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Airworthiness Directive

AD 2014-24-01 79 FR 71302 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the aircraft maintenance records to determine the date of installation or the date of last replacement of the lateral fuselage tie rods.

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FR document
2014-27789
Amendment
39-18034
Published
2014-12-02
Effective
2015-01-06
Models covered
2

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2014-24-01 · 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

2014-24-01

FR doc 2014-27789 · 79 FR 71302

AD 2014-24-01Published 2014-12-02Effective 2015-01-06

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 aircraft maintenance records to determine the date of installation or the date of last replacement of the lateral fuselage tie rods.

Full official abstract

We are adopting a new airworthiness directive (AD) for all Harry E. Williams de Havilland Model DH 82A airplanes, all Cliff Robertson de Havilland Model DH 82A airplanes, and all de Havilland Model DH 83 airplanes. This AD was prompted by reports of structural failure of the attachment of the wing to the fuselage that resulted from failed lateral fuselage tie rods. This AD requires inspecting the aircraft maintenance records to determine the date of installation or the date of last replacement of the lateral fuselage tie rods. This AD also requires repetitively replacing all lateral fuselage tie rods and attaching nuts at a specified life limit interval. We are issuing this AD to correct the unsafe condition on these products.

More directives for de Havilland DH 82A Tiger Moth

  1. AD 2014-17-09 Airworthiness Directives; Various de Havilland Airplanes Effective 2014-09-18

All de Havilland DH 82A Tiger Moth 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 2 models in our index