AD 90-19-03

final rule
Data completeness: 70%

Airworthiness Directives; PIPER Model PA-38-112 Airplanes

AD Number
90-19-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-CE-03-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-38-112 Airworthiness Directives; PIPER Model PA-38-112 Airplanes

Unsafe Condition

Loosening of the landing gear attachments and possible gear separation.

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

Required Actions

Modify the main landing gear system in accordance with Piper Service Bulletin 673B. Airplanes may be flown under FAR 21.197 to a location where this AD can be accomplished. Alternate methods of compliance or compliance time adjustments may be approved by the Manager, Atlanta Aircraft Certification Office.

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 after the effective date of this AD, unless already accomplished

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

Affected Aircraft

PIPER Model PA-38-112 (all serial numbers) airplanes 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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