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federal_register: 03-31183

All Federal Register documents (rules, proposed rules, notices, presidential documents) from 1994 to present.

Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API

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document_number title type abstract publication_date pub_year pub_month html_url pdf_url agency_names agency_ids excerpts
03-31183 Airworthiness Directives; Bombardier Model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 Airplanes Proposed Rule This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all Bombardier Model DHC-8-101, - 102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This proposal would require a detailed inspection of the wing leading edge de-icer boots to determine if they comply with the patch size and/or patch number limits in the critical zone as defined in the Aircraft Maintenance Manual; 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. 2003-12-18 2003 12 https://www.federalregister.gov/documents/2003/12/18/03-31183/airworthiness-directives-bombardier-model-dhc-8-101--102--103--106--201--202--301--311-and--315 https://www.govinfo.gov/content/pkg/FR-2003-12-18/pdf/03-31183.pdf Transportation Department; Federal Aviation Administration 492,159 This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all Bombardier Model DHC-8-101, - 102, -103, -106, -201, -202, -301, -311, and -315 airplanes. This proposal would require a detailed inspection of the wing...

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