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Airworthiness Directive

AD 2002-14-17: Eurocopter Deutschland GmbH Model EC135 Helicopters

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 Helicopters

Effective
Jul 26, 2002
Published
Jul 11, 2002
Registered aircraft
2

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

  • Eurocopter Deutschland Gmbh EC-135
  • Only with: Main rotor hub shaft assemblies P/N L623M1003 101, L623M1003 102, L623M1003 103, L623M1003 104, L623M1003 105, L623M1003 106, or L623F1003 107 installed.
  • Only with: Main rotor hub shaft assemblies P/N L623M1003 101, L623M1003 102, L623M1003 103, L623M1003 104, L623M1003 105, L623M1003 106, or L623F1003 107 installed.

Applicability

From the AD text
Model EC135 helicopters, with main rotor hub shaft (shaft) assemblies, part numbers L623M1003 101, L623M1003 102, L623M1003 103, L623M1003 104, L623M1003 105, L623M1003 106, or L623F1003 107, installed, certificated in any category.

Related ADs

Supersedes or revises AD 99-12-01.

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