EASA.SAS.A.041 Issue 01, 27/03/2007

Segelflugzeugbau A. Neukom Elfe

Page 1 of 2

European Aviation Safety Agency

EASA SPECIFIC AIRWORTHINESS
SPECIFICATION
for
Segelflugzeugbau A. Neukom Elfe
Models: Elfe S3, S4, S4A
as specified in Section I

. This Specific Airworthiness Specification is issued in accordance with Regulation (EC) 1592/2002 Article 15(1)(b). There is no valid Type Certificate for this aircraft type. The former type certificate holder was Segelflugzeugbau A. Neukom, CH-8213 Neunkirch, Switzerland.
List of effective Pages: Page 1 2 Issue 01 01

EASA.SAS.A.041 Issue 01, 27/03/2007

Segelflugzeugbau A. Neukom Elfe

Page 2 of 2

CONTENT
SECTION 1: Aircraft Design Definition
Refer to Type Certificate Data Sheet S 39-05 available on the Swiss FOCA website at: http://www.bazl.admin.ch/fachleute/lufttechnik/entwicklung/00507/index.html?lang=en

SECTION 2: Airworthiness Directives
Applicable Airworthiness Directives for this aircraft type can be located on the Swiss FOCA website at:
http://www.bazl.admin.ch/fachleute/lufttechnik/entwicklung/00656/index.html?lang=en
SECTION 3: Occurrence Reporting
The Specific Airworthiness Specification may be used as a basis for the issue of a Restricted Certificate of Airworthiness in accordance with 21A.173(b)(2) under the following conditions:
a) The holder of a Restricted Certificate of Airworthiness based on this Specific Airworthiness Specification shall report to the State of Registry all information related to occurrences associated with the operation of the aircraft which affects or could affect the safety of operation1.
b) Such reports shall be despatched within 72 hours of the time when the occurrence was identified unless exceptional circumstances prevent this.
c) The State of Registry shall forward the information received under (a) to the Agency when it relates to failures, malfunctions, defects or other occurrences which cause or might cause adverse effects on the continuing airworthiness of the aircraft.
SECTION 4: Other Limitations
[This is reserved for EASA use. Additional limitations may be necessary, as found necessary to reduce the risks associated with deficiencies in the reporting chain in Section 3. These may be based on the expectation that specific maintenance may be required due to aircraft ageing, etc.]

1 AMC 20-8 contains guidance describing the occurrences which are to be reported. This document can be found on the EASA website under Regulations>Certification Specifications:
http://www.easa.europa.eu/doc/Agency_Mesures/AMC_GM/decision_ED_2003_12_RM.pdf