AD 92-01-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Fan Jet Falcon Series G | Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes |
| aircraft | Dassault Aviation | Mystere-Falcon 200 | Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes |
Unsafe Condition
In-flight separation of the engine cowls due to failure of hinges and fasteners (latches and aprons).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 14 days after the effective date, and every 7 days thereafter, inspect hinges and fasteners on engine cowls per the maintenance manual. Replace discrepant parts before further flight. Reinforce latches per SB F200-59, install new hinge pin latching systems per SB F200-78, and reinforce small aprons/modify hinged cowl attachments per SB F200-87.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 14 days after the effective date of this AD, and thereafter at intervals not to exceed 7 days
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Affected Aircraft
Dassault Aviation Model Fan Jet Falcon Series G and Mystere Falcon 200 series airplanes, 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 8, 2026
Rights: U.S. Government Public Domain
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