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Airworthiness Directive

AD 2001-17-32: Eurocopter France Model AS350B, B1, B2, B3, BA, D, D1 and AS355E, F, F1, F2, and N…

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

Effective
Oct 4, 2001
Published
Aug 30, 2001
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 change spider assembly P/N 350A33-2004-00, -01, -02, -03, -05, or 350A33-2009-00 or -01 installed, and MOD 076554 not incorporated.
  • Only with: Tail rotor pitch change spider assembly P/N 350A33-2004-00, -01, -02, -03, -05, or 350A33-2009-00 or -01 installed, and MOD 076554 not incorporated.

Applicability

From the AD text
AS350B, B1, B2, B3, BA, D, D1 and AS355E, F, F1, F2, and N helicopters, with tail rotor pitch change spider assembly (spider assembly), part number (P/N) 350A33-2004-00, -01, -02, -03, -05, or 350A33-2009-00 or -01, installed, and which do not incorporate MOD 076554, certificated in any category.

Related ADs

Supersedes or revises AD 99-24-18.

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