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ASTM F2243-05

(Specification)

Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft

Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft

ABSTRACT
This specification covers the requirements that apply for the manufacture of powered parachute aircraft; it includes pilot operating handbook requirements for powered parachute aircraft. This applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other similar documentation. Each light sport aircraft must include an aircraft operating instructions which includes: operating limitations, operating data, format; supplements, and data location and contact information. Each aircraft shall have a maintenance manual provided for the aircraft that covers the minimum of the requirements as defined by the aircraft manufacturer.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured in accordance with ASTM standards.
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first end user.
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers.
1.2 This specification applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation.
This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory requirements prior to use.

General Information

Status
Historical
Publication Date
28-Feb-2005
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F37 - Light Sport Aircraft
Drafting Committee
F37.30 - Power Parachute
Current Stage
Ref Project

Relations

Replaces
ASTM F2243-03 - Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft
Effective Date
01-Mar-2005
Replaced By
ASTM F2243-11 - Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft
Effective Date
01-Nov-2011
Referred By
ASTM F2244-14(2022) - Standard Specification for Design and Performance Requirements for Powered Parachute Aircraft
Effective Date
01-Mar-2005
Referred By
ASTM F2426-13(2018)e1 - Standard Guide on Wing Interface Documentation for Powered Parachute Aircraft
Effective Date
01-Mar-2005
Referred By
ASTM F3060-20 - Standard Terminology for Aircraft
Effective Date
01-Mar-2005

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ASTM F2243-05 - Standard Specification for Required Product Information to be Provided with Powered Parachute AircraftASTM F2243-05 - Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft
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ASTM F2243-05 - Standard Specification for Required Product Information to be Provided with Powered Parachute Aircraft
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Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F2243 – 05
Standard Specification for
Required Product Information to be Provided with Powered
1
Parachute Aircraft
This standard is issued under the fixed designation F2243; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope 3. Significance and Use
1.1 The following requirements apply for the manufacture 3.1 The purpose of this specification is to provide the
of powered parachute aircraft. This specification includes pilot minimum information necessary for the proper identification
operating handbook requirements for powered parachute air- and operation of each light sport aircraft.
craft that were designed and manufactured in accordance with
4. Information Requirements
ASTM standards.
4.1 The information given shall be included where appli-
1.1.1 This specification covers the minimum requirements
for information that shall be provided by the manufacturer or cable on the information plate as specified in 4.2. In addition,
the documented operating and maintenance instructions speci-
seller of new light sport aircraft, engines, or propellers as a part
of the initial sale or transfer to the first end user. fied in Sections 5 and 6 are to be furnished by the manufacturer
or seller, at the time of initial sale of each aircraft.
1.1.2 This specification does not apply to the sale or transfer
of used light sport aircraft, engines, or propellers. 4.2 Information Plate—A manufacturer-issued fire proof
information plate, printed in English or as defined by the
1.2 This specification applies to powered parachute aircraft
seeking civil aviation authority approval, in the form of flight governing civil aviation authority or agency in which the
aircraft was initially sold, shall be permanently affixed to the
certificates, flight permits, or other like documentation.
1.3 This standard does not purport to address all of the aircraft in a visible location and shall be designed to remain
legible for the expected life of the aircraft. The information
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro- plate shall be made of steel, and have the required information
either stamped or engraved onto the plate.
priate safety and health practices and determine the applica-
4.2.1 Serial Number—A manufacturer-issued unique iden-
bility of regulatory requirements prior to use.
tifying number or code affixed to the aircraft.
2. Terminology
4.2.2 Name and Manufacturer, including the name of the
2.1 Definitions: manufacturer’s city, state, and country.
2.1.1 powered parachute, n—aircraft comprised of a flex- 4.2.3 Model Number—A manufacturer-issued unique iden-
ible or semi-rigid wing connected to a fuselage in such a way tifying number or code assigned to each manufactured type of
that the wing is not in position for flight until the aircraft is in aircraft having the same structural design or components.
motion. This aircraft has a fuselage with seats, engine, and 4.2.4 Date of Manufacture—The date (month and year)
wheels (or floats), such that the wing and engine cannot be determined by the manufacturer that the aircraft met his
flown without the wheels (or floats) and seat(s). Unique to the required design and manufacturing specifications.
powered parachute is the large displacement between the
5. Aircraft Operating Instructions
center of lift (high) and the center of gravity (low), which is
pendulum effect. Pendulum effect limits angle of attack 5.1 Each light sport aircraft must include an Aircraft Oper-
ating Instructions which includes:
changes, provides stall resistance and maintains flight stability.
5.1.1 Operating Limitations—The instructions shall include
listings of all appropriate air-speed limitations for stall and
1
maximum speed, maximum wind limitations, weight and
This specification is under the jurisdiction of ASTM Committee F37 on Light
Sport Aircraft and is the direct responsibility of Subcommittee F37.30 on Power
balance, and power plant limitations.
Parachute.
5.1.2 Operating Data—The instructions shall include infor-
Current edition approved March 1, 2005. Published March 2005. Originally
mation concerning normal and emergency procedures and
approved in 2003. Last previous edition approved in 2003 as F2243 – 03. DOI:
10.1520/F2243-05. other pertinent information.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
1

---------------------- Page: 1 ----------------------
F2243 – 05
5.1.3 Format—The Aircraft Operating Instructions shall 5.1.5 Data Location and Contact Info
...

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SCOPE
1.1 This specification covers minimum requirements for the design, manufacture, and installation of parachutes for airframes. Airframe emergency parachutes addressed in this specification refer to parachute systems designed, manufactured, and installed to recover the airframe and its occupants at a survivable rate of descent. This specification is not applicable to deep-stall parachutes, spin recovery parachutes, drogue parachutes, or other airframe emergency aerodynamic decelerators not specifically intended for safely lowering the airframe and occupants to the ground. The specification is applicable to these types of parachutes if they are an integral part of an airframe emergency parachute system designed to recover the airframe and occupants at a survivable rate of descent.  
1.2 The values stated in SI units are to be regarded as standard. There may be values given in parentheses that are mathematical conversions to inch-pound units. Values in parentheses are provided for information only and are not considered standard.  
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1.3 Airframe emergency parachute recovery systems have become an acceptable means of greatly reducing the likelihood of serious injury or death in an in-flight emergency. Even though they have saved hundreds of lives in many different types of conditions, inherent danger of failure, even if properly designed, manufactured and installed, remains due to the countless permutations of random variables (attitude, altitude, accelerations, airspeed, weight, geographic location, etc.) that may exist at time of usage. The combination of these variables may negatively influence the life saving function of these airframe emergency parachute systems. They are designed to be a supplemental safety device and to be used at the discretion of the pilot when deemed to provide the best chance of survivability.  
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