Airworthiness directives › 2005-11-07
AD 2005-11-07 Airworthiness Directives; Extra Flugzeugproduktions-und Vertriebs-GmbH Models EA-300, EA-300S, EA-300L, and EA-300/200 Airplanes
Makes named: extra. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(c) This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial numbers (1) Group A: (i) EA-300 0 through 67. (ii) EA-300S 0 through 31. (iii) EA-300L 0 through 167, 168 through 170 (or converted to 1168 through 1170), 1171, 172 (or converted to 1172), 173 (or converted to 1173), and 1174 through 1181. (iv) EA-300/200 0 through 31. (2) Group B: EA-300, EA-300S, EA-300L, and EA-300/200 All.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) For airplanes listed in Group A of paragraph (c)(1) of this AD: Seal with firewall sealant the gaps between the bottom fuselage cover (belly fairing) and the firewall Within the next 50 hours time-in-service (TIS) or 3 calendar months after July 18, 2005 (the effective date of this AD), whichever occurs first, unless already done Follow EXTRA Flugzeugproduktions-und Vertriebs-GmbH Service Bulletin No. 300-4-04, Issue: A, dated May 25, 2004. (2) For airplanes listed in Group B of paragraph (c)(1) of this AD: Whenever you install the bottom fuselage cover (belly fairing), do the sealing procedure required by paragraph (e)(1) of this AD As of July 18, 2005 (the effective date of this AD), whenever you install the bottom fuselage cover (belly fairing) Follow EXTRA Flugzeugproduktions-und Vertriebs-GmbH Service Bulletin No. 300-4-04, Issue: A, dated May 25, 2004.
Unsafe condition
(d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to prevent fuel from flowing behind the firewall in the case of a fuel leak. This could result in an in-flight fire, which could cause loss of the airplane and crew.
Affected ADs
(b) None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1