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ASTM F2448-04(2007)

(Practice)

Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft

Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft

SIGNIFICANCE AND USE
The 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.
If final assembly is completed outside of the main production facility, the manufacturer shall specify the required procedures and what persons are authorized to perform them.
SCOPE
1.1 This practice covers minimum requirements for a quality assurance program for weight-shift-control aircraft.
1.2 This practice applies to weight-shift-control aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation.
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.

General Information

Status
Historical
Publication Date
14-Feb-2007
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F37 - Light Sport Aircraft
Drafting Committee
F37.40 - Weight Shift
Current Stage
Ref Project

Relations

Replaces
ASTM F2448-04 - Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft
Effective Date
15-Feb-2007
Replaced By
ASTM F2448-04(2009) - Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft (Withdrawn 2014)
Effective Date
01-Jul-2009

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ASTM F2448-04(2007) - Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control AircraftASTM F2448-04(2007) - Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control Aircraft
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ASTM F2448-04(2007) - Standard Practice for Manufacturer Quality Assurance System for Weight-Shift-Control 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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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:F2448–04 (Reapproved 2007)
Standard Practice for
Manufacturer Quality Assurance System for Weight-Shift-
Control Aircraft
This standard is issued under the fixed designation F 2448; 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 3.2.2 This procedure shall provide the purchasing agent
with all of the information required to order appropriate
1.1 This practice covers minimum requirements for a qual-
material.
ity assurance program for weight-shift-control aircraft.
3.2.3 Awritten receiving procedure shall be in effect so that
1.2 This practice applies to weight-shift-control aircraft
incoming material and components are checked against the
seeking civil aviation authority approval, in the form of flight
purchasing specifications.
certificates, flight permits, or other like documentation.
3.2.4 A written procedure shall be in effect so that material
1.3 This standard does not purport to address all of the
in stock can be properly identified for future use.
safety concerns, if any, associated with its use. It is the
3.2.5 Documentation on any material, process, or compo-
responsibility of the user of this standard to establish appro-
nents certified shall be filed for reference.
priate safety and health practices and determine the applica-
bility of regulatory limitations prior to use.
4. Inspection
2. Significance and Use 4.1 Awritten procedure shall be in effect so that appropriate
inspections are made on manufactured parts and subassemblies
2.1 The purpose of this practice is to provide the minimum
for conformance with engineering specifications.
requirements necessary for the establishment of a written
4.2 Awritten procedure shall be in effect so that appropriate
quality assurance program for a light sport aircraft manufac-
inspections are made on purchased components.
turer, or component supplier.
4.3 A written procedure shall be in effect so that completed
2.2 If final assembly is completed outside of the main
units are inspected prior to delivery.
production facility, the manufacturer shall specify the required
4.4 Nonconforming components shall be identified and
procedures and what persons are authorized to perform them.
evaluated for disposition as follows:
3. Materials and Manufacture 4.4.1 A component not suitable for use shall be altered or
disposed of to avoid accidental use.
3.1 Drawing Control Procedure—Aw
...

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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 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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