AD Amdt-39-11239

Recurring final rule
Data completeness: 70%

Airplanes

AD Number
Amdt-39-11239
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-370-AD
FR Citation
64 FR 41775

Applicability

TypeManufacturerModelDetails
aircraft Bombardier CL-215-1A10 and CL-215- 6B11 Airplanes

Unsafe Condition

Cracking on certain wing to fuselage frame-angles, which could result in reduced structural integrity of the airframe.

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

Required Actions

Continue to perform repetitive inspections to detect cracking on certain wing to fuselage frame-angles. Repair, if necessary.

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.

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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View Official Source ↗ Find More ADs for Bombardier CL-215-1A10 and CL-215- 6B11

Related Airworthiness Directives

2005-18-05 Recurring

final rule

Airworthiness Directives; Bombardier Model CL-215-1A10 (Water Bomber), CL-215-6B11 (CL215T Variant), and CL-215-6B11 (CL415 Variant) Airplanes

Unsafe Condition: could result in reduced structural integrity of the airplane.

Effective: Oct 6, 2005 Category: aircraft

View all Bombardier ADs →