Dit is de tweede integrerende opdracht van het tweede thema van engineering. In dit verslag is er een fault tree opgesteld en worden er twee onderhoudstaken uitgelicht. Dit verslag is beoordeeld met een 7,5
, Inhoudsopgave
Inleiding .......................................................................................................................................... 3
1. Krachten in het flight control system ....................................................................................... 4
1.1 Krachtberekeningen voor de piper seneca II .......................................................................... 4
1.2 Samenvatting van de krachtberekeningen voor de Airbus A320............................................ 7
2. Het hydraulische systeem ........................................................................................................ 8
2.1 Doel van het hydraulische systeem ........................................................................................ 8
2.2 Inrichting van het hydraulische systeem van de A320............................................................ 8
3. Fly-by-Wire en het elektrische systeem.................................................................................. 11
3.1 Doel en werking van het FBW systeem ...................................................................................... 11
3.2 doel en inrichting van het elektrische systeem .......................................................................... 11
4. Compliance met CS 25.1309 ................................................................................................... 13
5. Onderhoud aan het systeem .................................................................................................. 14
5.1 Taak 1: Check of the aileron servo controls and hinge bearings for too much play and condition
.......................................................................................................................................................... 14
5.2 Taak 2: Check of the aileron servo controls fluid reserve piston position with hydraulic reservoir
depressurized ................................................................................................................................... 15
Conclusie....................................................................................................................................... 16
Literatuurlijst ................................................................................................................................ 17
Bijlage I: Fault Tree Analyse ........................................................................................................... 19
Bijlage II: gehanteerde planning ................................................... Fout! Bladwijzer niet gedefinieerd.
Bijlage III: reflectie ....................................................................... Fout! Bladwijzer niet gedefinieerd.
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