AD 70-16-07

final rule
Data completeness: 70%

Airworthiness Directives; Hughes Model 369 Series Helicopters

AD Number
70-16-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft MD Helicopters, Inc. 369 Airworthiness Directives; Hughes Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369A Airworthiness Directives; Hughes Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369H Airworthiness Directives; Hughes Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HE Airworthiness Directives; Hughes Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HM Airworthiness Directives; Hughes Model 369 Series Helicopters
aircraft MD Helicopters, Inc. 369HS Airworthiness Directives; Hughes Model 369 Series Helicopters

Unsafe Condition

Failure of the main rotor blade P/N 369A1100 and P/N 369A1100-501 due to cracks or doubler peeling or separation.

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

Required Actions

Determine identification notation on blade top and bottom doublers per Hughes Service Information Notice No. HN-8. Inspect blades with 'PR-12' stamps or lacking stamps before further flight, addressing cracks or separation. Repeat inspections every 25 hours until 100 hours post-AD effective date. Remove blades from service after 100 hours time in service from AD effective date.

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

Compliance Time

Within 25 hours time in service after the effective date of this AD

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

Affected Aircraft

Hughes Model 369 Series helicopters with main rotor blades P/N 369A1100 and P/N 369A1100-501, serial numbers listed in Hughes Service Information Notice No. HN-8 (November 19, 1969) or later FAA approved revision, and OH-6A Information Notices 120, 120A, 120B.

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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