ASTM F2240-08
(Specification)Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
ABSTRACT
This specification sets the minimum requirements necessary for the establishment of a written quality assurance program for a manufacturer or component supplier of powered parachute aircrafts that seeks civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation.
SCOPE
1.1 This specification covers minimum requirements for a quality assurance program for powered parachute aircraft.
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 limitations prior to use.
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Designation:F2240 −08
StandardSpecification for
Manufacturer Quality Assurance Program for Powered
1
Parachute Aircraft
This standard is issued under the fixed designation F2240; 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 LSA manufacturer, the supplier shall provide verification that
the material meets the LSA manufacturers’ specifications.
1.1 This specification covers minimum requirements for a
3.2.2 This procedure shall provide the purchasing agent
quality assurance program for powered parachute aircraft.
with all of the information required to order appropriate
1.2 This specification applies to powered parachute aircraft
material.
seeking civil aviation authority approval, in the form of flight
3.2.3 Awritten receiving procedure shall be in effect so that
certificates, flight permits, or other like documentation.
incoming material and components are checked against the
1.3 This standard does not purport to address all of the purchasing specifications.
safety concerns, if any, associated with its use. It is the
3.2.4 A written procedure shall be in effect so that material
responsibility of the user of this standard to establish appro- in stock can be properly identified for future use.
priate safety and health practices and determine the applica-
3.2.5 Documentation on any material, process, or compo-
bility of regulatory limitations prior to use. nents certified shall be filed for reference.
4. Inspection
2. Significance and Use
4.1 Awritten procedure shall be in effect so that appropriate
2.1 The purpose of this specification is to provide the
inspections are made on manufactured parts and
minimum requirements necessary for the establishment of a
subassemblies, for conformance with engineering specifica-
written quality assurance program for a light sport aircraft
tions.
manufacturer, or component supplier.
4.2 Awritten procedure shall be in effect so that appropriate
2.2 Off-Site Final Assembly—Off-site final assembly or
inspections are made on purchased components.
divided production facilities, or both, are specifically allowed if
the QAprocedures provide for training, reporting, and tracking
4.3 A written procedure shall be in effect so that completed
consistent with the overall QA system.
units are inspected prior to delivery.
4.4 Nonconforming components shall be identified and
3. Materials and Manufacture
evaluated for disposition as follows:
3.1 Drawing Control Procedure—A written procedure shall
4.4.1 A component not suitable for use shall be altered or
be in effect so that appropriate manufacturi
...
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. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation:F2240–05 Designation: F 2240 – 08
Standard Specification for
Manufacturer Quality Assurance Program for Powered
1
Parachute Aircraft
This standard is issued under the fixed designation F 2240; 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
1.1 This specification covers minimum requirements for a quality assurance program for powered parachute aircraft.
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
limitations prior to use.
2. Significance and Use
2.1 Thepurposeofthisspecificationistoprovidetheminimumrequirementsnecessaryfortheestablishmentofawrittenquality
assurance program for a light sport aircraft manufacturer, or component supplier.
2.2 Off-Site FinalAssembly—Off-site final assembly or divided production facilities, or both, are specifically allowed if the QA
procedures provide for training, reporting, and tracking consistent with the overall QA system.
3. Materials and Manufacture
3.1 Drawing Control Procedure—A written procedure shall be in effect so that appropriate manufacturing drawings, their
manufacturing revisions, and related documents are utilized for each project.
3.2 Component Control Procedure :
3.2.1A written procedure shall be in effect so that materials, processes, and components, including raw materials, are in
accordance with the manufacturing specifications.
3.2.1 A written procedure shall be in effect so that materials, processes, and components, including raw materials, are in
accordance with the manufacturing specifications. In the case of outsourced components manufactured specifically for the LSA
manufacturer, the supplier shall provide verification that the material meets the LSA manufacturers’ specifications.
3.2.2 This procedure shall provide the purchasing agent with all of the information required to order appropriate material.
3.2.3 A written receiving procedure shall be in effect so that incoming material and components are checked against the
purchasing specifications.
3.2.4 A written procedure shall be in effect so that material in stock can be properly identified for future use.
3.2.5 Documentation on any material, process, or components certified shall be filed
...
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