Airworthiness Directive

AD 2005-15-11 70 FR 43025 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-14390
Amendment
39-14200
Published
2005-07-26
Effective
2005-08-30
Models covered
1
Last live check
2026-09-30
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AD

2005-15-11

FR doc 05-14390 · 70 FR 43025

AD 2005-15-11Published 2005-07-26Effective 2005-08-30

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 and specialized inspections to detect fatigue damage in the fuselage, replacement of certain bolt assemblies, and corrective actions if necessary.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. This AD requires repetitive detailed and specialized inspections to detect fatigue damage in the fuselage, replacement of certain bolt assemblies, and corrective actions if necessary. This AD results from a review of primary airframe fatigue test results and a Maintenance Steering Group 3 (MSG-3) analysis. We are issuing this AD to detect and correct fatigue damage of the fuselage, door, engine nacelle, empennage, and wing structures, which could result in reduced structural integrity of the airplane.

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  3. AD 2009-02-07 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-26
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All British Aerospace Jetstream 41 directives

Applies to 1 model in our index