SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM

This thesis contain about a safety assessment conducted on the N219 aircraft to ensure that its systems meet the safety requirements. Several N219 aircraft systems which concern in this thesis consist of hydraulic power, braking and steering system. Further, the safety requirements will be establish...

Full description

Saved in:
Bibliographic Details
Main Author: Yulasmana, Yoga
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/33771
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:33771
spelling id-itb.:337712019-01-29T11:33:44ZSAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM Yulasmana, Yoga Indonesia Theses Safety Assessment, Safety Requirement, Quantitative Analysis INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/33771 This thesis contain about a safety assessment conducted on the N219 aircraft to ensure that its systems meet the safety requirements. Several N219 aircraft systems which concern in this thesis consist of hydraulic power, braking and steering system. Further, the safety requirements will be established by the aviation authority as a certification basis for satisfying the CASR Part 23 according to the N219 category as a commuter aircraft. To conduct safety assessment process on those systems, this thesis follows the process outlined in SAE ARP4761 document. It encompasses Functional Hazard Assessment (FHA) and System Safety Assessment (SSA). For Preliminary System Safety Assessment (PSSA) had been performed, because design of the system was already defined. The quantitative analysis for this assessment use Fault Tree Analysis (FTA) and Markov Analysis (MA). The comparative results obtained from both of methods show that there is no significant difference. The difference in results is only found for longer period of operation in the system. These results indicate that MA can be used as a validation method for FTAs as well, and vice versa. Subsequently because MA method can handle repair condition better than FTA, this thesis conduct a maintainability study for further consideration analysis. It concludes that the high maintainability target can only obtained for the small failure rate. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description This thesis contain about a safety assessment conducted on the N219 aircraft to ensure that its systems meet the safety requirements. Several N219 aircraft systems which concern in this thesis consist of hydraulic power, braking and steering system. Further, the safety requirements will be established by the aviation authority as a certification basis for satisfying the CASR Part 23 according to the N219 category as a commuter aircraft. To conduct safety assessment process on those systems, this thesis follows the process outlined in SAE ARP4761 document. It encompasses Functional Hazard Assessment (FHA) and System Safety Assessment (SSA). For Preliminary System Safety Assessment (PSSA) had been performed, because design of the system was already defined. The quantitative analysis for this assessment use Fault Tree Analysis (FTA) and Markov Analysis (MA). The comparative results obtained from both of methods show that there is no significant difference. The difference in results is only found for longer period of operation in the system. These results indicate that MA can be used as a validation method for FTAs as well, and vice versa. Subsequently because MA method can handle repair condition better than FTA, this thesis conduct a maintainability study for further consideration analysis. It concludes that the high maintainability target can only obtained for the small failure rate.
format Theses
author Yulasmana, Yoga
spellingShingle Yulasmana, Yoga
SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
author_facet Yulasmana, Yoga
author_sort Yulasmana, Yoga
title SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
title_short SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
title_full SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
title_fullStr SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
title_full_unstemmed SAFETY ASSESSMENT OF N219 AIRCRAFT HYDRAULIC POWER, BRAKING AND STEERING SYSTEM
title_sort safety assessment of n219 aircraft hydraulic power, braking and steering system
url https://digilib.itb.ac.id/gdl/view/33771
_version_ 1822924091915501568