AD Amdt-39-10209
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | CL-600-1A11 | Airworthiness Directives; Bombardier Model CL-600-1A11, -2A12, and -2B16 Series Airplanes |
Unsafe Condition
Cracking in the pressure bulkhead at frame station (FS) 409.00 could result in uncontrolled depressurization of the airplane and/or reduced structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections to detect cracks in the fuselage bulkhead web at specified locations, repair as necessary, and follow mandatory continuing airworthiness information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Bombardier Model CL-600-1A11, -2A12, and -2B16 series airplanes subject to mandatory continuing airworthiness information from a foreign civil airworthiness authority.
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
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