AD 2003-19-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eagle | Various | Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B Airplanes |
Unsafe Condition
Detachment of the rear spar bracket from the canard rear spar, which could result in failure of the canard rear spar.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the canard rear spar by adding additional laminated plies; modify the rear spar bracket; replace the existing console support bracket with a new part (P/N 3100D41-001); modify the Vinikor cap; install an additional support bracket (P/N 581B131-03) and rear spar bracket cap (P/N EO(VAR) 15566-01 or 581B131-02, as applicable).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours time-in-service after November 3, 2003, unless already accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B airplanes, serial numbers 001 through 003 and 005 through 030, 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 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.