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Module5.13 Software Management Control(1of2)
Sub-Module 13 - Software Management Control Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programms.
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Requirements for configuration management of software can be found in.
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1 point
AWN 43.
JAR Ops (M).
ATA Chapter 46, Information Systems.
An aircraft system that, should it fail due to a software error, would cause a slight increase in crew workload, has a software level of.
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1 point
D.
B.
C.
What is the effect of a level 1 software failure?.
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Option 1
As far as a software product is concerned.
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the 'Software Release' phase is the same as the 'Finished Product' phase.
the 'Validation' phase is done to the software rather than to the component.
the 'Verification' phase includes performance testing a programmed EPROM.
Level 1 software failure.
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is defined as essential and will reduce safety margins.
is defined as essential and may have a minor effect.
is defined as critical and can lead to loss of aircraft.
An aircraft system that, should it fail due to a software error, would cause no injuries to occupants, has a criticality category of.
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1 point
major effect.
minor effect.
hazardous effect.
Where would you find the rules regarding upgrade of software?.
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1 point
JAR OPS.
The aircraft manufacturer.
AWN 43.
Software documentation procedures are laid down in.
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MOE.
JAA Ops.
AWN (45).
can be modified by.
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the manufacturer.
using the same rules as apply as to modifications to hardware.
licensed avionics engineers.
An aircraft system allocated a Criticality Category of Hazardous has a Software Level of.
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A.
B.
C.
If due to a software error in an aircraft system that would cause injuries to some of the occupants, the system has a software criticality category of.
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major effect.
hazardous effect.
minor effect.
An aircraft system that, should it fail due to a software error, would cause a significant reduction in safety margins may also cause.
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no injuries to occupants.
injuries to some occupants.
the loss of the aircraft.
Software changes come under the responsibility of.
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the engineer.
the national aviation authority.
the aircraft constructor.
Who can sign for a software update?.
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Design organization or the aircraft manufacturer.
Engineer.
Chief pilot.
What is the definition of level one software?.
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Non-essential.
Essential.
Critical.
Who can design new software?.
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1 point
BCAR section A8 approved company.
BCAR section A1 approved company.
The CAA.
Requirements for software control can be found in.
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JAR AWO.
AWN 43.
JAR OPS.
Who is responsible for producing the operational program of the FMS?.
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The manufacturer.
The pilot.
The engineer.
Control of software is carried out by.
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the aircraft manufacturers.
a licensed engineer.
the National Aviation Authority.
AWN 43 requires that.
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the aircraft operator be responsible for software assessment.
the CAA be responsible for software assessment.
the aircraft constructors be responsible for software assessment.
An aircraft system with a software level of D, should it fail due to a software error, may cause the aircraft safety margin to be.
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slightly decreased.
slightly increased.
significantly decreased.
An aircraft system allocated a software level of C that, should it fail due to a software error, may cause.
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injuries to some occupants.
injuries to a large proportion of occupants.
no injuries to occupants.
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