S10 EASA AD Pressure Line Crack

S10 EASA AD Pressure Line Crack


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June 24, 2005 | D-2005-228

Ripped pressure lines between Airbox-Carburator- Differential fuel pressure sensor were found during a requested maintenance event after engine trouble in the range between maximum continuous power and take off power. The cracks can be a result of non complete temperature resistance. This type of pressure line was installed since July 27, 2004. It was used for serial production and for spare parts

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