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ASTM F2353-05(2013)

(Specification)

Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)

Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)

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.
WITHDRAWN RATIONALE
This specification covers minimum requirements for a quality assurance program for lighter-than-air light sport aircraft.
Formerly under the jurisdiction of Committee F37 on Light Sport Aircraft, this specification was withdrawn in November 2014 and replaced by Specification  on Light Sport Aircraft Manufacturer’s Quality Assurance System.
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards volume information, refer to the standard's Document Summary page on the ASTM website.

General Information

Status
Withdrawn
Publication Date
31-May-2013
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(2010) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
Effective Date
01-Jun-2013
Replaced By
ASTM F2972-15 - Standard Specification for Light Sport Aircraft Manufacturer’s Quality Assurance System (Withdrawn 2024)
Effective Date
18-Nov-2014

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ASTM F2353-05(2013) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)ASTM F2353-05(2013) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)
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ASTM F2353-05(2013) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)
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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 2013)
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 4.1.2 Awritten receiving procedure shall be in effect so that
incoming material and components are checked against the
1.1 This specification covers minimum requirements for a
purchasing specifications.
quality assurance program for lighter-than-air light sport air-
craft. 4.1.3 A written procedure shall be in effect so that material
in stock can be properly identified for future use.
1.2 This standard does not purport to address all of the
4.1.4 Documentation on any material, process, or compo-
safety concerns, if any, associated with its use. It is the
nents certified shall be filed for reference.
responsibility of the user of this standard to establish appro-
priate safety and health practices and determine the applica-
bility of regulatory requirements prior to use. 5. Inspection
5.1 Awritten procedure shall be in effect so that appropriate
2. Significance and Use
inspections are made on manufactured parts and
2.1 The purpose of this specification is to provide the
subassemblies, for conformance with engineering specifica-
minimum requirements necessary for the establishment of a
tions.
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
divided production facilities, or both, are specifically allowed if
5.3 A written procedure shall be in effect so that completed
the QA procedures specify the applicable QA requirements for
units are inspected prior to delivery.
the activities being conducted at the final assembly or produc-
5.4 Nonconforming components shall be identified and
tion facility where the activity is being conducted, or both.
evaluated for disposition as follows:
These QA requirements shall be consistent with this specifica-
tion. 5.4.1 A component not suitable for use shall be altered or
disposed of to avoid accidental use.
3. Drawing Control Procedure
5.4.2 Reworked components shall be re-inspected in accor-
dance with 5.1, 5.2,or 5.3 of this practice prior to use.
3.1 Awritten procedure shall be in effect so that appropriate
manufacturing drawings, their manufacturing revisions, and
5.4.3 In some cases, a
...

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4.1 The purpose of this practice is to provide the minimum requirements necessary for the establishment of a production acceptance program for a manufacturer of light sport aircraft.  
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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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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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