AD 2006-20-13

final rule
Data completeness: 80%

Airworthiness Directives; Fuji Heavy Industries, Ltd. FA-200 Series Airplanes

AD Number
2006-20-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25259
FR Citation
71 FR 59366

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Fuji Heavy Industries, Ltd. FA-200 Series Airplanes

Unsafe Condition

Corrosion of the flanges of the main wing spars, which could cause deterioration of wing strength.

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

Required Actions

Create inspection holes, inspect the flange of the wing spar for corrosion, repair corrosion if necessary, and remove the sealing compound. Repetitively inspect the flange of the wing spar for corrosion at intervals not to exceed 5 years, repairing corrosion before further flight if necessary.

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

Compliance Time

Within 1 year after the effective date of this AD.

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

Affected Aircraft

All FA-200 series airplanes, certificated in any U.S. 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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