Airworthiness Directive

AD 2004-24-01 69 FR 69274 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-25674
Amendment
39-13877
Published
2004-11-29
Effective
2004-12-28
Models covered
1
Last live check
2026-10-01
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AD

2004-24-01

FR doc 04-25674 · 69 FR 69274

AD 2004-24-01Published 2004-11-29Effective 2004-12-28

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 you to replace the existing Viking Air Ltd.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all Bombardier Inc. Model (Otter) DHC-3 airplanes that have been modified by 524085 BC, Ltd. Supplemental Type Certificate (STC) Number ST01243NY or SA01243NY. This AD requires you to replace the existing Viking Air Ltd. elevator servo tab assembly with a redesigned Viking Air Ltd. elevator servo tab assembly. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Canada. There has been one failure of the elevator servo tab assembly. We are issuing this AD to prevent the structural failure of the elevator servo tab. This failure could lead to loss of control of the airplane.

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All de Havilland DHC-3 Otter directives

Applies to 1 model in our index