AD 2007-03-17

final rule
Data completeness: 70%

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

AD Number
2007-03-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-26234 Directorate Identifier 2006-CE-64-AD
FR Citation
72 FR 5923

Applicability

TypeManufacturerModelDetails
aircraft Socata TBM 700 Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes
aircraft Aviat Various Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition

Loose rivets on frames C18 BIS and C19, which could result in reduced structural integrity of the tail area.

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

Required Actions

Inspect frames C18 BIS and C19 for loose rivets. Replace any loose rivets as necessary. Ensure structural integrity is restored.

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

Compliance Time

Before further flight

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

Affected Aircraft

EADS SOCATA Model TBM 700 airplanes

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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