AD 2011-27-09

final rule
Data completeness: 70%

Airworthiness Directives; Socata Airplanes

AD Number
2011-27-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1139
FR Citation
77 FR 1622

Applicability

TypeManufacturerModelDetails
aircraft Socata TBM 700 Airworthiness Directives; Socata Airplanes
aircraft Aviat Various Airworthiness Directives; Socata Airplanes

Unsafe Condition

Installation of the wrong (switched) aileron control cables in the wing, leading to restricted movement of the aileron and reduced control of the airplane.

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

Required Actions

Inspect the aileron control cables in left and right wings for proper installation. If improperly installed, remove and correctly re-install the cables. After February 15, 2012, re-install using specified maintenance manual temporary revisions.

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

Compliance Time

Within 12 months after February 15, 2012, or within 100 hours time-in-service after February 15, 2012, whichever occurs first.

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

Affected Aircraft

Socata Model TBM 700 airplanes, serial numbers 1 through 572, 574, and 576, 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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