Unit 3 Flashcards

1
Q

Measure of the force in an electrical system that causes current flow; measure of EMF

A

voltage

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2
Q

typical voltage

A

12V or 24V

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3
Q

Measure of electricity through a conductor

A

current

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4
Q

unit of current

A

amps

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5
Q

end of battery that electrons are attracted to

A

positive terminal

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6
Q

unit of resistance

A

ohm

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7
Q

what is resistance?

A

the “friction” an electron encounter as it flows
EMF must be required

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8
Q

which of the following best described the contributing factors to thermal runaway in a nickel-cadmium battery installed in an aircraft?

A

low internal resistance intensified by high cell temperatures and a high current discharge/charge rate in a constant potential charging system

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9
Q

what do rectifiers do

A

AC to DC

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10
Q

what do rectifiers have

A

transformer, stack, and cabinet

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11
Q

what do inverters do

A

increase DC voltage, then DC to AC

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12
Q

how is electrical energy transferred from one circuit to another without any connections?

A

induction

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13
Q

how is the voltage output of an alternator regulated?

A

controlling the voltage output of the DC exciter
solid state transistor and a “zener diode” to regulate voltage

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14
Q

purpose of circuit breakers

A

designed to protect the circuit from damagingly high levels of current flow

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15
Q

tell me about DC

A

single direction
constant polarity
changes magnitude when current turns on and off

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16
Q

tell me about AC

A

direction of current changes
easy to generate
easily stepped up/down with transformers

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17
Q

with an electromagnet, what affects the strength?

A

winding a coil around a soft iron core

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18
Q

where to find lead acid batteries

A

piston

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19
Q

NiCad CONS

A

low internal resistance
long life
expensive
prone to thermal runaway

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20
Q

where to find NiCad batteries

A

turbine

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21
Q

what is useful load

A

crew, usable fuel, passengers, and cargo

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22
Q

independent braking system

A

pressure only as great as foot pressure applied

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23
Q

boosted brakes

A

actuating system that augments force with hydraulic pressure

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24
Q

aircraft with boosted brakes

A

medium to large aircraft that do not require a full power system

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25
power brakes
use hydraulic system as source of power to apply the brakes
26
aircraft with power brakes
large and high performance aircraft
27
expander tube brakes
1930s-1950s lightweight, low-pressure brakes
28
single disc brakes
friction to both sides of disc
29
aircraft with single disc brakes
small, light aircraft
30
aircraft with multiple disc brakes
large, heavy
31
aircraft with segmented rotor
high performance
32
purpose of torque links
wheel alignment movement prevents over extension
33
function of oleo strut
absorbs shock of landing with hydraulic fluid
34
when an air/oil type of landing gear shock strut is used, the initial shock of landing is cushioned by
the fluid being forced through a metered opening
35
purpose of chines
deflect water away from fuselage
36
types of hydraulic fluid
vegetable base mineral base synthetic, phsophate-ester
37
color of veggie base
blue
38
color or mineral base
red
39
color of phosphate- ester
purple clear
40
vegetable base hydraulic fluid
least used oldest
41
mineral hydraulic fluid
common in most aircraft
42
phosphate-ester hydraulic fluid
skydrol fire resistant used in WW2
43
how is fuel flow measured in fuel-injected engines
measure the pressure drop across the fuel injector nozzles
44
what does a manifold pressure gauage indicate
absolute pressure inside induction system
45
what does engine pressure ratio measure
differential pressure between tailpipe total pressure and compressor inlet total pressure
46
how does a turbine tach indicate
reads RPM of low compressor and high pressure, and gives a percentage
47
what is the purpose of an EGT gauge
measures the temperature of the exhaust gas indicates combustion efficiency
48
monocoque
hardly any internal framework
49
semi-monocoque
internal arrangement of formers and stringer to provide additional rigidity and strength to the skin
50
airfoil
shape of wing at any cross section
51
angle of incidence
determined by manufacturer angle between chord line and reference axis
52
center of lift
point where lifting forces are concentrated
53
center of gravity
point where weight forces are concentrated
54
CG and CP relationship
CG forward of CP
55
stall strips
cause wing to stall in non-critical locations before it normally would
56
servo tabs
small-hinged device installed to assist movement
57
relationship between alternator and battery
alternator spins and creates electricity for the battery
58
seminole circuit breaker popping
tripped circuit breakers should be reset only if the affected system/component is considered essential for safety of flight
59
voltage and amperage
two belt driven 28V, 65 amp alternators 13.6 amp-hour, 24V battery
60
stops flow of current to the gear pump on the Seminole when on ground
squat switch
61
stops the flow of current to the gear pump when gear is fully retracted
pressure switch
62
"CHECK GEAR" CAS message causes
- gear not down and locked and manifold pressure below 14" - gear position UP and airplane on the ground - gear not down and locked and flaps are extended 2/3rd notch
63
empennage of Seminole
vertical stabilizer all-moveable horizontal stabilator rudder
64
flaps on Seminole
flaps on wings anti-servo tab mounted on trailing edge