AD 2007-02-04

final rule
Data completeness: 70%

Airworthiness Directives; SOCATA-Groupe Aerospatiale TB 20 and TB 21 Airplanes

AD Number
2007-02-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-26236 Directorate Identifier 2006-CE-66-AD
FR Citation
72 FR 2606

Applicability

TypeManufacturerModelDetails
aircraft Socata Various Airworthiness Directives; SOCATA-Groupe Aerospatiale TB 20 and TB 21 Airplanes
aircraft Aviat Various Airworthiness Directives; SOCATA-Groupe Aerospatiale TB 20 and TB 21 Airplanes

Unsafe Condition

Interference between the wing spar lower boom and the wheel fairing attaching screw.

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

Required Actions

Inspect for interference between the wing spar lower boom and the wheel fairing attaching screw. If interference is found, take corrective action as specified in the AD.

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

SOCATA-Groupe Aerospatiale TB 20 and TB 21 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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