AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2022-17-05 87 FR 52434 Active

Federal Aviation Administration · 14 CFR part 39

Requires either doing recurring visual inspections, borescope inspections, and non-destructive inspections (NDIs) of the struts and airframe lugs with corrective action as necessary or replacing the struts every 15 years and…

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
2022-18383
Amendment
39-22143
Published
2022-08-26
Effective
2022-09-30
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2022-17-05 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2022-17-05

FR doc 2022-18383 · 87 FR 52434

AD 2022-17-05Published 2022-08-26Effective 2022-09-30

Supersedes 2002-14-28

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 either doing recurring visual inspections, borescope inspections, and non-destructive inspections (NDIs) of the struts and airframe lugs with corrective action as necessary or replacing the struts every 15 years and doing recurring NDIs of the airframe lugs with corrective action as necessary.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2002-14- 28, which applied to all de Havilland Inc. (type certificate currently held by Viking Air Limited) Model DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III airplanes. AD 2002-14-28 established a life limit for the front fuselage struts and required repetitively replacing the front fuselage struts every 15 years or repetitively inspecting the struts for corrosion or fatigue damage and replacing when the damage exceeded a certain level. Since the FAA issued AD 2002-14-28, Transport Canada superseded its mandatory continuing airworthiness information (MCAI) to correct this unsafe condition on these products. This AD requires either doing recurring visual inspections, borescope inspections, and non-destructive inspections (NDIs) of the struts and airframe lugs with corrective action as necessary or replacing the struts every 15 years and doing recurring NDIs of the airframe lugs with corrective action as necessary. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for de Havilland DHC-2 Beaver

  1. AD 2023-19-06 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2023-11-06
  2. AD 2023-06-11 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2023-04-28
  3. AD 2020-16-15 Airworthiness Directives; Viking Air Limited Airplanes Effective 2020-09-21
  4. AD 2018-19-11 Airworthiness Directives; Viking Air Limited Airplanes Effective 2018-10-30
  5. AD 2016-25-22 Airworthiness Directives; Viking Air Limited Airplanes Effective 2016-12-22

All de Havilland DHC-2 Beaver directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (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