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ASTM F2241-14

(Specification)

Standard Specification for Continued Airworthiness System for Powered Parachute Aircraft (Withdrawn 2023)

Standard Specification for Continued Airworthiness System for Powered Parachute Aircraft (Withdrawn 2023)

ABSTRACT
This specification covers the continued airworthiness requirements that apply to the manufacture of powered parachute aircrafts and their qualification for possible civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.
SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.  
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.  
1.3 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.
WITHDRAWN RATIONALE
The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.
Formerly under the jurisdiction of Committee F37 on Light Sport Aircraft, this specification was withdrawn in January 2023 in accordance with Section 10.6.3 of the Regulations Governing ASTM Technical Committees, which requires that standards shall be updated by the end of the eighth year since the last approval date.

General Information

Status
Withdrawn
Publication Date
31-Oct-2014
Withdrawal Date
08-Jan-2023
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

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ASTM F2241-14 - Standard Specification for Continued Airworthiness System for Powered Parachute Aircraft (Withdrawn 2023)ASTM F2241-14 - Standard Specification for Continued Airworthiness System for Powered Parachute Aircraft (Withdrawn 2023)
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ASTM F2241-14 - Standard Specification for Continued Airworthiness System for Powered Parachute Aircraft (Withdrawn 2023)
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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:F2241 −14
Standard Specification for
Continued Airworthiness System for Powered Parachute
1
Aircraft
This standard is issued under the fixed designation F2241; 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 3.1.1 powered parachute, n—aircraftcomprisedofaflexible
or semi-rigid wing connected to a fuselage in such a way that
1.1 The following continued airworthiness requirements
the wing is not in position for flight until the aircraft is in
apply for the manufacture of powered parachute aircraft and
motion. That aircraft has a fuselage with seats, engine, and
their qualification for possible certification.
wheels (or floats), such that the wing and engine cannot be
1.2 This specification applies to powered parachute aircraft
flown without the wheels (or floats) and seat(s). Unique to the
seeking civil aviation authority approval, in the form of flight
powered parachute is the large displacement between the
certificates, flight permits, or other like documentation.
center of lift (high) and the center of gravity (low), which is
1.3 This standard does not purport to address all of the
pendulum effect. Pendulum effect limits angle of attack
safety concerns, if any, associated with its use. It is the changes, provides stall resistance and maintains flight stability.
responsibility of the user of this standard to establish appro-
4. Current Operators List Documentation
priate safety and health practices and determine the applica-
bility of regulatory requirements prior to use.
4.1 The manufacturer shall maintain a list of registered
aircraft owners that includes all aircraft in service by serial
2. Referenced Documents
number, registration number, together with the name and
2
2.1 ASTM Standards:
address of the owner.
F2241 Specification for ContinuedAirworthiness System for
4.2 In cases where the appropriate Civil Aviation Authority
Powered Parachute Aircraft
maintains records of registered owners sufficient for tracking
F2242 Specification for ProductionAcceptance Testing Sys-
aircraft and the manufacturer has access to such records, the
tem for Powered Parachute Aircraft
manufacturer may elect to utilize such records for complying
F2243 Specification for Required Product Information to be
with this section.
Provided with Powered Parachute Aircraft
F2244 Specification for Design and Performance Require-
5. Monitoring, Investigation and Remedial Action
ments for Powered Parachute Aircraft
5.1 The manufacturer shall maintain contact with dealers
F2483 Practice for Maintenance and the Development of
and owners who report incidents or other situations that might
Maintenance Manuals for Light Sport Aircraft
relate to safety, operations, or maintenance of aircraft produced
F2563 Practice for Kit Assembly Instructions of Aircraft
and placed in service. The manufacturer will promptly inves-
Intended Primarily for Recreation
tigate all reported failures, malfunctions, or defects and de-
F2972 Specification for Light Sport Aircraft Manufacturer’s
velop the appropriate corrective action. The magnitude of the
Quality Assurance System
service problem will define the subsequent publication to the
operators.
3. Terminology
3.1 Definitions:
6. Safety Directives
6.1 A safety directive will be distributed to all operators
1
This specification is under the jurisdiction of ASTM Committee F37 on Light
when a condition is found to exist that may also exist in other
Sport Aircraft and is the direct responsibility of Subcommittee F37.30 on Power
aircraft in the fleet and which would cause a deviation from
Parachute.
original design or unsafe condition for flight, rendering the
Current edition approved Nov. 1, 2014. Published December 2014. Originally
aircraft unairworthy. This change, maintenance procedure,
approved in 2003. Last previous edition approved in 2013 as F2241 – 13. DOI:
10.1520/F2241-14.
inspection procedure, or other procedures deemed appropriate
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
by the manufacturer is mandatory and must be performed and
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
documented in the individual aircraft logs in order for that
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. aircraft to maintain compliance withASTM standards. When a
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F2241−14
safety directive is issued, immediately provide a copy to the complian
...

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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.  
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