Airworthiness Directives; Eurocopter Deutschland Model EC135 Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2002-05-30 · Effective 2002-06-14 · 67 FR 37666
Document
Document number
02-13290
Federal Register citation
67 FR 37666
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter Deutschland Model EC135
Publication date
2002-05-30
Effective date
2002-06-14
FAA docket
Docket No. 2001-SW-69-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for Eurocopter Deutschland (Eurocopter) Model EC135 helicopters with Turbomeca Arrius 2B1 engines installed. This action requires modifying the engine electrical control unit (FADEC) software and the collective linear transducer (LVDT). This amendment is prompted by a parameter discrepancy within the engine fuel main metering unit that is transmitted to the FADEC. This condition, if not corrected, could result in deactivation of the engine main fuel-metering valve, loss of automatic control of the affected engine, and subsequent loss of control of the helicopter.