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Airworthiness Directive

AD 2013-11-03 78 FR 32353 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires repetitive detailed inspections for cracking of the left-hand (LH) and right-hand (RH) wing lower skin, and repair if necessary.

Superseded by AD 2019-02-05Federal Register (opens in a new tab)

FR document
2013-12615
Amendment
39-17463
Published
2013-05-30
Effective
2013-06-14
Models covered
1

Last live check: 2026-08-19

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AD

2013-11-03

FR doc 2013-12615 · 78 FR 32353

AD 2013-11-03Published 2013-05-30Effective 2013-06-14

Superseded by 2019-02-05

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 repetitive detailed inspections for cracking of the left-hand (LH) and right-hand (RH) wing lower skin, and repair if necessary.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-215-1A10 and CL-215-6B11 (CL-215T Variant) airplanes. This AD requires repetitive detailed inspections for cracking of the left-hand (LH) and right-hand (RH) wing lower skin, and repair if necessary. This AD also provides terminating action for the repetitive detailed inspections. 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.

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All Canadair CL-215 / CL-415 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2013-11-03 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index