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Airworthiness Directive

AD 98-08-13: Eurocopter France Model SA 330F, G, and J, and AS 332C, L, L1, and L2 Helicopters

Airworthiness Directives; Eurocopter France Model SA 330F, G, and J, and AS 332C, L, L1, and L2 Helicopters

Effective
Apr 27, 1998
Published
Apr 10, 1998
Registered aircraft
3

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

  • Eurocopter France AS332L1
  • Eurocopter France SA330J
  • Only with: Tail rotor head pitch change spider arm P/N 330A330104.20 or .21, or 332A330039.20 or .21 installed (SA 330 models); P/N 332A330039.20 or .21 installed (AS 332 models).
  • Only with: Tail rotor head pitch change spider arm P/N 330A330104.20 or .21, or 332A330039.20 or .21 installed (SA 330 models); P/N 332A330039.20 or .21 installed (AS 332 models).

Applicability

From the AD text
Model SA 330F, G, and J helicopters with tail rotor head pitch change spider arm (spider arm), part number (P/N) 330A330104.20 or .21, or 332A330039.20 or .21, installed and Model AS 332C, L, L1, and L2 helicopters with spider arm, P/N 332A330039.20 or .21 installed, certificated in any category.

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