Slip-Test Questions Flashcards
1
Q
A
(b) Rudder, Elevators, ailerons
2
Q
A
(a) lateral
3
Q
A
(a) It helps to destroy lift on landing
4
Q
A
(a) Yes
5
Q
A
(b) Differential Ailerons
6
Q
A
(a) Nose up
7
Q
A
(a) aileron
8
Q
A
(a) it will increase the angle of attack
?
9
Q
A
(a) wing leading edge
10
Q
A
(c) It won’t move
'’In the manual mode of operation, the flight control column moves the tab on the control surface, and the aerodynamic forces caused by the deflected tab move the main control surface’’
On ground = no oncoming airflow = no aerodynamic force to move main control surface
11
Q
What has the most effect on the speed of sound?
(a) Altitude
(b) Air Temperature
(c) Air Density
A
(b) Air Temperature
12
Q
A
(a) M 0.75 - M 1.2
13
Q
A
(a) By sweeping the wings back
14
Q
A
(b) It slows down
15
Q
A
(c) A part will be replaced after a fixed number of cycles.
16
Q
A
(a) Prevents a control cable from damaging the structure.
’’ Special consideration will need to be given to the routing of control cables to protect the aircraft structure from the cables. This is accomplished by the use of grommets, fairleads and pressure seals’’
17
Q
A
(b) Secondary
18
Q
A
(b) The vertical axis
19
Q
A
(c) Doors
20
Q
A
(c) Twisting
21
Q
A
(c) Tension
22
Q
A
(c) Semi-monocoque
23
Q
A
(b) Larger than their frame
24
Q
A
(b) Gates
25
(c) Gold Oxide
26
(a) It has no external support braces
27
(c) Ribs
28
(c) Fillet seal
????? requires check
may be wrong
29
(b) Carbon Fibre
'' Primary structural components of stabilisers (Spars, Ribs and skin panels) are made of laminations of Carbon Fibre Reinforced Plastic (CFRP).
All other components are made of the same material or Glass Fibre Reinforced Plastic (GFRP) or of light alloy''
30
(a) 1
31
(a) front
'' Change the balance weight in the leading edge of the surface as indicated in the maintenance manual''
Dale Crane pg 295
32
How are composite engine cowling doors protected from heat?
(a) Fan from the engine air is blown against them.
(b) Bleed air from the engine air is blown against them.
(c) Titanium heat shield.
(c) Titanium heat shield
'' Very modern engine hot section doors are rather of composite than of metal sheet construction, but to provide fire protection are covered with stainless steel blankets and titanium alloys heat shield''
33
(c) Both
34
(a) Engines
35
(b) To vent the cabin
'' Most aircraft are equipped with an emergency ram air system. The system can be used in flight to ventilate the cockpit and cabin if all packs fail or for smoke removal''
36
(b) The vapour cycle system
37
(c) It controls the temperature
38
(a) Ram air
39
(a) Low temperature
'' The larger reduction in temperature causes the moisture int he air to condense''
???? double check ans
40
(c) It is injected overboard
41
(b) Through the louvers on the sidewall panel
42
What is the most commonly used cabin altitude?
(a) 8000 ft
(b) 10000ft
(c) 38000 ft
(a) 8000 ft
43
(b) 500 ft/min
44
(c) An outflow valve
45
(a) To prevent the aircraft from exceeding its max cabin press differential
''Pressure relief valves also called safety relief valves should avoid excessive cabin pressure. When the pressure difference between cabin and outside air becomes too large, there is a chance of damage to the fuselage structure. For this reason, safety relief valves are installed to open in case of too much pressure difference.''
46
(b) Aural warning in the cockpit
47
(b) Platinum
48
(c) To allow linear expansion
'' The bellows are designed with corrugations that allow the expansion to be linear with a change in altitude.''
49
(b) Static
50
(c) Flight level
(Note: QNE = STD)
51
(b) Barometric setting
52
(a) Precession
53
(b) Vertical Gyro
54
(a) -Needs to be double checked
55
(c) Double check tho
56
(a) Commutator
57
(a) Magnetising the poles
58
(b) Generator output voltage
59
(c) PMG, Exciter generator, Main generator
''A brushless alternator consists of three separate fields, a permanent magnetic field, an exciter field, and a main output field.''
60
(c) 115V, AC 400 Hz
61
What is the purpose of a Constant Speed Drive System?
