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Boeing 737NG > B737-NG Oral Question > Flashcards

B737-NG Oral Question Flashcards

0
Q

What engine instruments are left on standby?

A

TBR

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1
Q

What do you have left when on standby power?

A

To be Reviewed

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2
Q

What engine instruments are self generating.

A

TBR

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3
Q

If start engine valve does not close, what do you do, and why?

A

TBR

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4
Q

What is the difference between LE flaps transit light on FWD panel and transit yellow lights on aft overhead panel?

A

Auto Slat indication?

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5
Q

With the flight recorder switch in NORMAL, when does the flight recorder operate?

On the ground?

In the Air?

A

On the Ground? Oil Pressure rise on first engine started

In the Air? Any time electrical power is available

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6
Q

What does the illuminated OFF light mean adjacent to the Flight recorder switch?

A

There is a Power Failure, Loss of Input Data or Electronic Malfunction, Test Failed

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7
Q

What are some of the things that the flight recorder moitors?

A

Altitude, Heading, Acceleration, Airspeed

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8
Q

Where is the flight recorder located?

A

Aft Cabin Ceiling

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9
Q

What does the crew oxygen gage indicate?

A

Pressure in the Crew Oxygen Bottle

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10
Q

What is the normal crew O2 pressure?

A

1,850 psi

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11
Q

What is the normal minimum crew O2 for pressure for dispatch.

A

Based on the table in Performance Inflight

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12
Q

Where is the crew O2 bottle located?

A

Aft end of the E&E compartment

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13
Q

How is the crew O2 bottle accessed?

A

Through the FWD Cargo Compartment, FWD Bulkhead Access Panel

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14
Q

What happens if the Crew O2 bottle becomes overheated and thermally discharges?

A

Loose oxygen from the bottle and the green disk (Right Side FWD Fuselage) will be gone. Pre-flight inspection Item

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15
Q

What kind of crew O2 do you get in normal operation of the crew mask?

A

Diluter demand (Air/O2 mix on demand)

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16
Q

What kind of crew O2 do you get when 100% is selected?

A

100% O2 on Demand

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17
Q

What kind of crew O2 do you get in EMERGENCY?

A

100% O2 under pressure

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18
Q

Where is the passenger O2 supply stored?

A

Each individual PSU unit.

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19
Q

With the switch in the guarded NORML position, when will the passenger O2 masks be presented?

A

When cabin altitude rises to approximately 14,000 feet

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20
Q

What is the function of the ON position of the PASS O2 switch?

A

Manually activates the pax oxy doors.

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21
Q

How many oxygen masks are connected to each generator?

A

4 at the passenger seats

2 at flight attendant’s station and lavatories

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22
Q

What is indicated by the PASS OXY ON light?

A

System is activated

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23
Q

With the PASS OXY ON light illuminated, what other light might you expect to see ON?

A

Auto Fail Light

MC Lights

Overhead Annunciator (Alt horn @ 10,000 feet cabin altitude)

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24
Q

When does the passenger O2 generator actually start to manufacture oxygen?

A

When the first mask (laniard) is pulled down on a specific bank of seats.

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25
Q

How long will the passenger O2 flow through the passenger masks, once activated?

A

12 min.

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26
Q

Can passenger oxygen be shut off after flow has started?

A

No

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27
Q

What can you do if a passenger oxygen mask compartment does not open when activated?

A

Manually open it with special tool.

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28
Q

Should passengers use oxygen when the cabin altitude is below 14,000 ft.? Why or why not?

A

No

Air is mix of O2 and cabin air.

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29
Q

What is available with the Service Interphone in the OFF position

A

Communication with the between the Flight Deck and Cabin

Flight Deck to Cabin
or
Cabin to Flight Deck

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30
Q

What is available with the Service Interphone in the ON position?

A

Connects all external jacks to the interphone system

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31
Q

With the Service Interphone switch in the OFF position, is communication between flight deck and cabin possible?

A

Yes

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32
Q

Is there an exterior service interphone switch? Where?

