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Airworthiness Directive

AD 2003-20-11: 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
Nov 14, 2003
Published
Oct 10, 2003
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 torque strut assembly P/N L633M1001 103 or L633M1001 105 installed.
  • Only with: Main rotor drive 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 torque strut assembly (strut), part number (P/N) L633M1001 103 or L633M1001 105, installed, certificated in any category.

Related ADs

Superseded or revised by AD 2004-22-11.

Supersedes or revises AD 2001-18-13.

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