AD 98-08-13

final rule
Data completeness: 70%

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

AD Number
98-08-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-SW-27-AD
FR Citation
Federal Register: April 10, 1998 (Volume 63, Number 69)

Applicability

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

Unsafe Condition

Fatigue cracking in the tail rotor head pitch change spider (spider), part numbers 332A330039.20 or .21 for Model AS 332 helicopters, and 330A330104.20 or .21 for Model SA 330 helicopters, could result in failure of the spider arm, loss of control of the tail rotor 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

Perform daily inspections before first flight of each day at the root of each spider arm for cracks, and conduct detailed inspections within 250 hours time-in-service for cracks and fretting corrosion. Install an airworthy modified, replacement, or repaired spider as a terminating action.

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

Compliance Time

within 250 hours time-in-service (TIS)

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

Affected Aircraft

Eurocopter France Model SA 330F, G, J, and AS 332C, L, L1, L2 helicopters with specific part numbers 330A330104.20/.21 or 332A330039.20/.21 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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