Airworthiness Directive
AD 98-24-35: Eurocopter France Model AS-350B, B1, B2, BA, C, D, D1, and AS 355E, F, F1, F2, and N…
Airworthiness Directives; Eurocopter France Model AS-350B, B1, B2, BA, C, D, D1, and AS 355E, F, F1, F2, and N Helicopters
- Effective
- Dec 17, 1998
- Published
- Dec 2, 1998
- Registered aircraft
- 16
Models this AD may apply to
AI-extracted — verify against originalMatched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.
Aircraft
- Eurocopter France AS350B
- Eurocopter France AS350B2
- Eurocopter France AS350BA
- Eurocopter France AS355F1
- Eurocopter France AS355F2
- Eurocopter/France AS355N TWINSTAR
- Only with: Tail rotor pitch change control rod P/N 350A33-2145-01 installed.
- Only with: Tail rotor pitch change control rod P/N 350A33-2145-01 installed.
Applicability
From the AD textEurocopter France Model AS-350B, B1, B2, BA, C, D, D1, and AS 355E, F, F1, F2, and N helicopters, with tail rotor pitch change control rod (control rod), part number (P/N) 350A33-2145-01, installed, certificated in any category.
Related ADs
Superseded or revised by AD 2003-22-06.
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