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Airworthiness Directive

AD 2003-22-06: Eurocopter France Model AS350B, B1, B2, B3, BA, C, D, D1, and AS355E, F, F1, F2, and N…

Airworthiness Directives; Eurocopter France Model AS350B, B1, B2, B3, BA, C, D, D1, and AS355E, F, F1, F2, and N Helicopters

Effective
Dec 3, 2003
Published
Oct 29, 2003
Registered aircraft
24

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: Tail rotor pitch control rod P/N 350A33-2145-00 or 350A33-2145-01 installed.
  • Only with: Tail rotor pitch control rod P/N 350A33-2145-00 or 350A33-2145-01 installed.

Applicability

From the AD text
Eurocopter France Model AS350B, B1, B2, B3, BA, C, D, D1, and AS355E, F, F1, F2, and N helicopters, with tail rotor pitch control rod (control rod), part number (P/N) 350A33-2145-00 or 350A33-2145-01, installed, certificated in any category.

Related ADs

Superseded or revised by AD 2011-22-05.

Supersedes or revises AD 98-24-35.

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