A

No

There is an external flight interphone jack located on the external power panel.

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33
Q

What does PSEU stand for?

A

Proximity Switch Electric Unit

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34
Q

What does the PSEU monitor

A

Air/Ground sensors

Configuration status/alerts

Overwing exit locks

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35
Q

When is the PSEU light inhibited?

A

When in flight (takeoff power set to 30 seconds after landing)

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36
Q

Should you be concerned with the PSEU light if it is illuminated on the ground?

A

Yes

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37
Q

Should you be concerned with the PSEU light if it illuminates during recall?

A

No, if it will cancel by pushing the MC light it is okay to go.

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38
Q

Are there any limitations on use of the windshield wipers?

A

Do not operate on a dry windshield.

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39
Q

Why is it important to not use the wipers on a dry windshield?

A

Will destroy rain repellant coating.

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40
Q

What sort of rain repellant system do we use?

A

Rain repellant like Rain-X

41
Q

In the ARMED position, when will the emergency lights come on?

A

With the loss of DC bus 1 or AC power is turned off.

42
Q

What do the emergency lights illuminate?

A

Aisle lights, extry/exit lights, escape path lighting, dome light, locator signs, area lighting, exterior area lighting

43
Q

Where is the other Emergency Light switch located

A

The aft flight attendant’s panel

44
Q

Will the aft flight attendant panel Emergency Light switch override the cockpit switch?

A

Yes

45
Q

What cockpit light(s) are controlled by the emergency light switch?

A

Flight Deck Capt. dome light

46
Q

What does the blue light on the audio control panel indicate?

A

Ground or cabin is trying to call

47
Q

Can you call personnel on the ground?

A

Yes

48
Q

How is contacting ground personnel accomplished?

A

Thru the use of the ground call button and nosewheel well horn.

49
Q

Where is the CVR circuit breaker located?

A

Behind the Captain’s seat

50
Q

When does the CVR start recording?

A

Anytime 115v AC is applied to the Aircraft

51
Q

How long is the CVR recording?

A

120 min. Data is auto erased after 120 min.

52
Q

How do you erase what is on the CVR?

A

Must be on the ground, parking brake set, hold button for 2 sec.

53
Q

What is unique to the EQUIP door light?

A

It is the only one that has two doors associated with it.

54
Q

What does the Lights test position do?

A

It illuminates (at full bright) all system lights on center pedestal, overhead panel and most lights on instrument panel.

55
Q

Which NAV modes will display TCAS traffic?

A

Map, Center Map, VOR or APP modes

56
Q

What does a TA look like?

A

solid amber circle

57
Q

What does a TA look like?

A

Solid red squar

58
Q

What does pitch guidance on the PFD look like during an RA

A

Restrictive Red bands. (like a rectangle)

59
Q

What does the vertical speed guidance on the IVSI look like during an RA?

A

Red - do not fly to / Green - fly to markings

60
Q

In the TA/RA mode when is the RA inhibited?

A

Stall
Windshear
GPWS
Less than 1,000 ft RA

61
Q

What are the sources of bleed air?

A

Engines, APU, and Ground Air

62
Q

What is bleed air used for?

A

Anti-ice, Pressurization, Airconditioning, Pressurization of Hyd systems and water system, Engine Start, and Aspirated TAT probe if installed.

63
Q

What is indicated by the illumination of the DUAL BLEED light?

A

APU bleed is on with #1 Eng bleed on, or APU bleed on with #2 Eng bleed on and Isolation valve open.

64
Q

What would cause an Engine Bleed tripoff?

A

Excessive Pressure or Temperature

65
Q

How does the Isolation Valve work in AUTO?

A

The valve is closed when all engine bleeds and pack switches are on.

66
Q

What would cause a L WING BODY OVERHEAT light to illuminate?

A

A leak in the left side duct (eng. strut, wing leading edge, air conditioning bay, keel beam, or APU duct.

67
Q

What would cause a R WING BODY OVERHEAT light to illuminate?

