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Airworthiness Directive

AD 2016-19-08 81 FR 64053 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-22183
Amendment
39-18657
Published
2016-09-19
Effective
2016-10-24
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2016-19-08 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2016-19-08

FR doc 2016-22183 · 81 FR 64053

AD 2016-19-08Published 2016-09-19Effective 2016-10-24

Superseded by 2016-25-22

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.

Unsafe condition: corrosion of the elevator control rod and of the elevator actuating lever on the control column.

Full official abstract

We are adopting a new airworthiness directive (AD) for Viking Air Limited Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as corrosion of the elevator control rod and of the elevator actuating lever on the control column. We are issuing this AD to detect and correct corrosion and/or cracking of the elevator control rod assemblies and the elevator actuating lever, which if not detected and corrected, could cause these components to fail. This failure could result in loss of control.

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  4. AD 2020-16-15 Airworthiness Directives; Viking Air Limited Airplanes 2020-08-17
  5. AD 2018-19-11 Airworthiness Directives; Viking Air Limited Airplanes 2018-09-25

All de Havilland DHC-2 Beaver directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2016-19-08 (opens in a new tab)

Applies to 1 model in our index