AD 2004-03-13

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Bombardier Model CL-215-1A10 and CL-215-6B11 Series Airplanes

AD Number
2004-03-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-139-AD
FR Citation
69 FR 6538

Applicability

TypeManufacturerModelDetails
aircraft Bombardier CL-215-1A10 and CL-215-6B11 Airworthiness Directives; Bombardier Model CL-215-1A10 and CL-215-6B11 Series Airplanes

Unsafe Condition

Cracking of the inner bearing surface of the main landing gear (MLG) axles, which could result in axle failure and wheel separation, leading to reduced controllability during takeoff or landing.

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

Required Actions

Perform a dimensional check of the MLG axles. Take follow-on corrective actions as necessary. Terminate the applicability for certain airplanes as specified.

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-215-1A10 and CL-215-6B11 series airplanes, including three additional airplanes added to the existing AD.

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.