Exam 3 Final Review Flashcards

(73 cards)

1
Q

purpose of aircraft fuel system

A

deliver fuel to engines safely under a wide range of operational conditions

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2
Q

what should the aircraft fuel system monitor

A

quantity of fuel, check fuel pressures, temperatures, flow rates

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3
Q

Reliability of aircraft fuel systems

A

Piston: will not result in power interruption for more than 20 seconds
Turbine: will not cause flameout

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4
Q

fuel system independence

A

fuel system for one engine will not affect another engine
isolation of different fuel lines

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5
Q

gravity fed fuel system

A

uses force of gravity for fuel flow
has a both option

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6
Q

Pressure feed fuel system

A

uses boost pump to move fuel
tanks too low to provide adequate pressure

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7
Q

Fuel pump purpose

A

move fuel through fuel system when gravity flow is insufficient
provide positive pressure to eliminate vapor lock

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8
Q

Integral fuel tank

A

sealed with fuel proof compounds
wet wing
manufactured when aircraft is built

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9
Q

bladder fuel tank

A

rubberized synthetic bag
aircraft structure supports weight

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10
Q

fuel strain and filter

A

removes foreign materials from fuel system

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11
Q

what three points does a strainer strain from

A

bottom of fuel tank
lowest point in fuel system
near fuel control unit

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12
Q

fuel selector valve purpose

A

shutoff flow
select tank
transfer fuel
direct fuel

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13
Q

purpose of grounding (static bonding) during refueling

A

prevent static discharge and possible explosions

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14
Q

fuel sump vs fuel drain

A

sump: low point in tank for collection of water and sediment
drain: low point of sump for draining water and sediment

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15
Q

what is a cross feed system

A

supply any engine from any tank

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16
Q

what is the fuel jettison system

A

dumps fuel overboard in event of an inflight emergency

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17
Q

when is the jettison system required

A

when takeoff weight is greater than 105% of the certified landing weight

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18
Q

when are rigid fuel lines used

A

metal tubing
stationary applications where long and straight runs are possible

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19
Q

Class A fire compartment

A

crew and passenger area
fire may be visually detected, reached and combatted by flight crew

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20
Q

Class B fire compartment

A

cargo and baggage
access for a crew member to reach all areas and combat

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21
Q

what do both class A and B compartments have

A

smoke or fire detector

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22
Q

class C fire compartment

A

inaccessible compartments
fire detection/fighting done by remote sensors and fire control

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23
Q

class D fire compartment

A

inaccessible cargo and baggage
fire confined to area, crew may not know it is happening

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24
Q

class E fire compartment

A

cargo aircraft cargo area
Must have:
smoke/fire detector
shutoff air flow ability
controllability form flight deck
ability to isolate smoke or flames from flight deck

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25
Fire detection systems
spot: monitor one location, has thermocouple, produces current when heated continuous-loop: monitors greater area, ceramic changes resistance with heat
26
smoke detection system
photoelectric: samples for visible smoke particles ion: samples air for ionized gas (smoke)
27
Class A fire
paper, wood, cloth, trash
28
class B fire
flammable liquids
29
class c fire
electrical equipment
30
class D fire
metals
31
Water type extinguisher
class A fire removes heat leg
32
foam type extinguisher
class A and B fire removes oxygen leg
33
carbon dioxide extinguisher
type in most aircraft (Halon) takes away oxygen and heat legs class B and C fires
34
dry chemical extinguisher
class A, B, c fire barrier between oxygen and fuel
35
what is a squib
fired charge to set off a fire bottle
36
what happens when the fire handle is pulled
**ask in class wednesday**
37
what are the conditions needed for ice to form
freezing temperatures and visible moisture
38
what are the dangers of icing
frozen controls blocked pitot/static ports reduced lift added weight structural damage
39
ice detection systems
visual vibrating probe rotary cutter
40
What is anti-icing vs deicing
anti: prevents formation of ice deice: removes ice already formed
41
Anti-ice examples
engine bleed air electric heat fluid
42
deice examples
fluid boots
43
how do boots work
inflation tubes inflate and break off ice inner tube first than outer tubes may cause "bridging"
44
weeping wing / TKS fluid
AL-5 ethylene glycol isopropyl alcohol and water
45
rain control methods
windshield wipers chemical repellents pneumatic jet balset removal
46
what is the ADI and HSI
attitude director indicator horizontal situation indicator
47
what was the first jet passenger service
de Havilland Comet BOAC 1952
48
what does the ADI include
attitude indicator turn and slip indicator pitch and bank steering bars glide slope indicator warning flags
49
what does the HSI include
heading indicator course deviation indicator DME distance indicator
50
what were 1st gen EFIS
basic glass cockpit only flight instrument displays
51
How do 2nd and 3rd gen differ from 1st gen EFIS differ
2nd and 3rd gen have flight data airframe data engine data warnings/cautions
52
what is EICAS
boeing, ambraer, canadair need to know basis information
53
what is ECAM
airbus
54
EICAS Display formats
primary - main display, 4 levels messages secondary - auxiliary EICAS: N2, fuel flow, oil press/temp, oil quantity compact mode: when one display inactive or on maint pages
55
Level A ECAM
red warnings immediate attention and action
56
level B ECAM
amber caution immediate awareness, future action
57
level C ECAM
amber or light blue advisory immediate awareness, possible action
58
level D ECAM
white memos
59
PFD
primary function display basic flight information, display priority
60
ND
navigational display aircraft position navigational info weather, flight plans
61
MFD
multi-function display FO for checklists, maps
62
EFB classes
Class 1 - portable electronic device Class 2 - mounted in A/C Class 3 - permanently installed
63
HUD
heads up displays view critical flight instruments and ability to keep head up in flight eliminate transition time
64
CVR vs FDR
cockpit voice recorder flight data recorder both part of the "black box"
65
recording limit on CVR
120 minute limit
66
what aircraft require a CVR
any US registered multi-engine turbine powered aircraft with 6 or more passenger seats if 2 or more pilots are required for operation
67
when can the erase button be used
after a successful flight wheels on the ground engines are off
68
recording limit on FDR
25 hours
69
What aircraft must have FDRs
any multiengine turbine powered aircraft with 10 or more passenger seats
70
what information is recorded by an FDR
flight data attitude, altitude, speeds, etc
71
underwater locator beacon
underwater locating device attached to cockpit voice recorder and flight data activates when submerged in water 30 day operating capability
72
flight data recorder *crash withstandability*
3400Gs 1100C for 30 minutes submerged 20,000ft
73
why is a grounding cable used during aircraft refueling
to ensure the aircraft and fuel truck/tank are at the same electrical potential