ANALISIS DAN PENANGANAN KEGAGALAN
FUNGSI AILERON PADA PESAWAT BOEING 737-800 NG
DI HANGAR 4 PT. GMF AEROASIA
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
Rivaldo Fernandez, Dominikus
Subject
T Technology (General)
Datestamp
2024-04-25 03:55:24
Abstract :
The Flight Control System is used to control the effect of forces on the aircraft, the direction of flight and the attitude of the aircraft. Flight control consists of primary flight control and secondary flight control. The aileron is the main flight control on the Boeing 737-800 NG aircraft which is driven by a hydraulic system and cables. System failure on ailerons that often occurs is the ailerons experience slow movement or the ailerons do not return to their normal position. The effect of the damage is that the aircraft cannot be controlled to drive a rolling motion. In this study using the method of observation and information from various sources. In addition, this study also uses the Fault Tree Analysis (FTA) method to determine the cause of aileron failure on the Boeing 737-800 NG aircraft. The results of the research on problems with the aileron Boeing 737-800 NG are problems with the aileron power control unit (PCU) component. From these problems, the problem handling process is carried out which refers to the AMM Boeing 737-800 task 27-11-00. By analyzing the cause of failure of the aileron using the fault tree analysis (FTA) method, 10 basic events were obtained consisting of body cable loose, wing cable blockage, FOD, damage, stuck, actuator trouble, friction, packing seal broken, dirty, and clogging.
The Flight Control System is used to control the effect of forces on the aircraft, the direction of flight and the attitude of the aircraft. Flight control consists of primary flight control and secondary flight control. The aileron is the main flight control on the Boeing 737-800 NG aircraft which is driven by a hydraulic system and cables. System failure on ailerons that often occurs is the ailerons experience slow movement or the ailerons do not return to their normal position. The effect of the damage is that the aircraft cannot be controlled to drive a rolling motion. In this study using the method of observation and information from various sources. In addition, this study also uses the Fault Tree Analysis (FTA) method to determine the cause of aileron failure on the Boeing 737-800 NG aircraft. The results of the research on problems with the aileron Boeing 737-800 NG are problems with the aileron power control unit (PCU) component. From these problems, the problem handling process is carried out which refers to the AMM Boeing 737-800 task 27-11-00. By analyzing the cause of failure of the aileron using the fault tree analysis (FTA) method, 10 basic events were obtained consisting of body cable loose, wing cable blockage, FOD, damage, stuck, actuator trouble, friction, packing seal broken, dirty, and clogging.
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