Aircraft model

de Havilland DH 83 Fox Moth

de Havilland

Airworthiness Directives
2
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-022 of 2 re-checked
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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What Airworthiness Directives apply to the de Havilland DH 83 Fox Moth

The FAA has published 2 Airworthiness Directives that name the de Havilland DH 83 Fox Moth (de Havilland), the earliest in 2014 and the newest on 2014-12-02.

Newest

  1. AD 2014-24-01 Airworthiness Directives; Various de Havilland Airplanes 2014-12-02
  2. AD 2014-17-09 Airworthiness Directives; Various de Havilland Airplanes 2014-09-03

See all 2 directives

The ones owners meet again

  1. AD 2014-24-01 Airworthiness Directives; Various de Havilland Airplanes 2014-12-02 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

2 records
ADAD 2014-24-01Various de Havilland Airplanes2015-01-06Active
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.

Various de Havilland Airplanes

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

Airworthiness Directives; Various de Havilland Airplanes

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.

Source: Federal Register document 2014-27789, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2014-17-09Various de Havilland Airplanes2014-09-18Active
AD

2014-17-09

FR doc 2014-20241 · 79 FR 52177

AD 2014-17-09Published 2014-09-03Effective 2014-09-18

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.

Various de Havilland Airplanes

Requires inspecting the aircraft maintenance records and/or the installed lateral fuselage tie rods and attaching nuts to determine the origin of manufacture.

Full official abstract

Airworthiness Directives; Various de Havilland Airplanes

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 requires inspecting the aircraft maintenance records and/or the installed lateral fuselage tie rods and attaching nuts to determine the origin of manufacture. This AD also requires immediately replacing lateral fuselage tie rods and attaching nuts produced by a specific manufacturer. 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. We are issuing this AD to correct the unsafe condition on these products.

Source: Federal Register document 2014-20241, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 2 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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