(a) To maintain a constant generator RPM
(b) To maintain a constant Engine RPM
(c) To maintain a constant voltage
(a) To maintain a constant generator RPM
62
(b) It cannot be recharged
63
(c) a VSCF
VSCF = Variable Speed Constant Frequency alternator
64
(c) Nickel Cadmium
''If a nickel-Cadmium cell is subjected to an excessively high charging rate ...''
65
(b) Sodium Bicarbonate
''Spilled electrolyte must be neutralized by a solution of baking soda (sodium bicarbonate) and water''
66
(b) Constant Current
'' The problem of thermal runaway is minimized by using a constant-current charger that limits the amount of current that can be put into the cell''
67
(a) Convert AC to DC
68
(b) Convert DC to AC
69
(b) 3
(May need verifying)
70
(b) Split Bus System
71
(c) Blue
'' When external power of the correct voltage, frequency and phase sequence is available at the external power receptacle; the ''External Power Available'' indicator will illuminate. This is usually a **blue** indicator on the External Power Panel and is repeated in the Cockpit''
72
Above which of the following heights must an escape slide be provided?
(a) 1.8 meters
(b) 2.8 meters
(c) 3.8 meters
(a) 1.8 meters
73
(a) 1, 1/2 minutes
''For aircraft having a seating capacity of more than 44 passengers, it must be shown that the maximum seating capacity, including the number of crew members required by the operating rules for which certification is requested, can be evacuated from the aircraft to the ground under simulated emergency conditions within 90 seconds.''
74
(a) batteries
75
(c) Carrying baggage.
76
(a) The pilot
77
(a) A control tab takes over
78
(c) The flight control follow-up system
79
(c) The flight control follow-up system.
80
(c) No
81
(b) Pitch down at high speed.
''Modern aircraft are provided with automatic mach trim compensation achieved by the autopilot or flight management systems. It compensates the aerodynamic pitch down tendency at high speed (v \> 0.8M).''
82
(a) The flaps stop and the ailerons are trimmed.
83
(c) Hydraulic
84
(b) Rudder
85
(b) No.
86
(c) A part of the aircraft structure
87
(b) To transfer fuel from one tank to the opposite engine.
88
What is the most common principal of operation of a boost pump?
(a) Gear type.
(b) Piston type.
(c) Centrifugal type.
(c) Centrifugal type.
89
(a) To pressurise the fuel tank.
90
(b) Capacitors.
91
(c) 3000 psi
92
(a) To pressurise the system
93
(a) 30 psi
94
(a) To power one hydraulic system from another.
95
(c) To dampen out surges.
96
(b) Tricycle landing gear system
Tricycle = nose wheel unit forward of 2 main gear units
Conventional = tail wheel behind 2 main gear units
97
(b) Nitrogen.
98
(b) Centering cam.
99
(b) Over centre link.
100
Three green lights on the landing gear display in the cockpit mean that?
(a) All the gears are up and locked.
(b) All the gears are down and locked.
(c) All the gears are in transit.
(b) All the gears are down and locked.
101
(a) Two piece construction
102
??????
103
(b) Anti-skid control lever.
104
(a) Right side.
105
(c) Centre
106
(b) It can cause it to crack.
107
(a) 21%
108
(c) Because it has too high a moisture content.
109
(c) 2600.psi
110
(c) 14,000ft
111
(c) Check for discolouration.
112
(c) Closed
113
(c) Compressor section.
114
(c) Check valve.
115
(b) Under the floor.
''Potable water is stored in one or more tanks below the cabin floor.''
116
(a) An in line electrical heater.
117
(a) Pneumatic pressure.
118
(c) From the potable water tank.
119
????
120
(c) Both of the above.
121
(b) Chromel and Alumel
Fire Detection Thermocouples use iron and constantan along with oil sensors and other indicators
An exhaust gas temperature Thermocouple on Turbine Engines are made from Chromel and Alumel
'' These sensors have a piece of each of the two thermocouple wires, typically iron and constantan''
122
(a) Change in resistance when heated
123
(b) Discharge due to an overheat condition.
124
(a) Discharging a fire extinguisher.
'' The containers are sealed with a frangible disk that is broken when a cutter is fired into it by a powder charge, or squib, which is ignited when the pilot closes the agent discharge switch''
125
**(c) 800 PSI**
126
a) stringers and Longerons
127
a) Stringers
128
?????
129
(a) reporting mode
130
Where is the HF antenna normally located?
(a) Lower Fuselage
(b) Upper Fuselage
(c) Vertical Stabiliser
(c) Vertical Stabiliser
