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Airworthiness Directive

AD 2011-22-05: Eurocopter France Model AS350B, B1, B2, B3, BA, C, D, and D1; and AS355E, F, F1, F2, N…

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

Effective
Nov 25, 2011
Published
Nov 10, 2011
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 350A33-2100-00, -01, -02, -03, -04; 350A33-2121-00, -01, -02; 350A33-2143-00; or 350A33-2145-00 or -01 installed.
  • Only with: Tail rotor pitch control rod P/N 350A33-2100-00, -01, -02, -03, -04; 350A33-2121-00, -01, -02; 350A33-2143-00; or 350A33-2145-00 or -01 installed.

Applicability

From the AD text
Eurocopter Model AS350B, B1, B2, B3, BA, C, D, D1; and Model AS355E, F, F1, F2, N, and NP helicopters; with tail rotor (T/R) pitch control rod (control rod), part number (P/N) 350A33-2100-00, -01, -02, -03, -04; P/N 350A33-2121-00, -01, -02; P/ N 350A33-2143-00; or P/N 350A33-2145-00 or -01, installed; certificated in any category.

Related ADs

Supersedes or revises AD 2003-22-06.

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