ASTM F2240-03
(Specification)Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
SCOPE
1.1 This practice covers minimum requirements for a quality assurance program for powered parachute aircraft.
1.2 Applicability—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: F 2240 – 03
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 (e) indicates an editorial change since the last revision or reapproval.
1. Scope 3.2.3 Awritten receiving procedure shall be in effect so that
incoming material and components are checked against the
1.1 This practice covers minimum requirements for a qual-
purchasing specifications.
ity assurance program for powered parachute aircraft.
3.2.4 A written procedure shall be in effect so that material
1.2 Applicability—This specification applies to powered
in stock can be properly identified for future use.
parachute aircraft seeking civil aviation authority approval, in
3.2.5 Documentation on any material, process, or compo-
the form of flight certificates, flight permits, or other like
nents certified shall be filed for reference.
documentation.
1.3 This standard does not purport to address all of the
4. Inspection
safety concerns, if any, associated with its use. It is the
4.1 Awritten procedure shall be in effect so that appropriate
responsibility of the user of this standard to establish appro-
inspections are made on manufactured parts and subassem-
priate safety and health practices and determine the applica-
blies, for conformance with engineering specifications.
bility of regulatory limitations prior to use.
4.2 Awritten procedure shall be in effect so that appropriate
2. Significance and Use inspections are made on purchased components.
4.3 A written procedure shall be in effect so that completed
2.1 The purpose of this specification is to provide the
units are inspected prior to delivery.
minimum requirements necessary for the establishment of a
4.4 Nonconforming components shall be identified and
written quality assurance program for a light sport aircraft
evaluated for disposition as follows:
manufacturer, or component supplier.
4.4.1 A component not suitable for use shall be altered or
3. Materials and Manufacture
disposed of to avoid accidental use.
4.4.2 Reworked components shall be re-inspected in accor-
3.1 Drawing Control Procedure
dance with 4.1, 4.2, or 4.3 of this practice prior to use.
3.1.1 A written procedure shall be in effect so that appro-
4.
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