Airworthiness Directive 2000-10-07

one-time
Official AD 2000-10-07 · FR doc 00-12356 · 2000-05-17 · airframe

Airworthiness Directives; Eurocopter Deutschland GmbH (Eurocopter) Model EC 135 Helicopters

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to Eurocopter Model EC 135 helicopters. This AD requires replacing a certain oil cooler fan splined drive shaft (shaft) with a different airworthy shaft and re-identifying the part numbers on the oil cooler fans. This amendment is prompted by two incidents in which the shaft broke. The actions specified by this AD are intended to prevent failure of the shaft, loss of oil cooling, and a subsequent engine shutdown during flight.

Which aircraft AD 2000-10-07 applies to

ModelsEC135
Part-conditionalL 792M3004 225, L 792M3004 235, L 792M3004 102, L 792M3004 103, L 792M3005 102, L 792M3005 103.

Replace oil cooler fan splined drive shaft P/N L792M3004-225 with airworthy P/N L792M3004-235; re-identify left oil cooler fan P/N L792M3004-102 to -103 and right fan P/N L792M3005-102 to -103. Per Eurocopter Alert SB EC135-79A-001, dated Jan 23, 1998; related to LBA (Germany) AD 1998-109.

Whether AD 2000-10-07 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2000-10-07 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.