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Module 11B > Memory > Flashcards

Memory Flashcards

1
Q

When Anodising, parts are ?

A
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2
Q

'’Hard’’ Anodising

A
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3
Q

Static Inverter

A
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4
Q

Primary bending loads of a Semimonoque fuselage is taken by?

A
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5
Q

Wing internal loads are taken by?

A
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6
Q

Box Beam Spar

A
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7
Q

Stabilator = ?

A
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8
Q

Standby power is accompanied with a ?

A
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9
Q

Balance tabs move in what direction relative to the control surface?

A
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10
Q

What type of structure is the Nacelle?

A
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11
Q

What is the purpose of the ACM?

A
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12
Q

Standby HSI recieves info from where?

A
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13
Q

Remote reading compass does what?

A
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14
Q

What is the range of VHF?

A
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15
Q

ADF feeds its relative bearing output to?

A
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16
Q

Middle marker beacon causes what in the cockpit?

A
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17
Q

VOR information is displatyed on what instrument?

A
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18
Q

ILS vertical information is recieved from ?

A
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19
Q

How is voltage output from an alternator regulated?

A
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20
Q

AC parallel power system has a Diff. current fault, what happens?

A
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21
Q

Max height above the floor for escape path lighting is?

A
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22
Q

Emergency exit hatches open inward or outward?

A
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23
Q

What is the Flight crew escape rope made from?

A
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24
Q

Class B fires occur where?

A
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25
Q

Which has the higher fueling rate, Over wing or pressure fueling?

A
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26
Q

Refueling pressure is ? (psi)

A
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27
Q

How does a Parallel generator system control field excitation current?

A
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28
Q

Decade box = ?

A
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29
Q

GPS
total?
Orbits?
MHz?
? required
? Radar band

A
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30
Q

TCAS
* Transmit frequency?
* Receive frequency?
* TA = (time)

A
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31
Q
A

3/ The up going aileron moves through a greater distance than the down going

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32
Q
A

2/ The left moves down and the right moves up

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33
Q
A

2/ Eliminate control flutter

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34
Q
A

3/ The aileron wheel and speed brake lever

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35
Q
A

3/ Is increased or decreased depending on the type of Trailing Edge flaps used

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36
Q
A

1/ Operate Symmetrically

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37
Q
A

3/ To make the flight control harder to move

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38
Q
A

3/ Greater than at subsonic speeds, but less than at transonic speeds

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39
Q
A

3/ Slowed down but still supersonic

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40
Q
A

1/ and 3/ both marked on answer sheet
Double check required

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41
Q
A

2/ A fail safe structure is one in which the limit load can still be met even though one of its elements has failed

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42
Q
A

1/ Crack limiting joints

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43
Q
A

2/ Selenious Acid solution

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44
Q
  1. During the Anodising process the parts to be treated form the:
    1/ Cathode
    2/ Anode
    3/ Electrolyte
A

2/ Anode

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45
Q
  1. During ‘hard’ anodising the electrolyte is:
    1/ Heated to a higher temperature than ambient
    2/ Cooled to a temperature well below ambient
    3/ Kept at a temperature similar to ambient
A

2/ Cooled to a temperature well below ambient

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46
Q
  1. The primary bending loads of a semimonocoque fuselage are taken by the:
    1/ Stringers
    2/ Frames
    3/ Longerons
A

3/ Longerons

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47
Q
A

2/ Frames

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48
Q
A

1/ Tensile

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49
Q
A

2/ the outer pane only

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50
Q
A

3/ Does not use any external load carriers

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51
Q
  1. The box beam spar is constructed of two main members with connecting:
    1/ Stringers
    2/ Frames
    3/ Bulkheads
A

3/ Bulkheads

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52
Q
  1. Wing internal loads are taken by:
    1/ Spars and stringers running chordwise
    2/ Spars and stringers running spanwise
    3/ Spars and stringers running diagonally
A

2/ Spars and stringers running spanwise

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53
Q
A

2/ Maintain the correct contour of an aerofoil’s covering

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54
Q
  1. A Box beam stabiliser construction has:
    1/ One main longitudinal member
    2/ More than one main longitudinal member
    3/ Two main longitudinal members with connecting bulkheads
A

3/ Two main longitudinal members with connecting bulkheads

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55
Q
  1. A stabilator is a:
    1/ Stabilizer and a rudder
    2/ Elevator and stabilizer
    3/ Elevator and rudder
A

2/ Elevator and stabilizer

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56
Q
A

1/ Spanwise member of an aerofoil

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57
Q
A

2/ Chordwise member of an aerofoil

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58
Q
A

1/ Stringers

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59
Q
A

1/ The counter clockwise moment must equal the clockwise moment

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60
Q
A

1/ Rudders, Ailerons, and elevators

61
Q
A

1/ To add weights tothe control surface

62
Q
A

1/ Mass balancing

63
Q
A

1/ Is a leading edge device

64
Q
A

2/ Pylon

65
Q
  1. An engine nacelle is classified as a:
    1/ Primary structure
    2/ Secondary structure
    3/ Auxilliary structure
A

