AD Amdt-39-10209

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Bombardier Model CL-600-1A11, -2A12, and -2B16 Series Airplanes

AD Number
Amdt-39-10209
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-285-AD
FR Citation
62 FR 61436

Applicability

TypeManufacturerModelDetails
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

AI-generated summary from the source AD text. Verify against the official source before acting.

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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