AD 2007-02-13

final rule
Data completeness: 70%

Airworthiness Directives; DORNIER LUFTFAHRT GmbH Model 228-212 Airplanes

AD Number
2007-02-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-26597
FR Citation
72 FR 3355

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; DORNIER LUFTFAHRT GmbH Model 228-212 Airplanes

Unsafe Condition

Loose bolts or self-locking nuts in the landing gear carbon brake assembly could result in the brake assembly detaching and malfunctioning, degrading brake performance and potentially causing loss of control during landing and roll-out.

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

Required Actions

Inspect the landing gear carbon brake assembly to detect loose bolts or self-locking nuts. Replace any loose bolts or self-locking nuts found during the inspection.

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

DORNIER LUFTFAHRT GmbH Model 228-212 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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