A

A leak in the R side duct system (eng. strut, wing leading edge, Air Conditioning Bay)

68
Q

Can a BLEED TRIP OFF be reset?

A

Yes

69
Q

Can a WING BODY OVERHEAT be reset?

A

No

70
Q

Equipment cooling is for the most part automatic. When would you have to interact with the system?

A

When the OFF light illuminates

71
Q

What does the Equipment Cooling OFF light indicate?

A

Loss of air flow due to fan failure.

72
Q

How many supply fans are there? How many exhaust fans are there? (for equipment cooling)

A

Two and two

73
Q

Where is the equipment exhaust air drawn from?

A

Flight Deck Displays, Overhead and AFT electronics panels, circuit breaker panels, and the E&E bay.

74
Q

Where is is equipment cooling air exhausted?

A

The Overboard Exhaust Valve when open.

or

The Outflow Valve when the OEV is closed

75
Q

If a supply or exhaust fan should fail when on the ground, what indication would you get?

A

MC light with an Overhead annunciation and a nosewheel well horn.

76
Q

Is a single PACK capable of supplying all of the air conditioning and pressurization requirements of the airplane.

A

Yes

77
Q

What is indicated by a PACK light?

A

Pack trip (overheat) or dual controller failure

78
Q

When would you get HIGH FLOW if both packs were in AUTO?

A

Both engine bleeds off and APU bleed on

79
Q

If on downwind at 5 flaps and you had a pack 2 fault, would the remaining pack go to HIGH FLOW?

A

No not with flaps out

80
Q

Is it recommended to operate two packs from a single bleed?

A

No

81
Q

When would it be feasible? (to run two packs from a single bleed)

A

On the ground with the APU

82
Q

What sort of flow does the APU produce when a pack is in HIGH on the ground?

A

Max Rate

83
Q

What is indicated by a CONT CAB zone temp light?

A

Duct Temp Overheat or Dual Controller Failure

84
Q

What is indicated by a FWD CAB zone temp light?

A

Duct Temp Overheat

85
Q

What is indicated by a AFT CAB zone temp light?

A

Duct Temp Overheat

86
Q

Ca the AFT CAB zone temp light be reset?

A

Yes

87
Q

If both the primary and secondary controllers for a pack fail, will the pack continue to operate?

A

Yes

88
Q

Why would the engineers design an air conditioning system that is so seemingly difficult to understand?

A

to make is simple to operate

89
Q

When you move a zone temperature control up, what are you asking the system to do?

A

Add warm trim air (Bleed air)

90
Q

What do recirculation fans do?

A

Reduce pack workload and bleed air demand (which saves fuel)

91
Q

How would you achieve maximum cooling on the ground?

A

Packs on AUTO, APU bleed open, and Engine bleeds closed.

92
Q

Which windows do the air vent controls defrost?

A

1 windows only

93
Q

What is the max differential pressure?

A

9.1 psi

94
Q

What is indicated by the AUTO FAIL light illuminated by itself?

A

Dual Controller failure

95
Q

What is indicated by an AUTO FAIL light and the ALTN light?

A

Single controller failure

96
Q

What is indicated by the OFF SCHED DESCENT light?

A

Aircraft descended prior to reaching (within .25psi) cruise altitude

97
Q

What is the result of changing the FLT ALT setting after takeoff?

A

Inhibits the auto return feature

98
Q

How does the operation of the outflow valve in manual compare with the operations in AUTO?

A

its slower (20 sec. from full closed to full open)

99
Q

What would cause an AUTO FAIL light to illuminate?

A 
An excessive rate of cabin change (+/- 2000 fpm)
loss of DC power
Controller fault
Outflow valve problem
High cabin pressure (>8.75 psi)
High cabin altitude (15,800 ft)
100
Q

What does the HIGH ALT LDG Option Switch do?

A

Reprograms the initiation of the cabin altitude warning horn from 10,000 ft to 12,500 ft

Boeing 737NG (5 decks)

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