AD 2020-26-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream | Aerospace LP | Airworthiness Directives; Gulfstream Aerospace LP Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Gulfstream Aerospace LP Airplanes |
Unsafe Condition
solder cracking of the flight control electronic control units (FCECUs), which, combined with latent failure of the horizontal stabilizer trim actuator (HSTA) ``no-back'' mechanism, could result in uncontrolled HSTA operation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Comply with all required actions and compliance times specified in, and in accordance with, Civil Aviation Authority of Israel (CAAI) AD ISR-I-04-2020-06-02, dated June 28, 2020 (CAAI AD ISR-I-04-2020-06-02).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 work-hours per operator, although the agency recognizes that this number may vary from operator to operator.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Gulfstream Aerospace LP Model Gulfstream G280 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before September 15, 2019.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.