,000’ will shut-off the passenger oxygen supply.

This handle is not used frequently, because the passenger oxygen system is designed to operate automatically.

NEXT >

159



This frame shows the location of various items in the cockpit.

NEXT >

This frame shows the location of various items in the cockpit.

NEXT >

CrewOxygenValve

ObserversHandMicrophone

HalonFireExtinguisher

RainRepellent System

Emergency MedicalKit

CrashAxe

PBE

160

There are ten cockpit windows.

The windows are numbered 1 through 5 on each side.

NEXT >

There are ten cockpit windows.

The windows are numbered 1 through 5 on each side.

NEXT >

123

45

1 2 3

4 5

L1L2L3

L4L5

R1 R2 R3

R4 R5

Here is a view of the windows from inside the cockpit.

The windows are numbered as shown above.

The #2 windows Left and Right can be opened.

NEXT to open the #2 windows >

Here is a view of the windows from inside the cockpit.

The windows are numbered as shown above.

The #2 windows Left and Right can be opened.

NEXT to open the #2 windows >

L1L2L3

L4L5

R1 R2 R3

R4 R5

L1L3

L4L5

R1R3

R4 R5

The #2 windows move inward and aft when they are opened.

NEXT >

The #2 windows move inward and aft when they are opened.

NEXT >

L2 R2


164

QUESTION

How many cockpit jumpseats are installed?

a. One

b. Two


165

QUESTION

Which two blowout panels in the cockpit door may be removed for emergency evacuation from the cockpit?

a. Top two panels

b. Lower two panels


166

NEXT >NEXT >

737COCKPIT SEAT ADJUSTMENT

167

The pilot seat should be adjusted to that he may see over the top of the glareshield to the aircraft nose structure.

The pilot should also be able to see below the lightshield to the top of the Flight Guidance Approach Progress Display units.

NEXT >

The pilot seat should be adjusted to that he may see over the top of the glareshield to the aircraft nose structure.

The pilot should also be able to see below the lightshield to the top of the Flight Guidance Approach Progress Display units.

NEXT >

168

The pilot seat is controlled by these handles.

The “H” handle is used to adjust the horizontal (fore/aft) movement of the pilot seat.

The “V” handle is used to adjust the vertical position or seat height.

The “R” handle is used to Recline the seat back.

NEXT to animate the horizontal movement >

The pilot seat is controlled by these handles.

The “H” handle is used to adjust the horizontal (fore/aft) movement of the pilot seat.

The “V” handle is used to adjust the vertical position or seat height.

The “R” handle is used to Recline the seat back.

NEXT to animate the horizontal movement >

169

170

171

172

173

174

175

176

177

178

179

180

The horizontal seat movement will also cause the seat to vertically move up and down.

NEXT >

The horizontal seat movement will also cause the seat to vertically move up and down.

NEXT >To Replay - 169 ENTERTo Replay - 169 ENTER

181

A handle is installed at the top of each pilot’s window frame.

This handle is used to hold while making seat adjustments.

NEXT >

A handle is installed at the top of each pilot’s window frame.

This handle is used to hold while making seat adjustments.

NEXT >

182

QUESTION

Moving the pilot seat forward or aft will also affect the vertical position of the seat.

a. True

b. False


183








3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

NEXTNEXT


184

NEXT >NEXT >

737FORWARD STAIRS

185

If the aircraft is equipped with airstairs, the stairs provide entrance to the Main Cabin Door on the left side.

The Interior stair control panel is located inside the cabin, above the door.

NEXT for a close up of this panel >

If the aircraft is equipped with airstairs, the stairs provide entrance to the Main Cabin Door on the left side.

The Interior stair control panel is located inside the cabin, above the door.

NEXT for a close up of this panel >

186

The interior Stair Control Panel is shown on the right.

The LIGHTS switch on this panel has 3 positions. The ON position turns on the stairway tread lights; the Off position turns these lights off.

The AUTO position turns on these lights when the stairs extend.

NEXT >

The interior Stair Control Panel is shown on the right.

The LIGHTS switch on this panel has 3 positions. The ON position turns on the stairway tread lights; the Off position turns these lights off.

