AD 2009-14-03

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes

AD Number
2009-14-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0044
FR Citation
74 FR 32411

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes
aircraft Aviat Various Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes

Unsafe Condition

Stick Pusher Capstan Shaft failures causing dormant loss or severe degradation of the stick pusher function.

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

Required Actions

Revise the Normal Procedures section of the applicable airplane flight manual (AFM) by inserting a copy of the applicable temporary revision (TR) listed in Table 2 of this AD. Operate the airplanes per the procedures specified in the applicable TR. If the operator has an AFM not listed in Table 2, revise the AFM using a method approved by the FAA or Transport Canada Civil Aviation (TCCA).

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 this AD.

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

Affected Aircraft

Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) airplanes, with serial numbers as listed in Table 1 of the AD.

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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