Airworthiness Directive

AD 2009-02-07 74 FR 8732 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E9-3782
Amendment
39-15797
Published
2009-02-26
Effective
2009-03-13
Models covered
1
Last live check
2026-09-30
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AD

2009-02-07

FR doc E9-3782 · 74 FR 8732

AD 2009-02-07Published 2009-02-26Effective 2009-03-13

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 an eddy current conductivity test to measure the conductivity of the upper splice plate of the wing, and related investigative and corrective actions if necessary.

Full official abstract

The FAA is superseding an existing airworthiness directive (AD) that applies to certain British Aerospace (Jetstream) Model 4100 series airplanes. The existing AD currently requires an eddy current conductivity test to measure the conductivity of the upper splice plate of the wing, and related investigative and corrective actions if necessary. This AD revises the applicability to include additional airplanes. This AD results from reports of exfoliation corrosion of the upper splice plate of the wing. We are issuing this AD to detect and correct such corrosion, which could result in reduced structural integrity of the airplane.

More directives for British Aerospace Jetstream 41

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  2. AD 2009-10-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-05-07
  3. AD 2008-18-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-20
  4. AD 2008-17-04 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2008-08-19
  5. AD 2008-16-06 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2008-08-05

All British Aerospace Jetstream 41 directives

Applies to 1 model in our index