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Airworthiness Directive

AD 2005-01-17 70 FR 2946 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the upper longeron cutout-bridge for cracks, to repair any cracks found, and to modify this area.

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FR document
05-607
Amendment
39-13942
Published
2005-01-19
Effective
2005-02-28
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2005-01-17 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

2005-01-17

FR doc 05-607 · 70 FR 2946

AD 2005-01-17Published 2005-01-19Effective 2005-02-28

Supersedes 98-03-14

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 upper longeron cutout-bridge for cracks, to repair any cracks found, and to modify this area.

Full official abstract

The FAA adopts a new airworthiness directive (AD) to supersede AD 98-03-14, which applies to certain EXTRA Flugzeugbau GmbH (EXTRA) Model EA-300 and EA-300/S airplanes. AD 98-03-14 currently requires you to inspect the upper longeron cutout-bridge for cracks, to repair any cracks found, and to modify this area. This AD retains the actions of AD 98-03-14 and incorporates new service information. For owner/ operators of the affected airplanes that were able to do the modification required in AD 98-03-14, no further action is required. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct cracks in the upper longeron cutout-bridge, which could cause the upper longeron cutout-bridge to fail resulting in structural damage to the fuselage. This condition could lead to loss of control of the airplane.

More directives for Extra EA-300

  1. AD 2010-04-11 Airworthiness Directives; Extra Flugzeugproduktions- und Vertriebs- GmbH... Effective 2010-03-30
  2. AD 2007-02-11 Airworthiness Directives; EXTRA Flugzeugproduktions-und Vertriebs-GmbH M... Effective 2007-02-28
  3. AD 2005-11-07 Airworthiness Directives; Extra Flugzeugproduktions-und Vertriebs-GmbH M... Effective 2005-07-18
  4. AD 2003-17-02 Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300/200, EA-3... Effective 2003-10-10
  5. AD 2002-21-11 Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300S Airplanes Effective 2002-12-17

All Extra EA-300 directives

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