Airworthiness Directive

AD 2004-14-18 69 FR 41928 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive detailed inspections of the left and right aileron tab actuator arm channels for cracking, and corrective actions if necessary.

FR document
04-15513
Amendment
39-13727
Published
2004-07-13
Effective
2004-08-17
Models covered
1

Last live check: 2026-08-19

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AD

2004-14-18

FR doc 04-15513 · 69 FR 41928

AD 2004-14-18Published 2004-07-13Effective 2004-08-17

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 repetitive detailed inspections of the left and right aileron tab actuator arm channels for cracking, and corrective actions if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, and -106 airplanes, that requires repetitive detailed inspections of the left and right aileron tab actuator arm channels for cracking, and corrective actions if necessary. This proposal also provides an optional terminating action for the repetitive inspections. This action is necessary to prevent increased roll forces due to cracking of the left and right aileron tab actuator arms, which could be interpreted by the pilot as a flight control problem and might lead to loss of control of the airplane. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index