Exam 3 Flashcards

(79 cards)

1
Q

First air to air fueling

A

Nov 12 1921
Wesley May

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2
Q

First plane to plane refueling

A

June 27 1923
Capt Lowell Smith
Lt. John P Richter

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3
Q

fuel system purpose

A

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

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4
Q

how aircraft fuel needs to be delivered

A

uniform flow
clean fuel
constant pressure
delivered at various altitudes and attitudes
delivered in any reasonable maneuver

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5
Q

fuel system must be able to monitor

A

quantity of fuel
fuel pressures
fuel temperatures
fuel flow rates

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6
Q

When do aircraft fuel indicators have to be accurate

A

only when empty

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7
Q

what must the reliability of fuel systems be

A

not result in power interruption for more than 20 seconds for piston engine
will not cause flame out for turbine engine

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8
Q

independence of aircraft fuel systems

A

each tank should be able to feed each aircraft engine

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9
Q

gravity fed system

A

bottom of tank must be high enough to provide enough pressure
uses gravity to cause fuel flow

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10
Q

advantage of gravity fed system

A

“both” option takes fuel from both wings equally

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11
Q

primer

A

subsystem
on non fuel injected aircraft
draws fuel from carburetor inlet bowl or fuel strainer

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12
Q

pressure feed system

A

uses boost pump to move fuel
fuel tanks too low to provide fuel pressure
wing tanks same level as carburetor

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13
Q

fuel pumps in pressure feed

A

fuel boost pump - starts engine
engine driven pump - normal operation

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14
Q

bladder fuel tank downside

A

want to make sure always full
needs to be replaced every 15 years

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15
Q

integral fuel type

A

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

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16
Q

bladder fuel tank

A

rubberized synthetic bag manufactured to conform to space in wing
uses aircraft structure to support weight of fuel

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17
Q

purpose of grounding during aircraft fueling

A

fuel flowing in lines create static charge build up
prevents static discharge and potential explosion in fuel system

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17
Q

Jettison System

A

dumps fuel overboard in event of emergency to lower weight to landing weight

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18
Q

when is a jettison system needed

A

if max TO weight is greater than 105% certified landing weight

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19
Q

what does fire protection include

A

fire detection
fire control

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20
Q

Class A compartment

A

crew and pax
visually detected
reached, combated by flight crew

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21
Q

Class B Compartment

A

cargo and baggage
must have sufficient access to enable crew member to reach all parts of compartment effectively with a portable fire extinguisher while in flight

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22
Q

What use class A and B be equipped with

A

smoke detector or fire detector

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23
Q

Class C compartment

A

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

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24
Class D Compartments
inaccessible cargo and baggage no fire detection designed so fire will be confined to that area
25
what must all classes of compartments have
ventilation must be controlled
26
Class E compartment
cargo aircraft no windows, special shades fire resistant must have smoke/fire detector able to shut off flow to compartment controllable from flight deck able to isolate smoke, flames, gases from flight deck
27
Spot detectors
monitor one specific location produces current when heated
28
continuous loop detector
monitors greater area ceramic changes resistance with heat, more current flow = detection
29
smoke detection purpose
deter smoke present in a specific zone
30
photoelectric cell smoke detector
air sampled. if 10% visible smoke particles, the light sensor sends electrical signal to the warning system controller
31
ion detector smoke detector
smoke is ionized gas detector samples air, if air contains smoke - slightly less electrically conductive
32
class A fire
paper, wood, cloth, trash
33
class B fire
flammable liquids
34
class C fire
electrical equipment
35
class D fire
certain metals magnesium, titanium
36
Class A extinguisher
water type breaks heat ineffective, potentially dangerous in other classes
37
how do fire extinguishers work
one of the legs of the fire triangle must be broken
38
Foam extinguisher
class A and B removes oxygen leg
39
Carbon Dioxide extinguisher
B and C type takes away oxygen and heat
40
B and C type problems
ineffective for A easily blown away ineffective in ventilation
41
Dry chemical extinguisher
A, B. C type most common barrier between oxygen and fuel coats surface to prevent re-ignition
42
(B777) Loop overheat detection causes:
master caution lights on caution aural operates engine overheat caution message shows
43
(B777) engine fire detection causes:
master warning lights on fire warning aural operates engine fire warning message shows engine fire warning light on fuel control switch fire warning light on
44
What does the engine fire switch do
gives indication of engine fire stops engine isolates engine controls engine extinguishing system
45
electric ice detection
Probe mounted on front of AC vibrates at specific frequency Ice forming on probe changes frequency of vibration which causes light to illuminate in cockpit
46
Hawker ice detection
rotary cutter ice detection rotates if ice builds up, gets scraped off and sensed torque increases
47
windshield anti-ice
heated windshield windshield fluid
48
how are engines protected
heated with bleed air or electric coils
49
how is rain removed
windshield wipers chemical repellents combination pneumatic rain removal
50
difference between new and old EIS/EFIS
old - only display information for flight instruments new - flight instruments, aircraft systems, engine, warning/caution
51
what is EICAS / ECAM
engine alerts and aircraft monitoring systems
52
FAR for fire requirements 14CFR25?
Immediate awarning of fire or overheat Accurately indicate extinguished fire Durable and resistant to damage Include accurate method to test integrity of system Unlikely to have false indication Require minimum electrical power
53
Halon type fire extinguisher
air extinguisher removes oxygen
54
who is ECAM
airbus
55
who is EICAS
boeing embraer canadair
56
EICAS displays information all the time
no display on need to know basis
57
EICAS primary mode
main display during normal operation
58
EICAS secondary mode
on auxiliary EICAS display N2 speed, fuel flow, oil pressure, oil temp, oil quantity, engine vibration
59
EICAS compact mode
when display is inactive or used to show maintenance pages only display digital data format
60
Level A message
warning red aural, visual alert immediate action / attention
61
Level B message
caution amber visual, different aural crew awareness and future action
62
Level C message
advisory amber or light blue crew awareness and possible action
63
Level D message
memos white
64
PFD
replaced EADI most critical display
65
navigational display, ND
weather navigational info can change format
66
MFD
FO access checklist, info, nav maps
67
advantage of 3rd gen EIS
increased integration larger display weigh less less power needed
68
can the CVR (black box) be used for any other reason other than for accident/incident investigation
no
69
what is the cvr
cockpit voice recorder (part of the) black box audio monitor only
70
how long must the CVR record for
at least 120 minutes
71
where is the CVR located
empennage of plane maximizes likelihood of survival heat-resistant orange paint, high visibility
72
new CVR advantages
solid state memory and digital more resistant to shock, vibration, moisture have internal battery and can continue without electric power
73
how does an underwater locater beacon work
self contained unit actives frequency when submerged in water
74
when is CVR required
Any multi-engine turbine powered aircraft with 6 or more passenger seats must have a CVR if 2 pilots are required for operation
75
how long can the FDR record for
25 hours 1000 parameters
76
what can the FDR withstand
3400Gs impact 1100 C for 30 minutes fire 20,000ft submergence
77
when must an FDR be installed
multi-engine turbine powered aircraft with 10 or more passenger seats must have a flight data recorder
78
do the archer's have an FDR?
any Garmin 1000 airplane has an FDR capability