AD 2011-23-03

final rule
Data completeness: 70%

Airworthiness Directives; SOCATA Airplanes

AD Number
2011-23-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0868
FR Citation
76 FR 67341

Applicability

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

Unsafe Condition

The electrical protection of some TBM 700 airplanes is insufficient to allow in-flight handling of the standby compass lighting cover when energized, leading to failure of both essential bus bars (ESS BUS 1 and ESS BUS 2) and loss of instruments and navigation systems.

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

Required Actions

Install a protection fuse on the wire at the standby compass connector as specified in SOCATA Service Bulletin 70-192-34.

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

Compliance Time

Within 12 months of the effective date (December 6, 2011).

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

Affected Aircraft

SOCATA Model TBM 700 airplanes, serial numbers 148, 434 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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