1.
Instruments are classified as
a.
Flight instruments
b.
Engine instruments
c.
Navigation instruments
d.
All the above
2.
Basic six layout is also known as
a.
Blind flying panel
b.
Steam gauge cockpit
c.
Both a and b
3.
Among this which are Gyroscopic instruments
a.
Attitude indicator
b.
Heading indicator
c.
Turn coordinator
d.
All the above
4.
The panel mounted in vertical position or slopped forward at about ____ from vertical to
minimize parallax error
a.
15 degree
b.
45 degree
c.
30 degree
5.
The dial of VSI is generally calibrated in ___
a.
100's of feet per minute
b.
1000 feet per minute
c.
200 feet per minute
6.
Analog vertical speed indicator (VSI) may also be referred as ___
a.
Vertical velocity indicator
b.
Rate of climb indicator
c.
Rate of descent indicator
d.
All the above
7.
Angle of attack sensor is also known as
a.
Alpha sensor
b.
Beta sensor
c.
TAT sensor
8.
Analog flight instruments are operated by
a.
Pneumatic
b.
Gyroscope
c.
Both a and b
9.
Which instrumentation is often displayed in center of cockpit where it is easily visible to both
pilot and copilot
a.
Flight
b.
Engine
c.
Navigation
10.
Sensing and display of pressure and temperature information using bourdon tube mechanism
occurs in single housing they are called as
a.
Direct reading
b.
Remote reading
c.
Indicated reading
11.
In Basic 6 instruments the pitch and roll information is given by which indicator
a.
Heading indicator
b.
Direction indicator
c.
Attitude indicator
12.
Compass are classified as
a.
Direct reading
b.
1+ in which sensing and indication takes place inside indicator casing
c.
Remote Reading compass
d.
All the above are correct
13.
Angle of attack is angle between
a.
Chord line of wing of aircraft and relative airflow
b.
Relative wind and relative wing
c.
Chord line of wing and aircraft wing
14.
Stall warning system alerts pilot
a.
After stall
b.
Before stall
c.
At normal angle of attack
15.
In stall warning system, stick shaker is connected to
a.
Servo system
b.
Control column
c.
Transducer system
16.
Remote reading compass is also known as
a.
Gyromagnetic compass
b.
Heading reference unit
c.
Gyro stabilized compass
d.
All the above
17.
Stick pusher is also called as
a.
Stick shaker
b.
Stick nudger
c.
Stick puller
18.
Angle of attack indication is shown on
a.
Primary flight display
b.
1+ between attitude indication and altimeter scale indication
c.
Both a and b
19.
Advantages of glass cockpit
a.
Simplifies aircrafts operation and navigation
b.
Allows pilots to focus on important information
c.
Saves weight and space
d.
all the above
20.
Full form of EICAS
a.
Engine indicating and crew alerting system
b.
Engine crew alerting system
c.
Electronic indicating crew alerting system
21.
Which display displays information of airspeed, altitude, vertical speed, attitude of aircraft
a.
Primary flight display
b.
Navigation display
c.
Engine display
22.
Which display shows navigational information from multiple systems such as ILS,VOR,DME
a.
Primary flight display
b.
Navigation display
c.
Engine display
23.
EICAS is a name given to engine warning and system displays by which manufacturer
a.
Airbus
b.
Boeing
c.
Cessna
24.
In magnetic compass, the fluid used inside the instrument case is
a.
Kerosene
b.
Water
c.
Oil
25.
Rigidity property of gyroscope depends on
a.
Mass of rotor
b.
Speed of rotor
c.
Diameter of rotor
d.
All the above
26.
Precession property of gyroscope depends upon
a.
Strength and direction of force
b.
Mass of rotor
c.
Speed of Rotor
d.
All the above
27.
Precession of gyroscope is used in which gyro instrument
a.
Artificial Horizon
b.
Direction Indicator
c.
Turn and bank indicator
28.
Types of gyro
a.
Tied gyro
b.
Earth gyro
c.
Rate gyro
d.
All the above
29.
To avoid confusion with artificial horizon, turn coordinators are labelled with
a.
No pitch information
b.
No roll information
c.
No turn information
30.
Advantages of electric driven gyro
a.
Less maintenance
b.
More efficient
c.
Requires less component
d.
All the above
31.
Inclinometer in turn and slip indicator gives
a.
Slip
b.
Skid
c.
Both a and b
d.
Only skid information
32.
MTCS in case of Direction Indicator
a.
Works on rigidity
b.
