1、Designation: F2243 11 (Reapproved 2013)Standard Specification forRequired Product Information to be Provided with PoweredParachute Aircraft1This standard is issued under the fixed designation F2243; the number immediately following the designation indicates the year oforiginal adoption or, in the ca
2、se of revision, the year 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 requirements apply for the manufactureof powered parachute aircraft. This sp
3、ecification includes pilotoperating handbook requirements for powered parachute air-craft that were designed and manufactured in accordance withASTM standards.1.1.1 This specification covers the minimum requirementsfor information that shall be provided by the manufacturer orseller of new light spor
4、t aircraft, engines, or propellers as a partof the initial sale or transfer to the first end user.1.1.2 This specification does not apply to the sale or transferof used light sport aircraft, engines, or propellers.1.2 This specification applies to powered parachute aircraftseeking civil aviation aut
5、hority approval, in the form of flightcertificates, flight permits, or other like documentation.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health p
6、ractices and determine the applica-bility of regulatory requirements prior to use.2. Terminology2.1 Definitions:2.1.1 powered parachute, naircraft comprised of a flexibleor semi-rigid wing connected to a fuselage in such a way thatthe wing is not in position for flight until the aircraft is inmotion
7、. This aircraft has a fuselage with seats, engine, andwheels (or floats), such that the wing and engine cannot beflown without the wheels (or floats) and seat(s). Unique to thepowered parachute is the large displacement between thecenter of lift (high) and the center of gravity (low), which ispendul
8、um effect. Pendulum effect limits angle of attackchanges, provides stall resistance and maintains flight stability.3. Significance and Use3.1 The purpose of this specification is to provide theminimum information necessary for the proper identificationand operation of each light sport aircraft.4. In
9、formation Requirements4.1 The information given shall be included where appli-cable on the information plate as specified in 4.2. In addition,the documented operating and maintenance instructions speci-fied in Sections 5 and 6 are to be furnished by the manufactureror seller, at the time of initial
10、sale of each aircraft.4.2 Information PlateA manufacturer-issued fire proofinformation plate, printed in English or as defined by thegoverning civil aviation authority or agency in which theaircraft was initially sold, shall be permanently affixed to theaircraft in a visible location and shall be de
11、signed to remainlegible for the expected life of the aircraft. The informationplate shall be made of steel, and have the required informationeither stamped or engraved onto the plate.4.2.1 Serial NumberA manufacturer-issued unique identi-fying number or code affixed to the aircraft.4.2.2 Name and Ma
12、nufacturer, including the name of themanufacturers city, state, and country.4.2.3 Model NumberA manufacturer-issued unique iden-tifying number or code assigned to each manufactured type ofaircraft having the same structural design or components.4.2.4 Date of ManufactureThe date (month and year)deter
13、mined by the manufacturer that the aircraft met hisrequired design and manufacturing specifications.5. Aircraft Operating Instructions5.1 Each light sport aircraft must include an Aircraft Oper-ating Instructions which includes:5.1.1 Operating LimitationsThe instructions shall includelistings of all
14、 appropriate air-speed limitations for stall andmaximum speed, maximum wind limitations, weight andbalance, and power plant limitations.5.1.2 Operating DataThe instructions shall include infor-mation concerning normal and emergency procedures andother pertinent information.5.1.3 FormatThe Aircraft O
15、perating Instructions shallhave the following sections in order of listing1This specification is under the jurisdiction of ASTM Committee F37 on LightSport Aircraft and is the direct responsibility of Subcommittee F37.30 on PowerParachute.Current edition approved June 1, 2013. Published August 2013.
16、 Originallyapproved in 2003. Last previous edition approved in 2011 as F2243 11. DOI:10.1520/F2243-11R13.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States15.1.3.1 GeneralIncludes illustration of aircraft, lists theapproved engine(s), pr
17、opeller(s), fuel, and oil, and any defini-tions of abbreviations and terminology.5.1.3.2 LimitationsA listing of limits including but notlimited to the airspeed(s), approved maneuvers, and engineoperating limits.5.1.3.3 Emergency ProceduresA listing of emergencyprocedures for items such as engine fa
18、ilure, air restart, fire, etc.5.1.3.4 Normal ProceduresThis section shall cover themanufacturers recommended procedures for normal opera-tions such as preflight inspections, takeoff and landing.5.1.3.5 PerformanceInformation related to the perfor-mance of the aircraft in various environmental and op
19、eratingconditions such as fuel range, take off distances and landingdistances. Additional data shall be provided on performance at(at least one) different flight weight and at (at least one)different density altitude.5.1.3.6 Weight and BalanceInformation related to weightand center of gravity requir
20、ements for the safe operation of theaircraft.5.1.3.7 Description of the Aircraft and its SystemsAgeneral description of the aircraft, controls, instruments, andoptional equipment.5.1.3.8 Handling, Servicing and MaintenanceInformationrelated to the approved maintenance procedures, manuals andapproved
21、 sources for information or maintenance, or both.5.1.3.9 For powered parachute aircraft, the following addi-tional information shall be provided in the Aircraft OperatingInstructions, as required:(1) Aircraft SpeedMaximum and minimum speeds inmiles per hour.(2) Aircraft WeightMaximum and minimum tot
22、al aircraftflight weights.(3) Environmental RestrictionsRecommendations for op-erational restrictions relating to environmental conditions suchas, but not limited to, wind, rain, and extreme heat or cold.5.1.4 SupplementsThis section shall include any addi-tional information that the manufacturer wi
23、shes to add.5.1.5 Data Location and Contact Information, for recoveryof certification documentation, should the original manufac-turer lose its ability to support the make and model.6. Maintenance Manual6.1 Each aircraft shall have a maintenance manual providedfor the aircraft that covers the minimu
24、m of the requirements asdefined by the aircraft manufacturer.6.1.1 These shall include, as a minimum, mandatory para-chute assessment by manufacturer accepted personnel at theend of the second year of service and thereafter at the intervalsspecified by the parachute condition as specified by therevi
25、ewer and test.6.1.2 These tests shall include porosity, strength and defor-mation evaluations.7. Manufacturers Statement of Compliance7.1 Each aircraft, aircraft engine and propeller shall in-cluded a statement identifying the ASTM standards used forthe design, quality control, continued maintenance
26、, and pro-duction acceptance testing of the product and attesting to thefact that the product is in compliance with the provisions ofthose specifications.8. Operators Responsibility8.1 One of the following statements shall be included in thepilot operating handbook and posted in the aircraft passeng
27、erarea so that it is visible to both the pilot and passenger uponentry or when seated in the aircraft:8.1.1 “There are inherent risks in the participation in recre-ational aviation aircraft. Operators and passengers of recre-ational aviation aircraft, by participation, accept the risksinherent in su
28、ch participation of which the ordinary prudentperson is or should be aware. Pilots and passengers have a dutyto exercise good judgment and act in a responsible mannerwhile using the aircraft and to obey all oral or writtenwarnings, or both, prior to or during use of the aircraft, orboth.”8.1.2 “PASS
29、ENGER WARNING: This is a Special Light-Sport Aircraft and does not comply with federal safety regu-lations for standard aircraft.”9. Keywords9.1 light sport aircraft; powered parachute aircraft; specialairworthiness certificateASTM International takes no position respecting the validity of any paten
30、t 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 is subject to revision a
31、t 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 Headquarters. Your commen
32、ts 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 standard is copyrighted
33、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 serviceastm.org (e-mail); or through the ASTM website(www.astm.org). Permission rights to photocopy the standard may also be secured from the ASTM website (www.astm.org/COPYRIGHT/).F2243 11 (2013)2
