AD 82-16-07

final rule
Data completeness: 70%

Airworthiness Directives; HILLER AVIATION Model UH-12E, UH-12L, OH-23F and G Series Helicopters

AD Number
82-16-07
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-12L Airworthiness Directives; HILLER AVIATION Model UH-12E, UH-12L, OH-23F and G Series Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L4 Airworthiness Directives; HILLER AVIATION Model UH-12E, UH-12L, OH-23F and G Series Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; HILLER AVIATION Model UH-12E, UH-12L, OH-23F and G Series Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E-L Airworthiness Directives; HILLER AVIATION Model UH-12E, UH-12L, OH-23F and G Series Helicopters

Unsafe Condition

Cracks in the engine drive torsional coupling assembly housings P/N 21047-9, -11 (S/N 704 through 766), and P/N 21047-15 (all serial numbers) could lead to failure of the assembly.

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

Required Actions

Inspect the lower housing P/N 21046 in eight window areas adjacent to the engine attach flange using fluorescent penetrant inspection. Replace assemblies with cracked housings before further flight and install serviceable assemblies per maintenance manuals. Exclusions apply to helicopters with turbine engine installation via STC SH178WE.

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

Compliance Time

Within 10 hours' time in service after the effective date of this AD and thereafter at intervals not to exceed 50 hours' time in service

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

Affected Aircraft

Hiller Aviation/Siam Hiller Holdings, Inc. models UH-12E, UH-12L, OH-23F and G Series helicopters equipped with engine drive torsional coupling assemblies P/N 21047-9 (S/N 704-766), P/N 21047-11 (S/N 704-766), and P/N 21047-15 (all serial numbers)

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.