Safety Assessment hydraulic system Aircraft H-8

Cyrilus Sukoco Budiono

Submitted : 2017-11-01, Published : 2017-12-14.

Abstract

A hydraulic system is one of the secondary power used to drive the flight control surfaces, retract and extend landing gears, and to provide power to wheel brakes when the aircraft is on the ground. The failure of the hydraulic system results in aircraft lost of control which can lead to aircraft accident and passenger deaths. This journals discusses the safety assessment of the hydraulic system to be used in H-8 aircraft which includes the safety assessment process, regulations of the aircraft hydraulic system, the hydraulic system loads, and the aircraft hydraulic systems performance. The safety assessment begins with identification and classification of the functions, failure conditions, the effects of failure, and classify the failure conditions of the hydraulic system.

 

Keywords

System Safety Assessment (SSA), hydraulic system, Fault Tree Analysis (FTA), Markov Analysis (MA), Fanctional Hazard Asessment (FHA).

References

Barua, P. (2013). Empennage Statistics and Sizing Methods for Dorsal Fins. Hamburg: Hamburg University of Applied Sciences.

Crane, D. (2000). Aviation Mechanic Handbook. Washington: Aviation Supplies & Academics, Inc.

Currey, N. S. (1988). Aircraft Landing Gear Desain. Washington, D.C: AIAA.

Gudmundsson, S. (2011). Aircraft Preliminary Design Handbook. Great Owl Publishing.

P.Raymer, D. (2006). Aircraft Design : A Conceptual Approach Fourth Edition. Virginia: AIAA.

SAAB2000. (1998). Hydraulic System. Dalam Aircraft Operation Manual.

Sadraey, M. Wing Desaign. Daniel Webster College.

Sadray, M. (2012). Aircraft Design : A System Engineering Approach. Wiley Publication

Seabridge, I. M. (2008). Aircraft Systems. John Wiley & Sons, Ltd.

Smit, P. i. (1999, Januari). Vliegtuigsystemen. Vliegtuigsystemen . Delft: Faculteit der Luchtvaart-en Ruimtevaarttechniek Techniche Universiteit Delft.

W.L.Green. (1985). Aircraft Hydraulic Systems. Great Britain.

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