AD 2013-15-05

final rule
Data completeness: 80%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2013-15-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0216
FR Citation
78 FR 47529

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Airplanes

Unsafe Condition

Flap actuator inboard pinion seal is prone to leak, causing internal contamination of the actuator braking mechanism and subsequent actuator failure, which can lead to flap system failure and reduced control of the airplane.

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

Required Actions

Revise the maintenance program by incorporating new airworthiness limitation tasks (Tasks C27-50-111-15 and C27-50-111-17) within 30 days after the effective date of the AD.

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

Compliance Time

Within 30 days after the effective date of the AD.

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

Affected Aircraft

Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes equipped with Eaton flap actuators having part numbers 601R93101-23/-25, 601R93103-23/-24, or 601R93104-23/-24.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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