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ASTM F2240-08(2013)

(Specification)

Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft (Withdrawn 2014)

Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft (Withdrawn 2014)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 powered parachute aircrafts 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 powered parachute aircraft.  
1.2 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.
WITHDRAWN RATIONALE
This specification covers minimum requirements for a quality assurance program for powered parachute 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Formerly under the jurisdiction of Committee F37 on Light Sport Aircraft, this specification was withdrawn in November 2014 and replaced by Specification  on Light Sport Aircraft Manufacturer’s Quality Assurance System.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Withdrawn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
F37.30 - Power Parachute
Current Stage
Ref Project

Relations

Replaced By
ASTM F2972-15 - Standard Specification for Light Sport Aircraft Manufacturer’s Quality Assurance System
Effective Date
18-Nov-2014

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ASTM F2240-08(2013) - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft (Withdrawn 2014)ASTM F2240-08(2013) - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft (Withdrawn 2014)
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Technical specification
ASTM F2240-08(2013) - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute 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:F2240 −08(Reapproved 2013)
Standard Specification for
Manufacturer Quality Assurance Program for Powered
1
Parachute Aircraft
This standard is issued under the fixed designation F2240; 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 LSA manufacturer, the supplier shall provide verification that
the material meets the LSA manufacturers’ specifications.
1.1 This specification covers minimum requirements for a
3.2.2 This procedure shall provide the purchasing agent
quality assurance program for powered parachute aircraft.
with all of the information required to order appropriate
1.2 This specification applies to powered parachute aircraft
material.
seeking civil aviation authority approval, in the form of flight
3.2.3 Awritten receiving procedure shall be in effect so that
certificates, flight permits, or other like documentation.
incoming material and components are checked against the
1.3 This standard does not purport to address all of the purchasing specifications.
safety concerns, if any, associated with its use. It is the
3.2.4 A written procedure shall be in effect so that material
responsibility of the user of this standard to establish appro- in stock can be properly identified for future use.
priate safety and health practices and determine the applica-
3.2.5 Documentation on any material, process, or compo-
bility of regulatory limitations prior to use. nents certified shall be filed for reference.
4. Inspection
2. Significance and Use
4.1 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.
4.2 Awritten procedure shall be in effect so that appropriate
2.2 Off-Site Final Assembly—Off-site final assembly or
inspections are made on purchased components.
divided production facilities, or both, are specifically allowed if
the QAprocedures provide for training, reporting, and tracking
4.3 A written procedure shall be in effect so that completed
consistent with the overall QA system.
units are inspected prior to delivery.
4.4 Nonconforming components shall be identified and
3. Materials and Manufacture
evaluated for disposition as follows:
3.1 Drawing Control Procedure—A written procedure shall
4.4.1 A component not suitable for use shall be altered or
be in effect so that appropriate manufact
...

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SCOPE
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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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SCOPE
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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This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes for light sport aircraft. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties assumed in the design data, and (3) effects of environmental conditions, such as temperature and humidity, expected in service. Parachute model designations shall include the following: (1) parachute system parts list, (2) new parachutes model designations, (3) design changes, and (4) installation design changes. The strength requirements shall be specified in terms of limit loads and ultimate loads. The following minimum performance standards for the basic parachute system design shall be met: (1) parachute strength test to determine the ultimate load factor, (2) rate of descent, (3) component strength test, (4) staged deployment, and (5) environmental conditions. The installation design requirements are specified for the following: (1) coordination, (2) weight and balance, (3) system mounting, (4) extraction performance, (5) parachute attachment to the airframe, (6) activating housing routing, and (7) occupant restraint. Other requirements such as system function and operations and product marking are also detailed.
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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