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Transport Canada Exam Questions With Complete Solutions
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Transport Canada Exam Questions WithComplete Solutions
match the colored lights to its corresponding definitions
To aircraft on the ground during RONLY and NORDO aircraft
departure procedure:
1)SERIES OF GREEN FLASHES
2)STEADY GREEN LIGHT
3)SERIES OF RED FLASHES
4)STEADY RED LIGHT
5)FLASHING WHITE LIGHT
6)BLINKING RUNWAY LIGHTS
a) cleared to take off
b) clear to taxi
c) stop
d) return to starting point on airport
e) advises vehicles and pedestrian to vacate runway immediately
f) taxi clear of landing area in use correct answer: 1b, 2a, 3f, 4c,
5d, 6e
Order the correct procedure for this Radar Traffic Information
Issue traffic information to radar-identified aircraft as follows:
a)Type of aircraft, if known, or the relative speed and the
altitude, if known.
b)Position of the traffic in relation to the aircraft's
observed track.
,c)Direction of flight. correct answer: b, c, a
North Atlantic Tracks transatlantic flight routes that stretch from
the northeast of North America to western Europe across the
Atlantic Ocean, flying between the altitudes of: correct answer:
29000 and 41000 feet
The primary purpose of North Atlantic Track routes is to
provide: correct answer: minimum time route
North Atlantic Tracks are aligned in such a way as to minimize
any head winds and maximize tail winds impact on the aircraft
to result in more efficiency by reducing: correct answer: fuel
burn and flight time
To make such efficiencies possible, the routes are created
______ daily to take account of the shifting of the winds aloft
and the principal traffic flow, eastward in North America
evening and westward _______ hours later. correct answer:
twice, twelve
RVSM airspace is any airspace or route between _________
inclusive where aircraft are separated vertically by ______.
correct answer: fl290 and fl410 , 1000 ft (300M)
Aeroplane flying east need to be flying at _____ altitudes correct
answer: odd +500
Aeroplane flying west need to be flying at _____ altitudes
correct answer: even
,The complete structure of an airplane, including the fuel tanks
and lines, but without instruments and engine installed. correct
answer: airframe
The rate of doing work is: correct answer: power
the amount of transformed into energy is: correct answer: work
power developed within an internal combustion engine is called
correct answer: indicated horsepower
the power which is available, after friction and other losses is
called: correct answer: brake horse power
the average pressure within the clinder during the entire period
of the power stroke, from the time the piston is at the top dead
centre until it reaches bottom dead centre correct answer: mean
effective pressure
Term used to define the available to produce the net power
delivered at the propeller shaft correct answer: brake mean
effective pressure
Three types of piston engines in current use are: correct answer:
radial, in-line and horizontally opposed
This engine has 2 banks of cylinders working on the same
crankshaft which lie directly opposite to each other. Engine
design is flat, or pancake shape. correct answer: horizontally
opposed engine
, This type of engine always has an odd number of cylinders. This
is necessary because the firing order is alternate. correct answer:
radial engine
this engine type, the cylinders are arranged side b side in a row
along the crankcase. correct answer: in-line engine
As it rotates, it convert the torque, or turning moment, of the
crankshaft into thrust, or forward, speed. correct answer:
propeller
the distance in feet a propeller travels forward in one revolution
is called: correct answer: pitch
This propeller blade angle cannot be adjusted by the pilot. Best
for all flight conditions, but it is a trade-off between take-off
performance and cruise performance. correct answer: fixed
pitch propeller
This propeller has adjustable pitch, controllable pitch propeller,
and constant speed propellers correct answer: variable pitch
propellers
The mechanism for varying the pitch of the propeller may be:
correct answer: mechanical, hydraulic or electrical
The two types of hydraulic mechanism for variable pitch
propellers are: correct answer: counterweight and hydromatic
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