AIRWORTHINESS DIRECTIVE

CAA-AD-026/2002

Date of issue: March 29, 2002

POWERED SAILPLANE – ENGINE INLET – MODIFICATION

Applicability: Powered gliders L13SW and L13SE produced by EVEKTOR s.r.o. all serial numbers, certificated in any category.

Reason: Possibility of intrusion of impurities into the carburettor, because of the non-protected engine inlet, which can lead to the engine failure.

Effective date: May 16, 2002.

Compliance : Upon receipt of this AD protect the engine inlet hole by means of the metal strainer in accordance with Mandatory Bulletin No.: SW13-053a dated February 1, 2002, which becomes herewith part of this AD and may be obtained from: EVEKTOR – AEROTECHNIK a.s., 686 04 Kunovice, Czech Republic, phone: +420 632/537 533, e-mail: jhron@evektor.cz.

Remarks:. The compliance of this AD must be recorded in Aircraft Logbook, where applicable the requirements of this AD must be integrated into Aircraft Technical Documentation. Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel: 420 2 33320922, fax: 420 2 20562270

Ing. Pavel MATOUŠEK
Director of Airworthiness Division
CAA CZ