B737Cl Ac Gral Qrh 1

Front 1

The cockpit door

Back 1

Can only be locked with A.C. power.

Front 2

The cockpit door blow-out panels

Back 2

Open into the cockpit.

Front 3

To exit the cockpit with the cockpit door jammed closed

Back 3

Grasp the cockpit door emergency exit handle on the upper part of the door and pull forward.

Front 4

When turning the B737-300 on the ground

Back 4

The landing gear geometry and sweep back of the wings result in the tail arc being greater than the wing tip arc.

Front 5

When turning the B737-300 on the ground

Back 5

The landing gear geometry and sweep back of the wings result in an outward motion of the wing tips and tail.

Front 6

When turning the B737-300 on the ground the minimum pavement width for an 180 degree turn is

Back 6

65 feet ( 19.81 metres )

Front 7

The cargo compartments are

Back 7

Pressurised approximately equal to cabin pressure.

Front 8

In case of sudden loss of aircraft pressurisation, the pressure relief of the cargo compartments is accomplished by

Back 8

Blow-out panels.

Front 9

The aircraft water system is supplied by

Back 9

A single water tank located behind the aft cargo compartment.

Front 10

Water tank pressurisation is supplied from

Back 10

The left hand pneumatic duct only.

Front 11

Water tank capacity (737-300) is

Back 11

30 U.S. gallons.

Front 12

The potable water quantity indicator is located

Back 12

above the aft service door.

Front 13

Placing the Lights Test Switch to the TEST position

Back 13

Inhibits the master caution recall system.

Front 14

Failure of one main A.C. bus causes

Back 14

A partial loss of cockpit and passenger lighting.

Front 15

When ARMED, the emergency exit lights will automatically come on

Back 15

If electrical power to DC bus 1 fails or AC power is turned off.

Front 16

The NO SMOKING signs when selected to AUTO

Back 16

Illuminate when the landing gear is extended.

Front 17

The FASTEN BELTS signs when selected to AUTO will

Back 17

Illuminate when landing gear or flaps are extended.

Front 18

With Ground Power plugged in and the battery switch OFF, the Dim Entry Lights are powered

Back 18

By an electrical supply from the hot battery bus.

Front 19

The emergency exit lights and signs are powered

Back 19

From separate emergency power supplies installed in the passenger cabin.

Front 20

The illumination of the standby magnetic compass

Back 20

Is controlled by a separate switch at the base of the standby magnetic compass.

Front 21

With the NO SMOKING & FASTEN BELTS switches in the AUTO position

Back 21

The NO SMOKING signs will illuminate any time the gear is extended.

Front 22

Failure of the A.C. transfer bus NO.2 will

Back 22

Automatically turn on the emergency instrument flood lights.

Front 23

With the POSITION light switch in the ON BAT position and the AC buses not powered

Back 23

The position ( navigation ) lights will illuminate with the battery switch selected ON.

Front 24

With the Battery Switch ON and no AC power connected, available cockpit lighting includes

Back 24

White Dome lights, Standby Compass light.

Front 25

When operating the airstair from the interior control panel

Back 25

The entry door must be opened to the cocked position.

Front 26

When operating the airstair from the interior control panel in standby mode on DC power

Back 26

The STAIRS OPERATING light will not illuminate.

Front 27

Operation of the airstairs in winds above

Back 27

40 kts is not recommended.

Front 28

The fwd and aft entry doors and the galley service doors have

Back 28

Automatic slides.

Front 29

Portable EXIT lights are

Back 29

Not fitted on the B737 aircraft

Front 30

The emergency exit hatches can be removed from the outside by

Back 30

Pushing in the exterior panel at the top, then pushing inward and lifting it up.

Front 31

Escape lines (ropes/straps) are fitted

Back 31

Above the cockpit sliding windows and in overwing escape hatch frames.(Rear escape hatches only on B737-400).

Front 32

The First Officers sliding window can be

Back 32

Opened from the inside and outside.

Front 33

The passenger oxygen system is activated when the cabin reaches an altitude of

Back 33

14,000 Feet.

