1、Designation: F2241 13F2241 14Standard Specification forContinued Airworthiness System for Powered ParachuteAircraft1This standard is issued under the fixed designation F2241; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year
2、 of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and the
3、irqualification for possible certification.1.2 This specification applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flightcertificates, flight permits, or other like documentation.1.3 This standard does not purport to address all of the safety concerns,
4、if any, associated with its use. It is the responsibilityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatoryrequirements prior to use.2. Referenced Documents2.1 ASTM Standards:2F2240 Specification for Manufacturer Quality As
5、surance Program for Powered Parachute Aircraft (Withdrawn 2014)3F2241 Specification for Continued Airworthiness System for Powered Parachute AircraftF2242 Specification for Production Acceptance Testing System for Powered Parachute AircraftF2243 Specification for Required Product Information to be P
6、rovided with Powered Parachute AircraftF2244 Specification for Design and Performance Requirements for Powered Parachute AircraftF2483 Practice for Maintenance and the Development of Maintenance Manuals for Light Sport AircraftF2563 Practice for Kit Assembly Instructions of Aircraft Intended Primari
7、ly for RecreationF2972 Specification for Light Sport Aircraft Manufacturers Quality Assurance System3. Terminology3.1 Definitions:3.1.1 powered parachute, naircraft comprised of a flexible or semi-rigid wing connected to a fuselage in such a way that thewing is not in position for flight until the a
8、ircraft is in motion. That aircraft has a fuselage with seats, engine, and wheels (or floats),such that the wing and engine cannot be flown without the wheels (or floats) and seat(s). Unique to the powered parachute is thelarge displacement between the center of lift (high) and the center of gravity
9、 (low), which is pendulum effect. Pendulum effectlimits angle of attack changes, provides stall resistance and maintains flight stability.4. Current Operators List Documentation4.1 The manufacturer shall maintain a list of registered aircraft owners that includes all aircraft in service by serial nu
10、mber,registration number, together with the name and address of the owner.4.2 In cases where the appropriate CivilAviationAuthority maintains records of registered owners sufficient for tracking aircraftand the manufacturer has access to such records, the manufacturer may elect to utilize such recor
11、ds for complying with this section.5. Monitoring, Investigation and Remedial Action5.1 The manufacturer shall maintain contact with dealers and owners who report incidents or other situations that might relateto safety, operations, or maintenance of aircraft produced and placed in service. The manuf
12、acturer will promptly investigate all1 This specification is under the jurisdiction ofASTM Committee F37 on Light SportAircraft and is the direct responsibility of Subcommittee F37.30 on Power Parachute.Current edition approved June 1, 2013Nov. 1, 2014. Published July 2013December 2014. Originally a
13、pproved in 2003. Last previous edition approved in 20082013 asF2241 05a (2008).F2241 13. DOI: 10.1520/F2241-13.10.1520/F2241-14.2 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information
14、 refer to the standards Document Summary page on the ASTM website.This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict a
15、ll changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to be considered the official document.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2
16、959. United States1reported failures, malfunctions, or defects and develop the appropriate corrective action. The magnitude of the service problem willdefine the subsequent publication to the operators.6. Safety Directives6.1 A safety directive will be distributed to all operators when a condition i
17、s found to exist that may also exist in other aircraftin the fleet and which would cause a deviation from original design or unsafe condition for flight, rendering the aircraftunairworthy. This change, maintenance procedure, inspection procedure, or other procedures deemed appropriate by themanufact
18、urer is mandatory and must be performed and documented in the individual aircraft logs in order for that aircraft tomaintain compliance with ASTM standards. When a safety directive is issued, immediately provide a copy to the appropriateairworthiness authority.7. Service Bulletin Documents7.1 Servic
19、e bulletins will be distributed to all operators by the manufacturer when no unsafe condition exists that could lead toan unairworthy condition, but a service problem has become repetitive for which the manufacturer has developed a design change,or service procedure change that will contribute to th
20、e improvement or convenience of operation or maintenance of the aircraft.Service bulletin changes are not mandatory to maintain the aircrafts compliance with ASTM Standards.8. Service Letter Documents8.1 The manufacturer will issue service letters on any subject that is considered helpful to the ope
21、rators. Such letters areintended to maintain a good rapport with the operators, encourage feedback on service and other problems, or to circulate itemsof interest that an operator may feel would be of value to other operators.Aservice letter does not include any mandatory operatoractions.9. Continua
22、tion of Airworthiness9.1 Copies MaintainedIn order to help insure that the fleet of aircraft remains airworthy even after the original manufacturerhas ceased to exist as a viable business entity, the original manufacturer shall maintain documentation on file showing compliancewith Specifications F22
23、40, F2241, F2242, F2243, F2244, and F2972 and Practices F2483, and F2563. This documentation showingcompliance with the specifications and any safety directives shall be copied and maintained at a physically safe location. Forpurposes of this specification, a physically safe location is one which is
24、 at least 33 m (100 ft) from the main production facility,such that a fire could not destroy both sets of records.9.2 Access AssuranceThis documentation should be available in such a manner that it can be obtained for commercial use inthe event that existing avenues of recovering the information is
25、destroyed. This documentation shall be retained even after theoriginal manufacturer ceases business activity such that in the event that a future entity wishes to continue supporting theairworthiness of the make and model involved, they may do so by making use of the original manufacturers documenta
26、tion. Theoriginal manufacturer may either keep these documents on file such that they will be available at any future date or shall turn themover to a responsible agency such as the FAA, or other industry entity, for safe keeping. The location and contact for accessingthese documents shall be presen
27、ted in theAircraft Operating Instructions, and any revision to this information shall be disseminatedthrough service bulletins to the aircraft owners.10. Keywords10.1 light sport aircraft; powered parachute aircraft; special airworthiness certificatesASTM International takes no position respecting t
28、he validity of any patent rights asserted in connection with any item mentionedin this standard. Users of this standard are expressly advised that determination of the validity of any such patent rights, and the riskof infringement of such rights, are entirely their own responsibility.This standard
29、is subject to revision at any time by the responsible technical committee and must be reviewed every five years andif not revised, either reapproved or withdrawn.Your comments are invited either for revision of this standard or for additional standardsand should be addressed to ASTM International He
30、adquarters. Your comments will receive careful consideration at a meeting of theresponsible technical committee, which you may attend. If you feel that your comments have not received a fair hearing you shouldmake your views known to the ASTM Committee on Standards, at the address shown below.This s
31、tandard is copyrighted by ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959,United States. Individual reprints (single or multiple copies) of this standard may be obtained by contacting ASTM at the aboveaddress or at 610-832-9585 (phone), 610-832-9555 (fax), or
32、 serviceastm.org (e-mail); or through the ASTM website(www.astm.org). Permission rights to photocopy the standard may also be secured from the Copyright Clearance Center, 222Rosewood Drive, Danvers, MA 01923, Tel: (978) 646-2600; http:/ The last approved version of this historical standard is referenced on www.astm.org.F2241 142
