AD 2014-13-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Diamond | Aircraft Industries GmbH | Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes |
Unsafe Condition
The fatigue strength found in the aft main spar not ensuring unlimited lifetime structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the aft main spar in the cabin area to ensure the structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 2,000 hours time-in-service (TIS) after August 27, 2014, or within the next 114 months after August 27, 2014, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Diamond Aircraft Industries GmbH Models DA40 and DA40F airplanes, serial numbers 40.006 through 40.009, 40.011 through 40.1071, and 40.1073 through 40.1077; and Model DA40F airplanes, serial numbers 40.FC001 through 40.FC029; 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 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.