AD 98-04-48

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS 332L2 Helicopters

AD Number
98-04-48
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-SW-29-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters AS332L2 Airworthiness Directives; Eurocopter France Model AS 332L2 Helicopters

Unsafe Condition

Failure of a vibration absorber weight support assembly, part number 332A11-0470-00, could lead to adverse vibrations, contact between the fuselage and a main rotor blade, or loss of a main rotor blade, resulting in 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 the weight support assemblies, part number 332A11-0470-00, with reinforced weight support assemblies, part number 332A11-0474-00, in accordance with Eurocopter France Service Bulletin No. 62.00.43 dated February 13, 1997. Convert vibration absorbers from part number 332A11-0460-01 to 332A11-0460-02 as specified.

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

Compliance Time

within 25 hours time-in-service (TIS) after the effective date of this AD, unless accomplished previously

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

Affected Aircraft

Eurocopter France Model AS 332L2 helicopters with main rotor blade vibration absorbers, part number 332A11-0460-01, installed, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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