Mod 7-8-9-10 Flashcards

(105 cards)

1
Q

What are the two primary services that the APU provides to the operation of the aircraft?

A

electrical power and pneumatic air

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2
Q

What normally provides the power for APU operations?

A

Gas Turbine Engine

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3
Q

The CL-215 utilizes what for electrical power on the ground?

A

GPU & Battery

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4
Q

What precaution must be observed when servicing an APU ignition unit?

A

Wait for capacitors to discharge

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5
Q

This device provides the correct amount of fuel to the fuel nozzles for correct operation

A

Fuel Control Unit

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6
Q

What is used to start the APU?

A

DC electric motor

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7
Q

List four things that the cooling air is used for on the APU

A

Generator, Lubrication System, Accessories, Exhaust Shroud

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8
Q

Modern APUs operations are _________________ with the starting, running ad shutdown done by the APU Controller

A

automatic

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9
Q

These two inspections are commonly checked on APU’s

A

Oil Quantity, APU Hours

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10
Q

What is the maximum altitude that we can use APU bleed air for pressurization?

A

15,000

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11
Q

Which of the following has a door that’s closed when the APU is not in operation?

A

APU Intake

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12
Q

How many turbine stages are in the APU?

A

2

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13
Q

How many switches need to be pressed by the pilot to start the APU?

A

2

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14
Q

How does the pilot control the speed of the APU? Throttle lever Power Output Lever Ignition Transducer Control None of the above

A

non of above

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15
Q

How is the APU shutdown?

A

by deselecting the START/STOP switchlight by pressing the APU FIRE PUSH switchlight by pushing an APU emergency stop button

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16
Q

Where is information about the APU displayed to the pilot?

A

EICAS

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17
Q

The APU will automatically shutdown in flight if:

A

the APU speed is too high

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18
Q

What must a multi-tank, gravity fed fuel system for a carbureted engine have?

A

interconnected vents

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19
Q

What must a multi-tank, pump fed fuel system for a carbureted single-engine plane have?

A

redundant fuel pumps

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20
Q

Which engine type uses an accumulator tank in its fuel system?

A

fuel injected piston engine

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21
Q

The electric pump in a piston engine fuel system is used for

A

priming the engine starting the engine redundancy

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22
Q

The crossfeed valves in a fuel system is to allow:

A

any engine to use fuel from any tank

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23
Q

Large aircraft fuel systems employ ______________ refueling.

