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Airworthiness Directive

AD 2012-10-53: Eurocopter Deutschland GmbH Helicopters

Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

Effective
Dec 5, 2012
Published
Nov 20, 2012
Registered aircraft
286

Models this AD may apply to

AI-extracted — verify against original

Matched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.

Aircraft

  • Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.
  • Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed.

Applicability

From the AD text
This AD applies to Model EC135 P1, EC135 P2, EC135 P2+, EC135 T1, EC135 T2, and EC135 T2+ helicopters, with a main rotor hub (MRH) shaft, part number (P/N) L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed, certificated in any category.

Related ADs

Superseded or revised by AD 2014-16-24.

Read the AD in the Federal RegisterReport an error on this page