Airworthiness Directive

AD 2004-20-03 69 FR 58043 Active

Federal Aviation Administration · 14 CFR part 39

Requires a detailed inspection of the wing leading edge de-icer boots to determine if they comply with certain patch limits in the critical zone; and corrective action, if necessary.

FR document
04-21646
Amendment
39-13808
Published
2004-09-29
Effective
2004-11-03
Models covered
1

Last live check: 2026-08-19

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AD

2004-20-03

FR doc 04-21646 · 69 FR 58043

AD 2004-20-03Published 2004-09-29Effective 2004-11-03

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 a detailed inspection of the wing leading edge de-icer boots to determine if they comply with certain patch limits in the critical zone; and corrective action, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model DHC-8-101, -102, -103, -106, -201, - 202, -301, -311, and -315 airplanes. This amendment requires a detailed inspection of the wing leading edge de-icer boots to determine if they comply with certain patch limits in the critical zone; and corrective action, if necessary. This action is necessary to prevent reduced aerodynamic smoothness of the wing leading edge de-icer boots and possible reduced stall margin, which could result in a significant increase in stall speeds, leading to a possible stall prior to activation of the stall warning. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index