AD 86-17-02

final rule
Data completeness: 70%

Airworthiness Directives; ROGERSON HILLER CORP Model UH-12D, UH-12E, UH-12E4 Series and Military OH-23F and OH-23G Helicopters

AD Number
86-17-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12D Airworthiness Directives; ROGERSON HILLER CORP Model UH-12D, UH-12E, UH-12E4 Series and Military OH-23F and OH-23G Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; ROGERSON HILLER CORP Model UH-12D, UH-12E, UH-12E4 Series and Military OH-23F and OH-23G Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E-L Airworthiness Directives; ROGERSON HILLER CORP Model UH-12D, UH-12E, UH-12E4 Series and Military OH-23F and OH-23G Helicopters

Unsafe Condition

Cracks and failures in the main rotor blade fork P/N 52110-3 at the outboard tension-torsion bar retention bolt hole.

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

Required Actions

Verify each installed P/N 52110-3 fork has a serial number displayed; perform daily visual checks for cracks; conduct dye penetrant inspections every 100 hours' time in service, with initial inspections within 10 hours' time in service for forks with 240+ hours and prior to 250 hours' time in service for those with less. Replace cracked forks before flight.

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

Compliance Time

Within the next 10 hours' time in service after the effective date, and recurring intervals as specified.

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

Affected Aircraft

ROGERSON HILLER CORP Model UH-12D, UH-12E, UH-12E4 Series, Military OH-23F and OH-23G helicopters, including those converted under STC SH177WE and SH178WE, equipped with main rotor blade fork P/N 52110-3.

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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