EASA Regulations for Daher Aircraft Design KODIAK 100

2 airworthiness directives and regulations affecting Daher Aircraft Design KODIAK 100.

EASA AD US-2020-13-01

[Correction] Landing Gear - Nose Landing Gear Fork - Inspection

The Correction to Airworthiness Directive 2020-13-01 issued by the Federal Aviation Administration (FAA) addresses the nose landing gear fork inspection requirements for Daher Aircraft Design, LLC Model KODIAK 100 airplanes. This correction clarifies the type certificate holder's name and republishes the entire rule without changing the original inspection and replacement requirements for the nose landing gear fork and shimmy damper system.

Aug 10, 2020

Airworthiness DirectiveMaintenanceSafety MgmtDaher Aircraft Design, KODIAK 100Daher Aircraft Design KODIAK 100

EASA AD US-2020-04-13

Aircraft Pilot's Operating Handbook and Airplane Flight Manual - Revision

The Aircraft Pilot's Operating Handbook and Airplane Flight Manual - Revision is a final rule airworthiness directive issued by the FAA affecting all Daher Aircraft Design, LLC Model KODIAK 100 airplanes. This directive addresses incorrect low weight landing distances published in the performance section of the pilot's operating handbook and airplane flight manual or supplement 5. The AD mandates updating these manuals to ensure accurate obstacle landing distance data.

Mar 26, 2020

Airworthiness DirectiveFlight OpsSafety MgmtDaher Aircraft Design, KODIAK 100Daher Aircraft Design KODIAK 100