Circular card provide heading indication
c.
Indications due to outer gimbal displacement
d.
All the above
33.
Setting of heading with the help of adjustment or caging knob on heading indicator with respect
to magnetic compass due to gyro drift is called
a.
Slaving of gyro
b.
1+ done by twisting the knob
c.
Caging of gyro
d.
Both a and b
34.
In straight and level flight, turn coordinator shows
a.
Constant heading
b.
Rate of turn pointer centered
c.
Slip and skid ball centered
d.
All the above
35.
Freedom of free gyro rotor
a.
Spinning freedom
b.
Tilting freedom
c.
Veering freedom
d.
All the above
36.
Power supply used to drive gyro rotor is
a.
115V AC by alternators and inverter
b.
28 V DC by generator and rectifiers
c.
Both a and b
37.
Gyro horizons have pull to cage knob to
a.
realign gyro in straight and level flight
b.
to lock outer gimbal ring
c.
to update heading reference
s
38.
Artificial horizon is also known as
a.
Attitude indicator
b.
Gyro horizon
c.
Heading indicator
d.
Both a and b
39.
Which type of gyro is used by Turn and bank Indicator
a.
Tied gyro
b.
Rate gyro
c.
Earth gyro
40.
Which type of gyro is used by Direction Indicator
a.
Tied gyro
b.
Rate gyro
c.
Earth gyro
41.
MTCS : GRYO HORIZON
a.
is a primary instrument
b.
located at top center position
c.
Both a and b
d.
Only a is correct
42.
The panel mounted in vertical position or slopped forward at about ____ from vertical to
minimize parallax error
a.
15 degree
b.
45 degree
c.
30 degree
43.
Cross hatched area in altimeter displayed during operation of aircraft
a.
Above 10000 feet
b.
Below 10000 feet
c.
Below 20000 feet
d.
Above 20000 feet
44.
Thinnest pointer in altimeter registers registers altitude in ___foot increments
a.
10,000
b.
1000
c.
100
45.
Independent static vents are always located on
a.
Aft section
b.
Each side of aft section
c.
Each side of fuselage
46.
Pitot static system is also known as
a.
Manometric system
b.
Air data system
c.
Both a and b
47.
An adjustable pressure scale is visible on the face of analog altimeter known as
a.
Barometric window
b.
Kollsman window
c.
Atmospheric window
d.
Both a and b
48.
Mark the correct statement in case of Kollsman window
a.
Set to read existing atmospheric pressure
b.
Is on altimeter dial
c.
Adjusted by setting knob on front of instrument
d.
All are correct
49.
In modern aircraft cockpit altitude is displayed in
a.
Primary flight display
b.
a + near artificial horizon
c.
a + near airspeed indicator
d.
Only b is correct
50.
Longest pointer in altimeter indicates altitude in
a.
100 's of feet
b.
1000 feet
c.
10000 feet
51.
An altimeter is an instrument that is used to indicate the height of the aircraft above
predetermined level such as
a.
Sea level
b.
Terrain beneath the aircraft
c.
Either a or b
52.
Slaving system in remote reading compass
a.
Compares detector and gyro unit
b.
Compares compass and heading indicator
c.
Sense earth’s magnetic field
53.
Rigidity is also known as
a.
Precession
b.
Gyroscopic Inertia
c.
Both a and b
54.
Pitch freedom in artificial horizon is
a.
+- 85 degree
b.
360 degree
c.
45 degree
55.
An aircraft will, in its own characteristics provides warning of stalled condition.
a.
Buffeting
b.
Gentle or severe pitch down
c.
Wing drop
d.
All the above
56.
Small aircraft uses
a.
Hinged vane type sensor
b.
1+ mounted in wing leading edge
c.
2+ Vane protrudes in airstream
d.
All the above
57.
In aircraft's particularly those with rear mounted engines and T tail configuration
a.
Deep and super stall can occur
b.
To prevent deep stall in addition to stick shaker, stick pusher is installed
c.
Both a and b
58.
Which instrument continues to operate even if there is failures in the electrical, vacuum or pitot
static systems.
a.
Direct reading compass
b.
Artificial horizon
c.
Turn and bank indicator
59.
Remote reading compass consist of
a.
Magnetic field Detector
b.
Slaving system
c.
Gyro unit or indicator
d.
All the above
60.
Upper display of ECAM or EICAS is known as
a.
Primary ECAM/EICAS display
b.
Engine warning display
c.
Both a and b
d.
System display