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ASTM F2353-05(2010)

(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
30-Nov-2010
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(2008) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
Effective Date
01-Dec-2010
Replaced By
ASTM F2353-05(2013) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft (Withdrawn 2014)
Effective Date
01-Jun-2013

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ASTM F2353-05(2010) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport AircraftASTM F2353-05(2010) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
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ASTM F2353-05(2010) - Standard Specification for Manufacturer Quality Assurance Program for Lighter-Than-Air Light Sport Aircraft
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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:F2353 −05(Reapproved 2010)
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
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.
5.2 Awritten procedure shall be in effect so that appropriate
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-
5.4.1 A component not suitable for use shall be altered or
tion.
disposed of to avoid accidental use.
5.4.2 Reworked components shall be re-inspected in accor-
3. Drawing Control Procedure
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
5.4
...

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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.  
1.2 The values stated in SI units are to be regarded as standard. There may be values given in parentheses that are mathematical conversions to inch-pound units. Values in parentheses are provided for information only and are not considered standard.  
1.2.1 Note that within the aviation community mixed units are appropriate in accordance with International Civil Aviation Organization (ICAO) agreements. While the values stated in SI units are regarded as standard, certain values such as airspeeds in knots and altitude in feet are also accepted as standard.  
1.3 Airframe emergency parachute recovery systems have become an acceptable means of greatly reducing the likelihood of serious injury or death in an in-flight emergency. Even though they have saved hundreds of lives in many different types of conditions, inherent danger of failure, even if properly designed, manufactured and installed, remains due to the countless permutations of random variables (attitude, altitude, accelerations, airspeed, weight, geographic location, etc.) that may exist at time of usage. The combination of these variables may negatively influence the life saving function of these airframe emergency parachute systems. They are designed to be a supplemental safety device and to be used at the discretion of the pilot when deemed to provide the best chance of survivability.  
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