Airworthiness Directive

AD 2004-20-03 69 FR 58043

Federal Aviation Administration · 14 CFR part 39

FR document
04-21646
Amendment
39-13808
Published
2004-09-29
Models covered
1
Last live check
2026-08-17
AD

2004-20-03

FR doc 04-21646 · 69 FR 58043

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

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.

Applies to 1 model in our index