Airworthiness directives › 2013-11-03
AD 2013-11-03 Airworthiness Directives; Bombardier, Inc. Airplanes
Models named: CL-215-1A10. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Bombardier, Inc. Model CL-215-1A10 airplanes, serial numbers (S/Ns) 1001 through 1125 inclusive; and Model CL-215-6B11 (CL-215T Variant) airplanes, S/Ns 1056 through 1125 inclusive; certificated in any category.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
Within 10 flight hours after the effective date of this AD, do a detailed inspection for cracking of the left-hand (LH) and right-hand (RH) wing lower skin between wing stations (WS) 45.00 and 51.00, in accordance with Part A of Bombardier Alert Service Bulletin 215-A558, dated April 5, 2013. Repeat the inspection thereafter at intervals not to exceed 25 flight hours, until the inspection specified in paragraph (h)(1) or (h)(2) of this AD has been accomplished. If any cracking is found during the inspection required by paragraph (g) of this AD, before further flight, repair the crack using a method approved by the Manager, New York Aircraft Certification Office (ACO), FAA; or Transport Canada Civil Aviation (TCCA) (or its delegated agent).
Unsafe condition
This AD was prompted by reports of a fractured wing lower rear spar cap and reinforcing strap. We are issuing this AD to detect and correct cracked wing structure, which could result in failure of the wing.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1