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WorksheetsAvionic Job Function
Total questions: 20
Worksheet time: 15mins
What is the main purpose of this equipment?
To communicate with ATC
To detect location of another flying aircraft
To provide power to start engine
To provide weather condition during flight
To certify a new type of airplane with 19 passengers configuration, the applicant must complies to:
CASR 27
CASR 29
CASR 23
CASR 36
Which instrument is not a basic-T requirement?
Horizontal Situation Indicator
Altitude Indicator
Airspeed Indicator
VOR Indicator
To make sure the frequency for AC voltage constant at 400Hz is the function of:
GCU
CSD
Auxiliary Battery
RAT
To convert AC voltage to DC voltage in the aircraft is the function of:
Transformer Rectifier Unit
Inverter
Auxiliary Power Unit
Power Distribution Unit
These are example of ground based navigation system on the aircraft, except:
VOR
DME
ADF
HF
According to CASR, the minimum battery capacity for normal category airplanes with maximum altitude over 25.000 feet is:
1 Hour
30 Minutes
90 Minutes + Injury Time
5 Minutes
System that the aircraft needs to be able to continue safe operation is:
Main battery
Auxiliary battery
Non Essential system
Essential system
Below is the type of power source, except:
Generator control unit
Essential bus
Auxiliary battery
Ram air turbine
Below is the typical CAS message color, except:
White
Blue
Yellow
Red
CAS message color that indicates an advisory is:
White
Blue
Yellow
Red
Most common type of aircraft battery used in aircraft, except:
Li-ion
NiCd
Alkaline
Lead Acid
What kind of output will be given by Air Data Computer?
IAS
GPS position
Navigation database
Terrain
To prevent overload damage to the electrical system power distribution and to avoid fire hazard caused by overheating wiring, is the main function of:
Inverter
Circuit breaker
Outside Air Temperature probe
Auxiliary battery
Below are electromagnetic effect test required by CASR, except:
EMC Test
HIRF Test
Indirect Effect Lightning Test
Electrical Grounding Bonding Test
The main function of TCAS:
to prevent unintentional impacts with the ground
to communicate with ground based station
to avoid mid air collision
to provide air data to PFD
The main function of TAWS:
to prevent unintentional impacts with the ground
to communicate with ground based station
to avoid mid air collision
to provide air data to PFD
What is the main purpose of Radio Altimeter?
to provide radio communication with ATC
to provide aircraft altitude above ground level
to provide positioning for ADSB
to provide aircraft altitude information during cruise phase
What is the purpose of this component?
as the main power source for aircraft
to provide thrust
to provide power in case of generator and APU fail
for air conditioning
Below are methods of compliance that can be proposed by the applicant to DGCA for a new type aircraft certification, except:
Analysis
Flight Test
Exemption
Inspection
