Boeing 737-200 Quiz

Front 1

7 things the Fire Warning Switch does

Back 1

Generator Trips
Reverser is disarmed
Arms Engine Fire Warning Switch (Squib)
Bleed air shutoff valve - CLOSED
Disarms HYD PUMP LOW PRESS light (A sys)
Fuel Shutoff Valve - CLOSED
Hydraulic Shutoff Valve (A sys) - CLOSED

Front 2

6 things the APU Fire Warning Switch does

Back 2

Generator Trips
Arms the APU Fire Warning Switch (Squib)
Bleed Air Shutoff Valve - CLOSED
DoorInlet (APU) - CLOSES (17 seconds)
Fuel Shutoff Valve (at fuel manifold) - CLOSED
Solenoid Valve (FUEL) - CLOSED

Front 3

What indications do you get when doing the OVERHEAT/INOP test?

Back 3

Master Caution
Overheat CAP light
Engine 1 Overheat
Engine 2 Overheat
APU DET INOP

Front 4

What indications do you get when doing the FIRE test?

Back 4

Fire warning
Engine 1 Fire Switch
Engine 2 Fire Switch
APU Fire Switch
Wheel Well Fire Light (AC pwr required)
APU Wheel Well Bell/Light
Fire Warning Bell

Front 5

What components are powered by the A hydraulic system?

Back 5

Nosewheel steering
Ailerons
Inboard flight spoilers
Leading edge devices
Ground spoilers
Landing gear
Inboard brakes
Thrust reversers
Trailing edge flaps
Elevator
Rudder

Front 6

What components are powered by the B hydraulic system?

Back 6

Ailerons
Elevator
Rudder
Outboard flight spoilers
Outboard brakes
Yaw damper
Autobrakes
Autopilot

Front 7

What 4 things happen when the alternate flap switch does when placed to ARM?

Back 7

Bypass valve closes (Trailing Edge Flap hydraulic motor bypass valve)
Arms the STBY hydraulic LOW PRESS light
Pump activates (standby hydraulic pump motor)
210 switch activates (flaps switch)

Front 8

What 5 things occur when the FLIGHT CONTROL switch is placed to STDBY RUD?

Back 8

Shutoff valve closes (flight control shutoff valve)
Light is armed (flight control LOW PRESS light now indicates SHRAV posistion)
Arms STBY hyd LOW PRESS light
Pump activates (standby hydraulic pump motor)
Opens SHRAV (Standby Hydraulic Rudder Actuator Valve)

Front 9

What 2 things close the trailing edge flap hydraulic motor bypass valve?

Back 9

Alternate Flap switch placed to ARM
Flap comparitor notices more than 2 degree split on flap position gauge.

Front 10

Confirm these actions before opening the hydraulic ground interconnect...

Back 10

Parking Brake - SET
Flap Posistion - matches flap handle
Surfaces and NWS - Clear

Front 11

3 things that cause the pressure controller to switch to STBY:

Back 11

Cabin Pressure Altitude exceeds 13,875 ft.
Cabin ROC or DESCENT exceeds 1,800 fpm.
Loss of AC power for more than 15 seconds

Front 12

What are the three laws of the pack?

Back 12

ALWAYS ONE TO ONE ONE BLEED - ONE PACK
No ONE bleed source can power TWO pakcs (excessive bleed on engine)
No TWO bleed sources may power ONE pack (excessive bleed on the pack)

Front 13

What is the bleeds off takeoff procedure?

Back 13

Squeeze - Spread - Squeeze

L Pack - ON Isolation Valve - CLOSE R Pack - ON
L Bleed - OFF APU Bleed - ON R Bleed - ON

Front 14

When can the crew stop using oxygen after loss of pressurization?

Back 14

10,000 cabin pressure altitude

Front 15

On an unpressurized flight, when must the crew use supplemental oxygen?

Back 15

10k-12k if flight more than 30 minutes at that altitude
12k and above, at all times at those altitudes

Front 16

In normal pax operations in a pressurized cabin, when must crew use supplemental oxygen even though the aircraft is pressurized?

Back 16

FL 250 and above, if the other pilot is absent, the pilot at the controls must don a mask and use 100% oxygen.
Above FL 410, one pilot must be on O2 at all times even with a 2 man crew.

Front 17

What are the oxygen requirements for the crew/pax on the 737-200?

Back 17

Minimum Crew: 860 PSI
Minimum Pax: 1100 PSI
Normal for both: 1850 PSI
Min Manifold to activate Pax Oxygen: 3 PSI

Front 18

5 things that shut the APU down automatically:

Back 18

Low oil pressure
Actual overspeed
High oil temperature
Fire
Battery switch - OFF

Front 19

6 things we always turn LOW IGN on for:

Back 19

Landing
Icing conditions
Takeoff
Emergency Descent
Turbulence - Moderate to Severe
Precipitation - Moderate to Heavy

Front 20

Range of A/S Mach/VMO & Clacker:

Back 20

350-367 KIAS from SL to 23,456 ft
Mach .84 above 23,456 ft.