Front 34

The oxygen system on board the aircraft has

Back 34

Two separate systems, one for the flight deck and one for the cabin.

Front 35

During a decompression, the passenger oxygen will automatically drop from its stowage compartment. Oxygen will flow to all masks

Back 35

Only when any one of the masks of an oxygen generator unit is pulled down.

Front 36

In each lavatory there is

Back 36

A two mask passenger oxygen unit.

Front 37

To use the passenger portable oxygen

Back 37

Turn the yellow knob in a counterclockwise direction and plug the mask into the desired bottle outlet.

Front 38

The pre-flight inspection check of the escape slide units is

Back 38

The pressure indicator is in the green band.

Front 39

To operate a BCF extinguisher

Back 39

Hold the extinguisher upright, remove the ringed safety pin, aim the extinguisher at the base of the flames from a distance of 6 feet and press the top lever.

Front 40

Loud-hailers are located

Back 40

On the port side of the passenger cabin, one at the front, one at the rear.

Front 41

The passenger cabin Emergency Exit light switch is located at

Back 41

The Aft attendants panel.

Front 42

The fire axe is located in

Back 42

The flight deck.

Front 43

The lavatory fire extinguisher system operates

Back 43

automatically.

Front 44

The lavatory fire extinguisher system will automatically discharge when heat levels exceed

Back 44

180 degrees F.

Front 45

To check that a lavatory fire extinguisher has not discharged

Back 45

Check the nozzle tips (aluminium colour after discharge) and heat sensitive discs which discolour from the heat of the fire.

Front 46

Each passenger oxygen unit in the cabin

Back 46

Cannot be shut off once the flow of oxygen has started.

Front 47

The B737-300 aircraft cabin equipment includes

Back 47

Four portable oxygen bottles and two therapeutic oxygen sets.

Front 48

The passenger oxygen system

Back 48

Is supplied by individual chemical oxygen generators located at each Passenger Service Unit.

Front 49

Each passenger oxygen generator when activated

Back 49

Will produce oxygen for approximately 12 minutes.

Front 50

Passenger oxygen flowing to a mask is visually confirmed by

Back 50

A green in-line flow indicator.

Front 51

Normal pressure of the flight crew oxygen system is

Back 51

1850 P.S.I.

Front 52

Pressing the RESET/TEST slide lever at a crew member station will

Back 52

Activate the oxygen flow momentarily ( to test the regulator ) if the mask is stowed.

Front 53

The crew oxygen Flow Indicator will

Back 53

Show a yellow cross when oxygen is flowing.

Front 54

The crew member oxygen EMERGENCY/TEST selector is a

Back 54

Red control knob.

Front 55

100% oxygen is supplied under positive pressure at all cabin altitudes whenever

Back 55

The EMERGENCY/TEST selector is rotated clockwise.

Front 56

With the oxygen NORMAL/100% selector in the N (normal) position

Back 56

A mixture of ambient air with oxygen is provided on demand.

Front 57

To use a crew oxygen mask

Back 57

Squeeze the red RELEASE levers with the thumb and forefinger and remove from stowage.

Front 58

If the crew oxygen mask is not stowed, then by

Back 58

Closing both stowage box doors and pressing the RESET/TEST slide lever, the oxygen supply at the individual crew member station is shut off.

Front 59

As the crew oxygen harness inflates

Back 59

The flow indicator will momentarily show a yellow cross.

Front 60

To check the crew oxygen

Back 60

1) Mask stowed , NORMAL/100% switch - 100%.
2) RESET/TEST slide lever - push down and hold.
3) Observe a momentary yellow cross (FLOW INDICATOR)
4)EMERGENCY/TEST selector - push and hold.
5) Observe a constant yellow cross (FLOW INDICATOR)

Front 61

The passenger oxygen mask stowage units are activated

Back 61

Automatically by a barometric pressure switch when the cabin altitude is 14,000 Feet, or when the PASS OXYGEN switch on the overhead panel
is positioned to ON.

Front 62

Crew oxygen system pressure is correctly indicated when

Back 62

The battery switch is on.