Airworthiness Directive
AD 2013-15-02: Bell Helicopter Textron Helicopters
Airworthiness Directives; Bell Helicopter Textron Helicopters
- Effective
- Aug 14, 2013
- Published
- Jul 30, 2013
- Registered aircraft
- 205
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
- Bell 205A
- Bell 205A-1
- Bell 205A-1
- Bell 205B
- Bell 212
- Bell 212
- Bell 412
- Bell 412
- Bell 412 CF
- Bell 412 RSAF
- Bell 412EP
- Bell 412EP
- Bell 412EP
- Only with: Tail rotor blade assembly P/N 210-010-001-(all dash numbers) or 212-010-750-(all dash numbers) installed.
- Only with: Tail rotor blade assembly P/N 210-010-001-(all dash numbers) or 212-010-750-(all dash numbers) installed.
Applicability
From the AD textThis AD applies to Bell Helicopter Textron (Bell) Model 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP helicopters with a tail rotor blade assembly (T/R blade), part number (P/N) 210-010-001-(all dash numbers) or 212-010-750-(all dash numbers), certificated in any category.
Related ADs
Supersedes or revises AD 2008-10-03.
Read the AD in the Federal RegisterReport an error on this page