AD 2009-05-01

final rule
Data completeness: 70%

Airworthiness Directives; Gippsland Aeronautics Pty. Ltd. Model GA8 Airplanes

AD Number
2009-05-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0155
FR Citation
74 FR 8159

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Gippsland Aeronautics Pty. Ltd. Model GA8 Airplanes

Unsafe Condition

Cracks in the Horizontal Stabiliser rear spar splice plate and inboard main ribs around the area of the Horizontal Stabiliser rear pivot attachment. Additionally, failure of some attach bolts in service may be due to improper assembly.

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

Required Actions

Within the next 10 hours time-in-service (TIS) after March 2, 2009, inspect for cracks in the Horizontal Stabiliser rear spar splice plate and inboard main ribs around the area of the Horizontal Stabiliser rear pivot attachment. Replace parts if nut and bolt mating surfaces are damaged or not square, and if previously repaired by spotfacing.

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

Compliance Time

Within 10 hours time-in-service (TIS) after March 2, 2009

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

Affected Aircraft

Gippsland Aeronautics Pty. Ltd. Model GA8 airplanes, serial numbers GA8-00-004 and up, 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 4, 2026

Rights: U.S. Government Public Domain

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