Front 21

Stall warning test indications and meanings:

Back 21

Off light extinguishes (heat to AOA vane)
Spinner rotates (continuity - AOA, flap indicator, flap computer)
Stick Shaker Activates (stick shaker motor)

Front 22

What requirements must be met for the cockpit voice recorder to operate?

Back 22

On ground: Either of the 35 psi oil switches active and AC transfer bus powered

In flight: Battery Bus powered

Front 23

4 things that cause takeoff configuration warning horn to sound:

Back 23

Speed brake not in the DOWN DETENT
Stab Trim out of the green takeoff band
Flaps not in the 1-25 flap range
Leading edge devices do not agree with trailing edge flap posistion

Front 24

4 things required for thrust reverser operation:

Back 24

Engine FIRE switch - CLOSED
35 PSI oil switch - sensed
Air/Ground safety swtich - GND
A system hydraulic pressure (via gear handle) or STBY pump

Front 25

How would you know if a START VALVE did not close?

Back 25

Engine start switch does not trip off between 35-40% N2
START VALVE OPEN light remains illuminated

Front 26

5 actions the BUS TRANSFER SYSTEM allows:

Back 26

Transfer bus seeks alternate source (opposite main gen)
STBY HYD Pump seeks alternate source
Elec Hyd Pump seeks alternate source (host pump off)
Allows #1 DC bus to seek it's alternate source (TR3)
Battery Charger seeks alternate source (#2 main bus)

Front 27

What is powered by the HOT BAT BUS?

Back 27

Battery bus controller
Entry lights dim
Standby horizon
APU starter motor
Fuel shutoff valve
Extinguisher discharge

Front 28

What is powered by the BATT BUS?

Back 28

Fire and overheat protection
Master caution and CAP lights
APU control unit
Start valves for engines
High ignition for start

Front 29

What 4 busses are powered if inflight and both generators are lossed putting you on battery power only?

Back 29

4 busses:
Hot battery, battery, standby AC, standby DC

Front 30

5 things that cause the generator control relay (GCR) to trip:

Back 30

Over/Under voltage
CSD disconnect
Over amperage
Generator Control switch moved to OFF
Fire Switch pulled

Front 31

3 things that cause the Generator Breaker (GB) to trip

Back 31

Over/Under frequency
Another power source
Generator Control Relay (GCR) trip

Front 32

What is the power source for the engine ignition?

Back 32

Battery Bus

Front 33

The autopilot will only track navigation signals from which source?

Back 33

The #1 VHF NAV RADIO

Front 34

Which conditions would require an engine start to be aborted?

Back 34

No N1 rotation by 20% N2
No oil pressure increase in 30 seconds
Fuel flow grater than 1100 PPH at start
No increase in EGT 20 seconds after start lever moved to IDLE
EGT rapidly approaching or exceeding the start limit.

Front 35

When is the standby hydraulic system LOW QUANTITY light armed?

Back 35

ALWAYS

Front 36

The FLT/GND switch on the cabin pressure controller operates in which modes?

Back 36

AUTO and STBY

Front 37

Does the yaw damper disengage when the B system flight control switch is moved to STBY rudder?

Back 37

YES

Front 38

If the STBY PWR OFF light illuminates in flight, what does this mean?

Back 38

That the AC stby bus is NOT powered.

Front 39

Max TR load (with cooling)

Back 39

65 amps

Front 40

Max TR load (without cooling)

Back 40

50 amps

Front 41

TR voltage range

Back 41

24-30 volts

Front 42

Max N1% and N2%?

Back 42

N1: 102.4%
N2: 100.0%

Front 43

What is the ignition duty cycle in FLT?

Back 43

2 min on, 3 min off
2 min on, 23 min off

Front 44

6 Things that 13th stage bleed air is used for?

Back 44

Wing anti-ice
Hyd Res A
Air Cond / Pressurization
Turbo fan
Engine starter
Water tank pressure

Front 45

5 things that trip the GCR (Generator Control Relay)?

Back 45

Fire warn switch
Over / under voltage
Gen control switch to OFF
CSD disconnect
Over amps

Front 46

Some things that make the air/mix valve drive full cold?

Back 46

Anytime pack valve closes
Duct Overheat light
Manually with temp selector

Front 47

How much fuel do the surge tanks hold? And where are they?

Back 47

30 gallons in each wing tip.

Front 48

Fuel quantity gauges are on what bus?

Back 48

Standby AC

Front 49

What 3 things trip the GB?

Back 49

Over/Under frequency
Gen control relay trips
Another power source connected

Front 50

What does the Gen Off Bus light indicate?

Back 50

The GB is open.

Front 51

What two things are shed with the loss of a gen bus?

Back 51

The galley power and B hyd elec pump are the first to be power shed.

Front 52

Using Engine TAI on the ground in icing conditions, you should run the engines up to what N1, how often and for how long?

Back 52

80% N1 for 15 seconds every 10 minutes.