AD 76-19-03

final rule
Data completeness: 70%

Airworthiness Directives; Hughes Model 369H, 369HS, 369HE and 369HM Helicopters

AD Number
76-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Fatigue failures of the damper plunger could result in loss of the stabilizer strut and possible contact with the tail rotor.

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

Required Actions

Disassemble the stabilizer strut P/N 369A2001-601 and inspect the damper plunger P/N 369A2130 or P/N 369A2130-3 for cut threads within 25 hours time in service after the effective date. If cut threads are found, before further flight, either replace the damper plunger with one having rolled threads or inspect for cracks using dye penetrant or magnetic particle inspection. If cracks are found, replace the damper plunger immediately; if not, replace within 100 hours additional time in service. Allow equivalent methods or alternate parts with FAA approval.

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 369H, 369HS, 369HE, and 369HM helicopters equipped with shock mounted stabilizer strut assembly P/N 369A2001-601.

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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