Airplane General Flashcards

1
Q

What will cause the emergency exit lights to illuminate when armed?

A

Loss of AC power OR loss of DC Bus 1 SH 1.040 PG 45

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2
Q

Are there any limitations on an aircraft with retractable landing lights?

A

There is no speed restriction for operation of the lights.
SH 1.030 PG 30

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3
Q

What do each of the exterior lights illuminate? Where are they and what do they do*

A

Landing Lights (wing root) - shines straight ahead
Taxi - (nose or wing root) - shines straight ahead
Runway Turnoff - shine out at 45 degree angle (not forward facing)
Logo (on the tail) - Chester
Strobe (wings and tail) - strobe lights
Anti-collision (belly and roof) - red beacon
Position (wingtips) - nav lights
Wing lights (fuselage) - illuminates leading edge of the wing for inspection Wheel well (nose and main wheel wells) - illuminates wheel wells
SH 1.030 pg 33

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4
Q

When is 100% supplied to the flight deck oxygen masks?

A

Any time the switch is in the 100% position SH 1.040 PG 11

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5
Q

What triggers the MASTER CAUTION (amber) lights? What triggers the associated System Annunciator lights?
MASTER CAU

A

MASTER CAUTION = caution outside pilots’ normal field of view SH 1.030 PG 3

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6
Q

What causes the MASTER CAUTION and System Annunciators to Extinguish?

A

A Master Caution Reset (pushing the light)
A Master Caution Reset is accomplished by pushing either MASTER CAUTION light. This resets the Master Caution System and results in
- Both MASTER CAUTION lights extinguishing
- All system annunciator lights extinguishing, and
- The Master Caution System is reset for further cautions
The caution light on the overhead panel remains illuminated until the caution condition no longer exists (except for single / simple faults)
SH 1.030 PG 4

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7
Q

What is the difference between single and dual channel systems? How are system indications different for single channel vs dual channel systems?

A

Dual channel = redundancy within system
Single channel = no redundancy within system
Dual channel system loses a single channel? No caution light, only found by recall and is stored in the Master Caution system - it won’t tell you!
Single channel system fails? You will have an annunciator - it will tell you!
SH 1.030 PG 4-5

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8
Q

What is the light logic of the aircraft?

A

RED = Immediate
AMBER = Timely
Dim blue = Status light (correct position)
Bright blue = Status light (in transition or disagreement)
Dark aircraft concept - normal conditions in flight = no lights (mostly) SH 1.030 pg 1

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9
Q

How are the 6 Flight Deck windows different from each other? Which ones open?

A

R1/L1 and R2/L2 are heated. R2/L2 open. R3/L3 not heated and does not open. FO side (R2) window opens from the outside.
See Figure 5 in the SH 1.030 PG 11

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10
Q

What is the Flight Deck Access System (FDAS), and how does it operate?

A

Provides flight crew with full control of the flight deck door during normal operations.
- Automatically locks under DC power
- Manual control with deadbolt and FDAS switch
- Emergency code for access in case of pilot incapacitation
Flight deck door lock panel annunciators:
LOCK FAIL = lock selector in AUTO and lock has failed or FDAS switch is OFF

AUTO UNLK = correct access code entered, flashes and aural chime alert
After correct code entered into keypad, 60 second timer and: Two chimes each 20 seconds and steady (40 sec) Last 20 seconds are continuous chime and flashing
Flight crew can select DENY = locks out the keypad for 5 minutes
Selector spring loaded to AUTO. UNLK will unlock door as long as selector held in position.
SH 1.030 PG 17-18

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11
Q

How is the Passenger Oxygen system actuated and how long does it supply oxygen?

A

Automatically - cabin pressure of 14,000ft Manually - PASS OXYGEN switch ON
12 minute supply of oxygen
SH 1.040 pg 23

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12
Q

Which systems can pressurize the Potable Water System and what conditions must be met for it to operate?

A

Bleed air from engines or APU
OR if insufficient bleed air, an AC electric compressor IF:
- pressure in the water tank is less than 30 psig (pressure limit switch is closed) - water service panel door is closed (compressor cut-out switch is closed)
- CAB/UTIL switch ON
SH 1.030 PG 40

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13
Q

Do the FAs have control of the Emergency lights? What priority do they have, if any?

A

Yes, they can override cockpit switch
Works even if flight deck switch is OFF or failure of automatic control with loss of power
SH 1.040 PG 46

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14
Q

Where are the water fire extinguishers and halon fire extinguishers?

A

Water fire extinguishers - Passenger cabin only Halon fire extinguishers:
- 1 behind FO seat mounted to CB panel
- 2 in pax cabin (1 forward, 1 aft, see fig 74) *2 in pax cabin required for
dispatch
SH 1.040 pg 28 and SH 1.050 pg 86

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15
Q

What do they contain, and what kind of fires are they effective on?

A

Water fire extinguisher
- Contains water mixed with antifreeze
- Effective on class A fires only (wood, fabric, paper, etc)
AUTO UNLK
AUTO UNLK

Halon fire extinguisher
- Contains 2.5 lbs of Halon at 100psi nitrogen charge
- can be used for all types of fires, but primarily class A+B electrical, fuel,
and grease fires
SH 1.040 pg 28

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16
Q

How are they pressurized, and how can you tell they are serviceable?

A

Water - pressurized by Co2 cartridge, trigger is safety wired
Halon - pressurized by nitrogen, gauge in green and pin in with red tie indicates it’s serviceable
SH 1.040 PG 30

17
Q

What causes the overwing emergency exits to lock?

A

The overwing exit locks engage when:
- Minimum 3 of 4 entry/service doors closed AND
- Either engine running AND
- Airborne OR thrust levers advanced
Any of the above conditions not met or loss of DC power? Unlocked
SH 1.040 pg 55

18
Q

What do the Emergency Exit Lights illuminate, and how are they powered? Activated?

A

Illuminate approved emergency exit routes (inside cabin) and evacuation areas (exterior)
- Powered by battery packs charged by AC power and the EMR EXIT Lights switch in OFF or Armed
- Activated manually by switch ON or automatically with loss of AC power or power to DC Bus 1
SH 1.030 pg 45