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Airworthiness Directive

AD 2015-17-01: Airbus Helicopters (Previously Eurocopter France) (Airbus Helicopters) Helicopters

Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France) (Airbus Helicopters) Helicopters

Effective
Sep 24, 2015
Published
Aug 20, 2015
Registered aircraft
387

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 hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, or pitch horn P/N 350A121368.XX, installed.
  • Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, or pitch horn P/N 350A121368.XX, installed.

Applicability

From the AD text
This AD applies to Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters with tail rotor hub pitch horn (pitch horn) assembly, part number (P/N) 350A121368.01, 350A121368.02, 350A121368.03, or 350A121368.04, with a pitch horn, P/N 350A121368.XX, where XX stands for a two-digit dash number, installed, certificated in any category. The pitch horn may be marked with either the pitch horn assembly P/N or pitch horn P/N.

Related ADs

Supersedes or revises AD 2013-21-01.

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