AD 99-07-08

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model SA.315B Helicopters

AD Number
99-07-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-SW-57-AD
FR Citation
Federal Register: March 29, 1999 (Volume 64, Number 59)

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters SA.315B Alouette III Airworthiness Directives; Eurocopter France Model SA.315B Helicopters

Unsafe Condition

Bonding separation, corrosion, or a crack in the spar skin and main rotor blade root reinforcement strip area could result in blade failure 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 blade spar skin and root reinforcement strip area for bonding separation, corrosion, or cracks using 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, and thereafter at intervals not to exceed 100 hours time-in-service (TIS) or 6 months, whichever occurs first.

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

Affected Aircraft

Eurocopter France Model SA.315B helicopters with main rotor blades part numbers 3160S11-10000-all, 3160S11-30000-all, 3160S11-35000-all, 3160S11-40000-all, 3160S11-45000-all, 3160S11-50000-all, or 3160S11-55000-all.

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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