AD 2009-08-09

final rule
Data completeness: 70%

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

AD Number
2009-08-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0124 Directorate Identifier 2009-CE-004-AD
FR Citation
74 FR 17386

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

A damaged wiring harness, resulting from chafed wires due to interference with under-floor attachment fittings of the cabin partition net caused by incorrect routing on the production line, which can lead to an electrical short and potential loss of essential safety functions.

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

Required Actions

Inspect the electrical wiring harness at frame C14 and between frames C16 and C17 for wire chafing and incorrect routing. If wire chafing or incorrect routing is found, repair and reroute the electrical harness before further flight.

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

Compliance Time

Within 100 hours time-in-service or 12 months after May 20, 2009, whichever occurs first.

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

Affected Aircraft

EADS SOCATA Model TBM 700 airplanes, serial numbers 434 through 478, 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 6, 2026

Rights: U.S. Government Public Domain

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