AD 98-08-04

final rule
Data completeness: 70%

Airworthiness Directives; AERMACCHI S.p.A. Models S.208 and S.208A Airplanes.

AD Number
98-08-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-CE-140-AD
FR Citation
Federal Register: April 09, 1998 (Volume 63, Number 68)

Applicability

TypeManufacturerModelDetails
aircraft Aermacchi S.p.A. S.208 Airworthiness Directives; AERMACCHI S.p.A. Models S.208 and S.208A Airplanes.
aircraft Aermacchi S.p.A. S.208A Airworthiness Directives; AERMACCHI S.p.A. Models S.208 and S.208A Airplanes.

Unsafe Condition

Failure of the landing gear caused by an insufficient wire diameter of the rod springs, which could result in loss of control of the airplane during landing operations.

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

Required Actions

Inspect the landing gear rod springs to assure they are made with a wire diameter of 4.5 millimeters (mm). Replace any rod springs found to have a wire diameter of 4.0 mm prior to further flight after the inspection.

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

Compliance Time

Within the next 100 hours time-in-service (TIS) after the effective date of this AD

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

Affected Aircraft

Aermacchi S.p.A. Models S.208 and S.208A airplanes, 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

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