2/ Secondary structure

66
Q
A

3/ Prevents engine fires from spreading

67
Q
A

1/ Provide engine thrust transfer to the airplane

68
Q
A

1/ Provide an aerodynamic enclosure for strut mounted engines

69
Q
A

3/ 8000 feet

70
Q
A

2/ Prevent cabin pressure from being lower than ambient

71
Q
  1. The purpose of the Air Cycle Machine in an Air Conditioning system is to:
    1/ Increase the temperature
    2/ Decrease the temperature
    3/ Increase the flow rate
A

2/ Decrease the temperature

72
Q
A

3/ To supply air for a temperature and pressure environment

73
Q
  1. Which aircraft instrumentation system would provide the pilot with essential navigation information to guide the aircraft to its destination?
    1/ EICAS
    2/ EFIS
    3/ ECAM
A

2/ EFIS

74
Q

An aircraft Standby Horizon Indicator will receive it’s pitch and roll information from:
1/ The No. 1 Vertical Gyro
2/ The left inertial Reference System
3/ Its own self-containing gyro

A

3/ Its own self-containing gyro

75
Q

In a Digital Stall Warning system the primary inputs required for operation are:
1/ Groundspeed, Flap Position and Engine Thrust
2/ Angle of Attack, Air Temperature and Engine Thrust
3/ Airspeed, Flap Position and Angle of Attack

A

3/ Airspeed, Flap Position and Angle of Attack

76
Q

Remote reading compass systems normally feed which instruments?
1/ Standby Compasses and Radio Magnetic Indicators
2/ Attitude Director Indicators and Horizontal Situation Indicators
3/ Radio Magnetic Indicators and Horizontal Situation Indicators

A

3/ Radio Magnetic Indicators and Horizontal Situation Indicators

77
Q

The range of a VHF communication system is:
1/ Up to 40 Nautical miles
2/ Approximately 100 - 150 Nautical miles
3/ Beyond the Horizon

A

2/ Approximately 100 - 150 Nautical miles

78
Q
A

3/ Flight Compartment, Flight Attendants, Automatic Announcements, Boarding Music

79
Q

The ADF system on an aircraft would feed its relative bearing output to which instrument?
1/ Radio Magnetic Indicator
2/ Attitude Director Indicator
3/ Standby Horizon

A

1/ Radio Magnetic Indicator

80
Q

Which Marker Beacon ground station will cause the amber lights to illuminate in a cockpit?
1/ Outer Marker
2/ Middle Marker
3/ Airways Marker

A

2/ Middle Marker

81
Q

VOR Deviation information is displayed on which cockpit instrument?
1/ Radio Magnetic Indicator
2/ Attitude Director Indicator
3/ Horizontal Situation Indicator

A

3/ Horizontal Situation Indicator

82
Q

In an ILS system which radio receiver generates vertical deviation commands for an autoland system?
1/ Localizer
2/ Glideslope
3/ Marker Beacon

A

2/ Glideslope

83
Q

The voltage output of an alternator may be regulated by controlling the:
1/ Speed of the alternator
2/ Current of the field circuit
3/ Resistance in the rotor windings

A

2/ Current of the field circuit

84
Q

In a typical Alternating Current Paralled Power System when a Differential Current Fault Occurs:
1/ Associated Bus-Tie-Breaker (BTB) Trips Immediately
2/ Associated Bus-Tie-Breaker (BTB) and Generator Breaker (GB) Trip immediately
3/ Associated Generator Breaker (GB) and Generator Control Relay (GCR) both trip immediately

A

3/ Associated Generator Breaker (GB) and Generator Control Relay (GCR) both trip immediately

85
Q
A

2/ Potassium hydroxide solution

86
Q
A

3/ Webbing and straps

87
Q
A

1/ Double sided tape

88
Q
A

2/ Wool

89
Q
A

1/ Honeycomb core faced with fibreglass

90
Q
A

3/ pull the slide out of its pack

91
Q
A

2/ Red or similar obvious indication

92
Q
  1. What is the maximum height above the floor for the installation of the escape path lighting:
    1/ 2 feet
    2/ 4 feet
    3/ 6 feet
A

1/ 2 feet

93
Q
A

3/ Can also be used as a flotation device

94
Q
  1. An emergency exit hatch:
    1/ Can be opened from inside or outside the aircraft
    2/ Can be opened from inside the aircraft only
    3/ Can be opened from outside only
A

1/ Can be opened from inside or outside the aircraft

95
Q

Flight crew escape ropes are manufactured from what material?

