AD 2016-22-06

final rule
Data completeness: 70%

Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes

AD Number
2016-22-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9318
FR Citation
81 FR 74664

Applicability

TypeManufacturerModelDetails
aircraft Diamond Aircraft Industries GmbH Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes
aircraft Aviat Various Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes

Unsafe Condition

Cracked autopilot bridle cable clamps, potentially caused by overtorqueing, which could lead to detachment from the control system and reduced control of the airplane.

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

Required Actions

Inspect autopilot bridle cable clamps for cracks. Replace cracked clamps with redesigned clamps. Perform repetitive inspections as specified.

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

Diamond Aircraft Industries GmbH Models DA 40 NG, DA 42 NG, and DA 42 M-NG airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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