@thesis{thesis,
		author={ALDI RACHMADANI ARYA PRADANA  FAJAR},
		title ={TROUBLESHOOTING 
INDICATOR ERROR STANDBY ALTIMETER
PADA PESAWAT BOEING 737-NEXT GENERATION},
		year={2020},
		url={http://eprints.stta.ac.id/1876/},
		abstract={The standby altimeter is one of the standby navigation systems on the 
Boeing 737-NG which functions to indicate the altitude of an aircraft standby 
altimeter is an auxiliary instrument that uses an analog system. The instrument 
relies on differential pressure, obtained from the static port taken from the air 
outside the aircraft. Then the air is used to move the gear connected to the pointer. 
The altimeter must always be in serviceable condition, because in its use it cannot 
be separated from errors. One of them is an error indicator.
To find out the error indicator that occurs on the standby altimeter is to 
perform a system test using ADTS (Air Data Test Set). Proceed to the step of 
identifying possible causses. Problem was found with alternate static system block.
After knowing the problem, according to the Fault Isolation Manual TASK 
34-13-801 the troubleshooting process was carried out by means of a flush 
alternate static system. Followed by a system test, the results of the indicator on the 
standby altimeter have shown that it is within the specified tolerance limits and can 
operate normally. This indicates that the problem has been resolved and the system 
has returned to a serviceable state.}
		}