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Airworthiness Directive

AD 2016-23-05: Airbus Helicopters (Previously Eurocopter France) Helicopters

Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France) Helicopters

Effective
Dec 12, 2016
Published
Nov 25, 2016
Registered aircraft
6

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

  • Airbus Helicopters EC 155B1
  • Eurocopter France AS-365N2
  • Eurocopter France SA-365N1
  • Only with: Tail rotor gearbox pitch control rod assembly double bearing P/N 704A33-651-093 or P/N 704A33-651-104 installed.
  • Only with: Tail rotor gearbox pitch control rod assembly double bearing P/N 704A33-651-093 or P/N 704A33-651-104 installed.

Applicability

From the AD text
This AD applies to Model SA-365N1, AS-365N2, AS 365 N3, SA-366G1, EC 155B, and EC155B1 helicopters with a tail rotor gearbox (TGB) pitch control rod assembly double bearing (bearing) part number (P/N) 704A33-651-093 or P/N 704A33-651-104 installed, certificated in any category.

Related ADs

Superseded or revised by AD 2021-05-05.

Supersedes or revises AD 2007-25-08.

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