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ASTM F2353-05(2008)

(Specification)

Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft

Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport 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 lighter-than-air light sport aircraft 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 lighter-than-air light sport aircraft.
1.2 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
14-May-2008
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F37 - Light Sport Aircraft
Drafting Committee
F37.60 - Lighter than Air
Current Stage
Ref Project

Relations

Replaces
ASTM F2353-05 - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
Effective Date
15-May-2008
Replaced By
ASTM F2353-05(2010) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
Effective Date
01-Dec-2010

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ASTM F2353-05(2008) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport AircraftASTM F2353-05(2008) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
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ASTM F2353-05(2008) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
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REDLINE ASTM F2353-05(2008) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport 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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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: F2353 – 05 (Reapproved 2008)
Standard Specification for
Manufacturer Quality Assurance Program for Lighter-Than-
Air Light Sport Aircraft
This standard is issued under the fixed designation F2353; 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 4.1.1 This procedure shall provide the purchasing agent
with all the information required to order appropriate material.
1.1 This specification covers minimum requirements for a
4.1.2 Awritten receiving procedure shall be in effect so that
quality assurance program for lighter-than-air light sport air-
incoming material and components are checked against the
craft.
purchasing specifications.
1.2 This standard does not purport to address all of the
4.1.3 A written procedure shall be in effect so that material
safety concerns, if any, associated with its use. It is the
in stock can be properly identified for future use.
responsibility of the user of this standard to establish appro-
4.1.4 Documentation on any material, process, or compo-
priate safety and health practices and determine the applica-
nents certified shall be filed for reference.
bility of regulatory requirements prior to use.
5. Inspection
2. Significance and Use
5.1 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 subassem-
minimum requirements necessary for the establishment of a
blies, for conformance with engineering specifications.
written quality assurance program for a light sport aircraft
5.2 Awritten procedure shall be in effect so that appropriate
manufacturer, or component supplier.
inspections are made on purchased components.
2.2 Off-Site Final Assembly—Off-site final assembly or
5.3 A written procedure shall be in effect so that completed
dividedproductionfacilities,orboth,arespecificallyallowedif
units are inspected prior to delivery.
the QAprocedures specify the applicable QArequirements for
5.4 Nonconforming components shall be identified and
the activities being conducted at the final assembly or produc-
evaluated for disposition as follows:
tion facility where the activity is being conducted, or both.
5.4.1 A component not suitable for use shall be altered or
These QA requirements shall be consistent with this specifica-
disposed of to avoid accidental use.
tion.
5.4.2 Reworked components shall be re-inspected in accor-
3. Drawing Control Procedure dance with 5.1, 5.2,or 5
...


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:F2353–04 Designation: F 2353 – 05 (Reapproved 2008)
Standard Specification for
Manufacturer Quality Assurance Program for Lighter-Than-
Air Light Sport Aircraft
This standard is issued under the fixed designation F 2353; 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 lighter-than-air light sport aircraft.
1.2 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.
2. Significance and Use
2.1The purpose of this practice is to provide the minimum requirements necessary for the establishment of a written quality
assurance program for a light sport aircraft manufacturer, or component supplier.
2.1 Thepurposeofthisspecificationistoprovidetheminimumrequirementsnecessaryfortheestablishmentofawrittenquality
assurance program for a light sport aircraft manufacturer, or component supplier.
2.2 Off-Site Final Assembly—Off-site final assembly or divided production facilities, or both, are specifically allowed if the QA
procedures specify the applicable QA requirements for the activities being conducted at the final assembly or production facility
where the activity is being conducted, or both. These QA requirements shall be consistent with this specification.
3. Drawing Control Procedure
3.1 Awritten procedure shall be in effect so that appropriate manufacturing drawings, their manufacturing revisions, and related
documents are utilized for each project.
4. Material and Component Control Procedure
4.1 A written procedure shall be in effect so that materials, processes, and components, including raw materials, are in
accordance with the manufacturing specifications.
4.1.1 This procedure shall provide the purchasing agent with all the information required to order appropriate material.
4.1.2 A written receiving procedure shall be in effect so that incoming material and components are checked against the
purchasing specifications.
4.1.3 A written procedure shall be in effect so that material in stock can be properly identified for future use.
4.1.4 Documentation on any material, process, or components certified shall be filed for reference.
5. Inspection
5.1 A written procedure shall be in effect so that appropriate inspections are made on manufactured parts and subassemblies,
for conformance with engineering specifications.
...

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1.1 The following requirements apply for the manufacture of fixed wing aircraft, including gliders. This practice includes the production acceptance test requirements.  
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