AD 99-08-06

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B Helicopters

AD Number
99-08-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-SW-58-AD
FR Citation
Federal Register: April 07, 1999 (Volume 64, Number 66)

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters SA.316B Alouette III Airworthiness Directives; Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B Helicopters
aircraft Airbus Helicopters SA.316C Alouette III Airworthiness Directives; Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B Helicopters
aircraft Airbus Helicopters SA.319B Alouette III Airworthiness Directives; Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B Helicopters
aircraft Airbus Helicopters SE.3160 Alouette III Airworthiness Directives; Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B Helicopters

Unsafe Condition

Bonding separation, corrosion, or cracks in the spar skin and main rotor blade root reinforcement strip area could result in blade failure 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

Inspect the spar skin and blade root reinforcement strip area for bonding separation, corrosion, or cracks using a tapping method and visual inspection with a 3- to 7-power magnifying glass. Replace the blade if any separation, corrosion, or cracks are found.

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

Compliance Time

Before further flight for initial inspection, and repetitively at intervals not exceeding 100 flight hours or 6 calendar months, whichever comes first.

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

Affected Aircraft

Eurocopter France Model SE. 3160, SA. 316B, SA. 316C, and SA. 319B helicopters with specified main rotor blade part numbers installed.

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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