Airworthiness Directive

AD 2004-05-01 69 FR 9523 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-4373
Amendment
39-13493
Published
2004-03-01
Effective
2004-04-20
Models covered
1
Last live check
2026-10-01
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AD

2004-05-01

FR doc 04-4373 · 69 FR 9523

AD 2004-05-01Published 2004-03-01Effective 2004-04-20

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.

The FAA adopts a new airworthiness directive (AD) for certain Bombardier Inc.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Bombardier Inc. (formerly deHavilland Inc.) Model Otter DHC-3 airplanes that have turbine engines installed per one of three supplemental type certificates (STC). This AD prohibits you from operating any affected airplane with these engine and propeller configurations unless a new STC for an elevator servo-tab with a redundant control linkage is installed. This AD is the result of reports of the control rod to the elevator servo-tab system detaching from the elevator servo-tab, which caused the elevator servo-tab to flutter on airplanes with a turbine engine installed. We are issuing this AD to prevent a single failure of the elevator servo-tab system, which could cause severe tab flutter. This failure could lead to possible loss of control of the airplane.

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All de Havilland DHC-3 Otter directives

Applies to 1 model in our index