A

single point

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24
Q

what type of fuel tank Can develop leaks if left to dry out

A

bladder

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25
fuel tank that Can be removed or installed through a small opening.
Bladder
26
fuel tank Hardest to repair
integral
27
fuel tank Also known as collapsible.
bladder
28
fuel thank that has the Best use of available volume
intergral
29
fuel tank Lightest weight.
integral
30
fuel tank that uses clips, snaps, or lacing to secure in airframe
bladder
31
fuel tank that is Difficult to remove and install
Rigid/Metal (welded or riveted)
32
fuel tank type that Requires large openings to remove
Rigid/Metal (welded or riveted)
33
The fuel cell in the Piper Navajo is secured to the structure using:
Lacing
34
All aircraft tanks can be easily defined as either rigid metal, bladder or integral.
false
35
Allows left engine to use fuel from right fuel tanks.
Crossfeed Valve
36
These remote valves are fast acting valves.
solenoid valves
37
A solenoid valve uses a _____________ valve internally.
poppet
38
Whittaker valves are also known as
gate valves slide valves motor driven valves
39
A _______________ is an example of a single acting manual pump
primer
40
This pump outputs fuel on each stroke of the piston
double acting pump
41
This pump outputs fuel on one stroke of the piston and pulls fuel into the pump on the other stroke
Pulsating pump diaphragm pump single-acting pump
42
This pump has no moving parts
ejector pump
43
Fuel strainers are normally located in the lowest point of the fuel system:
to collect water
44
The difference between a fuel filter and a fuel screen is:
filters have a mesh size of under 40 microns and a screen is over 40 microns
45
finger strainers are usually found in
fuel tanks
46
The cause of the British Airways Flight 38 crash was
ice forming in fuel/oil heater exchanger.
47
At what temperature is ice formation in jet fuel a problem?
Between -8 and -20 degrees Celsius
48
The pump image shown is in what mode?
Pressure relief
49
What are the four parameters that we typically monitor on aircraft fuel systems?
quantity, flow, temperature, pressure
50
Drip sticks are used to determine fuel quantity
on the ground
51
Float type fuel gauges can operate without ?
electric power
52
capacitance type fuel gauges measures?
measure the dielectric value of the fuel and air
53
What are three advantages of the capacitance-type fuel quantity indicators?
more accuratre, measures fuel mass, no moving parts
54
Volume flow measurement is done using a
a transmitter with a movable vane
55
Mass flow measurement is done using a
a transmitter with an impeller and turbine
56
the Cessna 185 fuel flow measurement is done using a
fuel pressure gauge
57
Fuel temperature indication is usually found on
any aircraft using jet fuel
58
how many fuel tanks are installed on the Boeing 767
3 main and 2 surge
59
The Boeing 767 uses what type of tank
fuel cells
60
Main fuel tanks on the Boeing 767 vent to
the surge tanks
61
The Boeing 767 is equipped with a fuel jettison system true or false
true
62
Where is the fuel temperature taken from on the Boeing 767?
left tank
63
Visual fire detection is part of
smoke detection
64
When a lithium battery burns, its classed as a
Class D fire
65
When an electric wire burns, its classed as a
class C fire
66
An ionizing smoke detector uses
radioactive material
67
thermal switch is wired in series or parallel
wired in parallel
68
thermocouple is wired in parallel or series
series
69
A ______________ detects the light emitted from a flame
Flame detector
70
Your home should be equipped with a
Ionizing smoke detector
71
This heat detector uses two conductors in a metal tube
Kidde
72
These four indications are used to detect a fire on board an aircraft
smell, smoke, heat, flame
73
Dry chemical extinguishing agents are used in which kind of aircraft fire extinguishers?
Dry chemical is not used on aircraft
74
What three things should be checked on a fire extinguisher during an inspection
installation hydrostatic test date amount of charge
75
Water is used in which kind of aircraft fire extinguishers?
Lavatory fire extinguishers
76
If the (red/yellow)\_\_\_\_disk is (missing/intact) \_\_\_\_\_then the HRD bottle has been emptied through the pressure relief valve. If the (red/yellow)\_\_\_\_\_\_disk is (missing/intact) \_\_\_\_\_\_then the HRD bottle has been discharged normally through the firing of the squib.
red,missing,yellow, intact
77
In an airline HRD system, each engine/APU has a dedicated HRD bottle. true or false
false
78
What should be done to prevent the accidental firing of an HRD system squib when not installed?
Squib terminals should be grounded.
79
What conditions will cause the master warning light to illuminate and the fire bell to activate on the Boeing 767?
When a fire signal is detected from either of the engines, APU, Cargo Compartment or wheel wells
80
Where is the APU remote control panel located on the Boeing 767
On the nose gear
81
What type of heat sensor is used for the engines on the Boeing 767?
Kidde or Systron-Donner dual loop sensor
82
What are the overheat sensors used for on the Boeing 767
Bleed air pneumatic leaks
83
How many engine fire bottles are normally carried on the Boeing 767
2
84
How is a fire extinguished in the wheel well of a Boeing 767?
The main landing gear is lowered in flight
85
Most airplanes have some form of ice protection, even those flying Day VFR
yes
86
If an airplane is certified for IFR operations, then it is good to fly in known icing conditions. true or false
false
87
What forces acting on a plane are negatively impacted by icing?
weight drag thrust
88
type of icing that is Roughest form of ice causing the most drag
rime ice
89
Heaviest type of ice
Glaze Ice
90
Hardest ice to clear off the plane
glaze ice
91
Easiest for of ice for de-ice boots to remove
rime ice
92
Can forms in clear conditions when temperatures are below freezing.
frost
93
(Anti-ice/De-ice)\_\_\_\_\_\_systems are designed to remove ice after it has formed. (Anti-ice/De-ice) \_\_\_\_\_\_systems are designed to prevent the formation of ice from occurring.
de-ice / anti-ice
94
Ice doors on the King Air should
be used to prevent foreign object damage to the compressor section of the engine
95
Propeller de-ice boots are operated
using DC electric power
96
what kind of fuel distribution is this and what must have?
* Single Engine * High Wing * GravityFeed –Some still use a fuel pump •Interconnected Vent (Must have)
97
what kind of fuel distribution is ?
Pump Feed Single Engine –Electric and Engine Driven Pumps * In parallel * Electric pump for starting and backup –Plunger Type •Engine driven pump used when engine is running Diaphragm type Carbureted Primer
98
what kind of fuel distribution is this ?
* Fuel Injected–With primer * Single Engine–Electric and Engine Driven Pumps * Vane type * In parallel * Electric pump for starting and backup * Engine driven pump used when engine is running
99
what kind of fuel distribution is this?
•Fuel Injected –No primer •Multi Engine –Crossfeed •Common fuel feed from each wing
100
What kind of fuel distribuition is this?
•Transport Aircraft• Multi Engine •Single Point Refueling –Over wing refueling still available •Crossfeed –Any tank to any engine •Dump –To reduce weight allowing for emergency landing •No Inflight Transfer –A few large aircraft can transfer fuel in flight –Many large aircraft can transfer fuel on the ground
101
Fuel System Operational Checks
fillin,draining, supplying,transfering,crossfeding,dumping
102
fuel system ATA
ATA 28
103
what kind of Fuel Selector is? that must be pushed off of a seat by cam act
poppet
104
what kind of selector valve is this
cone
105
what kind of selector valve is ?
Slide or gate: Whittaker Valves