AD 2016-13-09

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2016-13-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-8129
FR Citation
81 FR 44996

Applicability

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

Unsafe Condition

Premature wear and cracking of the horizontal stabilizer trim actuator (HSTA), which could result in failure of the HSTA and consequent loss of control of the airplane.

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Required Actions

Within 30 days after the effective date, revise the maintenance or inspection program to incorporate Task 27-42-01-109, Restoration (Overhaul) of the Horizontal Stabilizer Trim Actuator, and Task 27-42-01-111, Detailed Inspection of the Horizontal Trim Actuator (HSTA) Secondary Load Path Indicator.

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Compliance Time

Within 30 days after the effective date of this AD.

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Affected Aircraft

Bombardier, Inc. Model CL-600-2B16 (CL-604 Variant) airplanes, certificated in any category, serial numbers 5301 through 5665 inclusive, and 5701 through 5962 inclusive.

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Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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