Airworthiness Directive

AD 2003-17-02 68 FR 49688 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-20832
Amendment
39-13275
Published
2003-08-19
Effective
2003-10-10
Models covered
1
Last live check
2026-10-01
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AD

2003-17-02

FR doc 03-20832 · 68 FR 49688

AD 2003-17-02Published 2003-08-19Effective 2003-10-10

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 you to inspect the fuel selector valve for leakage and the wing for structural damage and correct any damage or leakage.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all EXTRA Flugzeugbau GmbH (EXTRA) Models EA-300/200, EA- 300L, and EA-300S airplanes. This AD requires you to inspect the fuel selector valve for leakage and the wing for structural damage and correct any damage or leakage. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to detect and correct fuel leakage in the wings, which could lead to structural damage of the wings and possible reduced structural margins. Reduced structural margins could lead to eventual structural failure.

More directives for Extra EA-300

  1. AD 2010-04-11 Airworthiness Directives; Extra Flugzeugproduktions- und Vertriebs- GmbH... 2010-02-23
  2. AD 2007-02-11 Airworthiness Directives; EXTRA Flugzeugproduktions-und Vertriebs-GmbH M... 2007-01-24
  3. AD 2005-11-07 Airworthiness Directives; Extra Flugzeugproduktions-und Vertriebs-GmbH M... 2005-06-07
  4. AD 2005-01-17 Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 and EA-300... 2005-01-19
  5. AD 2002-21-11 Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300S Airplanes 2002-10-25

All Extra EA-300 directives

Applies to 1 model in our index