AD 2004-12-06

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model EC 155 B and B1 Helicopters

AD Number
2004-12-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2004-SW-05-AD
FR Citation
69 FR 32857

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model EC 155 B and B1 Airworthiness Directives; Eurocopter France Model EC 155 B and B1 Helicopters

Unsafe Condition

Crack in the blade tip cap mounting bracket (tenon), which could result in loss of the tip cap, leading to severe vibration and loss of control of the helicopter.

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

Required Actions

Inspect each main rotor blade tenon for cracks. Replace the blade if a crack is found. Measure vertical clearance between each blade assembly and a straight edge at the blade-to-tip cap junction. Replace the blade if the measured distance is not within specified limits.

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 EC 155 B and B1 helicopters.

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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