A

Nylon

96
Q
A

2/ the button is pushed again

97
Q
  1. Class b fires typically occur in
    1/ A passenger cabin
    2/ Engine compartments
    3/ Electrical bays
A

2/ Engine compartments

98
Q
A

2/ Weighting the container and its contents

99
Q
A

3/ A missing red (or visible red) disc in the thermal discharge line

100
Q
A

3/ Ailerons, Rudder and elevators

101
Q
A

1/ The stabiliser moves nose up

102
Q
A

2/ Assist in Lateral control

103
Q
A

3/ Assist pilot in moving control surface in manual mode

104
Q

When fuelling an aircraft using the over wing fill ports, it is necessary to
1/ Raise the fuelling rate in comparison to pressure filling
2/ Maintain the same fuelling rate as pressure fuelling
3/ Lower the fuelling rate in comparison to pressure fuelling

A

3/ Lower the fuelling rate in comparison to pressure fuelling

105
Q
A

2/ To ensure this lower specific gravity fuel will be accurately measured by tank capacitance system

106
Q

When using JET A fuel, the maximum refuelling pressure for commercial aircraft for pressure refuelling is normally:
1/ 25 PSI
2/ 50 PSI
3/ 100 PSI

A

2/ 50 PSI

107
Q
A

3/ The temperature of the day

108
Q
A

1/ of 3/ needs to be reviewed

109
Q
A

2/ or 3/ needs double check but certain its 2/

110
Q
A

1/ Variable displacement pump

111
Q
A

3/ Electric heater

112
Q
A

3/ On a surface below 0^C, where the water vapour converts directly into ice crystals

113
Q
A

3/ The fluid level is too high

114
Q
A

1/ air in the system

115
Q
A

1/ 5 minutes

116
Q
A

3/ The pilots of other aircraft can safely navigate around the aircraft

117
Q
A

1/ The Leading edge of the wing

118
Q
A

3/ A chemical reaction initiated by a primer

119
Q

If oxygen bottle pressure is allowed to drop below a specified minimum, it may cause:

A

needs double checking but think ans is
(Moisture to collect in the bottle)

120
Q
A

3/ It is to remove any remaining moisture from the compressed air after it leaves the moisture separator

121
Q
A

2/ The cabin/ambient differential pressure

122
Q
A

3/ Flight phase logic and flight leg logic

123
Q
A

1/ Is not normally assessable to the pilots unless the CMC system cues them to it

124
Q
A

c) the temp mix (hot) valve

125
Q
A

b) volume but set to achieve a certain mass

126
Q
A

a) the control colum moves and the trim wheels rotate

127
Q
A

c) in suspected icing conditions

128
Q
A

No answer given

129
Q
A

b) diaphragm

130
Q
A

a) chaffing

131
Q
A

c) low accumulater pre charge pressure

132
Q
A

a) upstream of the bleed valve

133
Q
A

No answer given

134
Q
A

a) not oppose the turn

135
Q
A

b) Overheat warning

136
Q
A

a) main deck

137
Q

An irreversible system

A

Aerodynamic loads on control surfaces due to air flow, are not transferred back to pilot.

138
Q

‘Q’ feel.

A

Provides artificial feel, particularly in elevator and horizontal stabiliser control systems

139
Q

How to prevent flutter?

A

Mass balance and dampen

140
Q

What 2 types of canards

A

Control and Lift

141
Q

Lift augmentation - ailerons

A

Lift augmentation –Here both ailerons are symmetrically ‘drooped’ to provide additional lift when flaps are extended.

142
Q

Manoeuvre load alleviation

A

Manoeuvre load alleviation –The ailerons are deflected upward (11°max) to create a downward force on the wing, which in turn reduces the overall load on the wing. This

143
Q

If a speed brake fails on one wing the other wing one:

A

If a speed brake fails on one wing the other wing one locks closed.

144
Q

QDM -
QDR -

A

QDM - Magnetic Bearing TO the station
QDR - Magnetic Bearing FROM the station

145
Q

In the northern hemisphere, during deceleration following a landing in an Easterly direction, the magnetic compass will indicate:
A) a heading fluctuating about 090° .
B) an apparent turn to the North.
C) an apparent turn to the South.

A

In the northern hemisphere, during deceleration following a landing in an Easterly direction, the magnetic compass will indicate:
A) a heading fluctuating about 090° .
B) an apparent turn to the North.
C) an apparent turn to the South.

A
C) an apparent turn to the South.
ANDS - Accelerate North, Decelerate South

146
Q

GCR:

A

GCR. Generator Control Relay

147
Q

Frise ailerons:

A

Frise ailerons:
Deflected up causes the LE to protrude down below the wing
Increases profile drag

148
Q

Purpose of speed brakes (air brakes)

A

increase drag while making little change to lift

Module 11B (42 decks)

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