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Airworthiness Directive

AD 2001-13-19 66 FR 35538 Active

Federal Aviation Administration · 14 CFR part 39

Requires revising the Bombardier maintenance program to incorporate repetitive inspections to detect fatigue cracking in certain structures; and corrective actions, if necessary.

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FR document
01-16736
Amendment
39-12301
Published
2001-07-06
Effective
2001-08-10
Models covered
1

Last live check: 2026-08-19

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AD

2001-13-19

FR doc 01-16736 · 66 FR 35538

AD 2001-13-19Published 2001-07-06Effective 2001-08-10

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 revising the Bombardier maintenance program to incorporate repetitive inspections to detect fatigue cracking in certain structures; and corrective actions, if necessary.

1 correction to this AD FAA · 2001-08-27

Correction published 2001-08-27

Issued by
Federal Aviation Administration
Published
2001-08-27
Document
Federal Register 01-21490 · Final rule; correction

This document corrects information in an existing airworthiness directive (AD) that applies to all Bombardier Model DHC- 8-102, -103, -106, -201, -202, -301, -311, -314, and -315 series airplanes. That AD currently requires revising the Bombardier maintenance program to incorporate repetitive inspections to detect fatigue cracking in certain structures; and corrective actions, if necessary. This document corrects certain airplane models specified in Table 1 of the final rule. This correction is necessary to ensure that operators are notified of the correct airplane models, as specified in Canadian airworthiness directive CF-2000-07, dated March 3, 2000, and de Havilland Temporary Revision TR AWL 2-15, dated September 3, 1999.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 01-21490, retrieved 2026-08-17

Read this correction on Federal Register (opens in a new tab)
Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model DHC-8-102, -103, -106, -201, -202, - 301, -311, -314, and -315 series airplanes, that requires revising the Bombardier maintenance program to incorporate repetitive inspections to detect fatigue cracking in certain structures; and corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information issued by a foreign airworthiness authority. The actions specified by this AD are intended to ensure that fatigue cracking of certain principal structural elements is detected and corrected; such fatigue cracking could adversely affect the structural integrity of these airplanes.

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View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index