The AUTO position turns on these lights when the stairs extend.

NEXT >

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY

MAIN CABIN ENTRY DOOR

ON

187

The NORMAL stair control switch utilizes A.C. electrical power to operate the stair in the Retract or Extend direction.

The STANDBY switch utilizes A.C. and D.C. power and requires that the Battery switch in the cockpit is turned ON.

NEXT >

The NORMAL stair control switch utilizes A.C. electrical power to operate the stair in the Retract or Extend direction.

The STANDBY switch utilizes A.C. and D.C. power and requires that the Battery switch in the cockpit is turned ON.

NEXT >

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

188

To use the Standby switch, one must hold the spring loaded guard to the left.

NEXT to animate >

To use the Standby switch, one must hold the spring loaded guard to the left.

NEXT to animate >

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

189

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

190

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

191

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

192

The guard must be held to the left while the Standby switch is used to extend the stairs.

NEXT >

The guard must be held to the left while the Standby switch is used to extend the stairs.

NEXT >

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON


193

The STAIRS OPERATIONAL light will illuminate while the stairs are in transit.

NEXT >

The STAIRS OPERATIONAL light will illuminate while the stairs are in transit.

NEXT >

FORWARD AIRSTAIR

LIGHTS STAIRS

OPERATIONAL

STAIRSOPERATIONAL

OFF

AUTO

AIRSTAIR

RETRACT

EXTEND

NORMAL

RETRACT

EXTEND

STANDBY


ON

194

An Exterior Stair Control Handle is located below and aft of the stair door.

To use this handle, the operator must push the square button in.

NEXT to animate >

An Exterior Stair Control Handle is located below and aft of the stair door.

To use this handle, the operator must push the square button in.

NEXT to animate >

AIRSTAIREXTERIOROPERATION

NORMAL STANDBY

RETRACT

EXTEND

CAUTION 1. STOW HANDRAIL EXTENSION BEFORE RETRACTING2. LOWER HANDLE MUST LATCH IN FOLDED POSITION DURING RETRACTION

PUSH

195


NORMAL STANDBY

RETRACT

EXTEND


PUSH

196


NORMAL STANDBY

RETRACT

EXTEND


PUSH

197

The handle may now be rotated in either direction to extend or retract the stairs.

NEXT to animate the handle rotated in the RETRACT mode >

The handle may now be rotated in either direction to extend or retract the stairs.

NEXT to animate the handle rotated in the RETRACT mode >


NORMAL STANDBY

RETRACT

EXTEND


PUSH


198


NORMAL STANDBY

RETRACT

EXTEND


PUSH

199

If normal A.C. and D.C. power is available the stairs will retract.

If normal power is not available, the switch below the handle must be used to select STANDBY DC power to the stair system.

NEXT >

If normal A.C. and D.C. power is available the stairs will retract.

If normal power is not available, the switch below the handle must be used to select STANDBY DC power to the stair system.

NEXT >


NORMAL STANDBY

RETRACT

EXTEND



200

This spring loaded Standby power switch must be held while the stairs are operating.

Standby will operate the stairs even if the Battery Switch is OFF.

NEXT >

This spring loaded Standby power switch must be held while the stairs are operating.

Standby will operate the stairs even if the Battery Switch is OFF.

NEXT >


NORMAL STANDBY

RETRACT

EXTEND


201

QUESTION

Where is the exterior airstair control handle located?

a. Below and aft of the Main Cabin Door

b. Below and forward of the Main Cabin Door


202

QUESTION

The correct answer is “A” NEXT >The correct answer is “A” NEXT >

Where is the interior airstair control handle located?

a. Over the Main Cabin Door

b. On the Forward Flight Attendant panel

203








THE ENDTHE END

3 ENTER3 ENTER

65 ENTER65 ENTER

83 ENTER83 ENTER

109 ENTER109 ENTER

115 ENTER115 ENTER

132 ENTER132 ENTER

183 ENTER183 ENTER

NEXTNEXT


204

THE END737

AIRCRAFT GENERAL





BOEING 737-200

Documents

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