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Airworthiness Directive

AD 2004-22-11: Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters

Effective
Dec 7, 2004
Published
Nov 2, 2004
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 drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.
  • Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.

Applicability

From the AD text
Model EC135 P1, P2, T1, and T2 helicopters, with main rotor drive aluminum torque strut assembly (strut), part number (P/N) L633M1001 103 or L633M1001 105, installed, certificated in any category.

Related ADs

Supersedes or revises AD 2003-20-11.

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