AD 77-02-10

final rule
Data completeness: 70%

Airworthiness Directives; CANADAIR Models CL-44D4 and CL-44J Airplanes

AD Number
77-02-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. CL-44D4 Airworthiness Directives; CANADAIR Models CL-44D4 and CL-44J Airplanes
aircraft Bombardier Inc. CL-44J Airworthiness Directives; CANADAIR Models CL-44D4 and CL-44J Airplanes

Unsafe Condition

Corrosion in the fuselage skin where the bonding strip under the ice guards contacts the fuselage.

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

Required Actions

Inspect bonding strip in accordance with Canadair Service Information Circular No. 385-CL44 or approved equivalent. Replace bonding strips and repair fuselage skin if corrosion is detected. Repetitive inspections apply even if bonding strips were replaced with aluminum alloy.

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

Compliance Time

within the next six months, unless already accomplished within the last six months, and thereafter at subsequent intervals not to exceed twenty-four months, after the effective date of this AD

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

Affected Aircraft

Bombardier Inc. Models CL-44D4 and CL-44J airplanes, certificated in all categories.

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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