@thesis{thesis,
		author={IKRAMULLAH  IKRAMULLAH},
		title ={ANALISIS KEAMANAN (SAFETY ASSESSMENT)
TERHADAP AILERON CONTROL SYSTEM
PADA PESAWAT N219},
		year={2019},
		url={http://eprints.stta.ac.id/1971/},
		abstract={Safety assessment is a method to analyse the value of function, structure and 
component safetiness off an aircraft. This process can be based on direct 
observation, through observing and analysing the function of system or the 
component of aircraft which has been done by its designer. This safety assessment 
process is done from designing stage, system building until every function from 
aircraft system are enable, then the value of highest severity classification is 
suitable with the requirement which has been verified in CASR part 23.1309 about 
equipment, systems and installations.
In this bachelor thesis, research about aileron control system on N219 
aircraft will be done using safety assessment process approach. Method used in by 
the writer in this thesis in functional hazard assessment, reliability data prediction, 
and fault tree analysis.
By using fault tree analysis method, can be proven that every failure condition 
exist in functional hazard assessment is confirmed that this possibility is hardly 
occurred. This is proven by the result of fault tree analysis, by the following 
statement, obtained a fact that aileron control system is complied with requirement 
which is stated in CASR part 23.1309. By the fact, aileron control system proper to 
be used in N219 aircraft.}
		}