AD 97-20-15

final rule
Data completeness: 70%

Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters

AD Number
97-20-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
96-SW-32-AD
FR Citation
Federal Register: October 08, 1997 (Volume 62, Number 195)

Applicability

TypeManufacturerModelDetails
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12A Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12B Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12C Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12D Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters

Unsafe Condition

Cracks in the head area of the outboard tension-torsion (T-T) bar pin could result in loss of in-plane stability of the main rotor blade and subsequent loss of control of the helicopter.

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

Required Actions

Inspect the alignment of the outboard T-T bar pin and adjust if necessary; inspect the head of the outboard T-T bar pin for cracks using dye penetrant or magnetic particle inspection; install shims between the inboard end of the drag strut and the outboard T-T bar pin. Report inspection results to the FAA within 7 working days if cracks are found.

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

Compliance Time

Within 25 hours time-in-service (TIS) after the effective date of this AD, or at the next 100 hour inspection, whichever occurs first. Thereafter, inspections must be repeated at intervals not to exceed 100 hours TIS.

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

Affected Aircraft

Hiller Aircraft Corporation Model UH-12A, UH-12B, UH-12C, UH-12D, and UH-12E helicopters, certificated in any category.

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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