AD 2002-08-16

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model SA341G, SA342J, and SA-360C Helicopters

AD Number
2002-08-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-SW-72-AD
FR Citation
67 FR 19640

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model SA341G, SA342J, and SA-360C Airworthiness Directives; Eurocopter France Model SA341G, SA342J, and SA-360C Helicopters

Unsafe Condition

Failure of the main rotor head torsion tie bar, leading to loss of a main rotor blade and subsequent loss of control of the helicopter.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace each affected unairworthy main rotor head torsion tie bar with an airworthy tie bar. Revise the limitations section of the maintenance manual by adding and further reducing the life limit for certain tie bars.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Eurocopter France Model SA341G, SA342J, and SA-360C helicopters with affected main rotor head torsion tie bars.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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