SAFETY ASSESSMENT WHEEL BRAKE SYSTEM PADA PRIMARY DESIGN PESAWAT TERBANG TM-13

RICO SIMANJUNTAK, JHON (2019) SAFETY ASSESSMENT WHEEL BRAKE SYSTEM PADA PRIMARY DESIGN PESAWAT TERBANG TM-13. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

	Text (ABSTRAK) 13040092_ABSTRAK.pdf Download (314kB)
	Text (BAB I) 13040092_BAB I.pdf Download (108kB)
	Text (DAFTAR PUSTAKA) 13040092_DAFTAR PUSTAKA.pdf Download (44kB)
	Text (FULL SKRIPSI) 13040092_.pdf Restricted to Repository staff only Download (728kB)

Abstract

Safety assessment starts from identification of aircraft function, identification of failure condition, aircraft FHA output. The result of function hazard assessment (FHA) of TM13 aircraft wheel brake system is categorized as catastrophic whose failure condition is “loss of all stopping capability and loss of some stopping capability”. In fault tree analysis (FTA) of wheel brake system, the failure probability is 1.1822×10-13 so that this wheel brake system is declared safe to use. The calculation result of braking power required is 129327 N, while the available power is 418800 N, thus the wheel brake system is declared safe to use.

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