Airworthiness Directive

AD 2012-05-05 77 FR 16151 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-6117
Amendment
39-16977
Published
2012-03-20
Effective
2012-04-24
Models covered
1
Last live check
2026-10-02
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AD

2012-05-05

FR doc 2012-6117 · 77 FR 16151

AD 2012-05-05Published 2012-03-20Effective 2012-04-24

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires inspecting the bracket assembly of the emergency water dump pulley to determine if certain rivets are installed; replacing rivets and installing new stiffeners on the bracket assembly, if necessary; inspecting the…

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-215-1A10, CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant) airplanes. This AD was prompted by reports of cracked or broken support bracket assemblies of the emergency water dump pulley. This AD requires inspecting the bracket assembly of the emergency water dump pulley to determine if certain rivets are installed; replacing rivets and installing new stiffeners on the bracket assembly, if necessary; inspecting the stiffeners for the bracket assembly for cracks, deformation, or corrosion, and replacement if necessary; and re-installing the bracket assembly with radius packers. We are issuing this AD to detect and correct failure of the support bracket assembly of the emergency water dump pulley, and in combination with other system failures, such as an engine failure during take off or a pitch control system jam, may result in loss of controllability of the airplane.

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All Canadair CL-215 / CL-415 directives

Applies to 1 model in our index