AD 99-07-02

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters

AD Number
99-07-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-SW-46-AD
FR Citation
(Federal Register: March 23, 1999 (Volume 64, Number 55))

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters AS332C Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters AS332L Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters AS332L1 Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters AS332L2 Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters SA330F Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters SA330G Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters
aircraft Airbus Helicopters SA330J Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters and Model SA 330F, G, and J Helicopters

Unsafe Condition

Mislocated and improperly bonded main rotor blade leading edge stainless steel protective strips replaced by C.T.I. Dallas could result in failure of the 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

Inspect blade strips for correct positioning within 10 hours time-in-service (TIS) by measuring distance from tip cap-blade junction (2228 mm ±15 mm). If mislocated, remove blade and replace with airworthy blade within 100 hours TIS. Additionally, inspect strips for proper bonding within 100 hours TIS and thereafter every 100 hours TIS using a bonding check by sound; replace blade if defects found.

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

Compliance Time

Within 10 hours time-in-service (TIS) for initial inspection, and within 100 hours TIS for subsequent inspections, with repetitive inspections not exceeding 100 hours TIS.

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

Affected Aircraft

Eurocopter France Model AS 332C, L, L1, L2 and SA 330F, G, J helicopters with main rotor blades part numbers 330A11-0020, 330A11-0022, or 330A11-0027 (all dash numbers).

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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