AD 83-07-05 R3

final rule
Data completeness: 70%

Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters

AD Number
83-07-05 R3
Status
final_rule
Effective Date
Product Category
aircraft
Docket
83-ASW-12
FR Citation
Federal Register Volume 50, Number 171 (Wednesday, September 4, 1985)

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters AS355E Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS355F Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS350B Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS350B1 Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS350C Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS350D Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters
aircraft Airbus Helicopters AS350D1 Airworthiness Directives; AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 Series Helicopters

Unsafe Condition

Failure of the main rotor mast due to surface finish deterioration, corrosion, or cracks in the upper areas above the swashplate, particularly around the 12 flange bolt holes and the flange-to-shaft radius.

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

Required Actions

Inspect the main rotor mast for surface finish deterioration, corrosion, or cracks using visual and magnified inspection, followed by magnetic particle or dye penetrant inspection where finish deterioration exposes metal. Re-work or replace corroded masts per service bulletins. Repeat inspections at intervals not exceeding 300 hours time in service. Daily pre-flight inspections are required for AS-355 and AS-350 helicopters.

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Compliance Time

Compliance is required as indicated: within 50 hours time in service for helicopters with 250+ hours on the mast by the effective date; before reaching 300 hours time in service for those with less than 250 hours; before further flight for those with severe tracking defects. AS-355 and AS-350 helicopters must comply within 10 hours time in service from the effective date for subsequent inspections.

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

Affected Aircraft

AEROSPATIALE HELICOPTER CORPORATION (SNIAS) Model AS-350 and AS-355 series helicopters, including AS355E, AS355F, AS350B, AS350B1, AS350C, AS350D, AS350D1, certificated in all categories.

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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