ASTM F2353-04
(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
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.
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Designation: F 2353 – 04
Standard Specification for
Manufacturer Quality Assurance Program for Lighter-Than-
1
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 (e) indicates an editorial change since the last revision or reapproval.
1. Scope 4.1.3 A written procedure shall be in effect so that material
in stock can be properly identified for future use.
1.1 This specification covers minimum requirements for a
4.1.4 Documentation on any material, process, or compo-
quality assurance program for lighter-than-air light sport air-
nents certified shall be filed for reference.
craft.
1.2 This standard does not purport to address all of the
5. Inspection
safety concerns, if any, associated with its use. It is the
5.1 Awritten procedure shall be in effect so that appropriate
responsibility of the user of this standard to establish appro-
inspections are made on manufactured parts and subassem-
priate safety and health practices and determine the applica-
blies, for conformance with engineering specifications.
bility of regulatory requirements prior to use.
5.2 Awritten procedure shall be in effect so that appropriate
2. Significance and Use inspections are made on purchased components.
5.3 A written procedure shall be in effect so that completed
2.1 The purpose of this practice is to provide the minimum
units are inspected prior to delivery.
requirements necessary for the establishment of a written
5.4 Nonconforming components shall be identified and
quality assurance program for a light sport aircraft manufac-
evaluated for disposition as follows:
turer, or component supplier.
5.4.1 A component not suitable for use shall be altered or
3. Drawing Control Procedure disposed of to avoid accidental use.
5.4.2 Reworked components shall be re-inspected in accor-
3.1 Awritten procedure shall be in effect so that appropriate
dance with 5.1, 5.2, or 5.3 of this practice prior to use.
manufacturing drawings, their manufacturing revisions, and
5.4.3 In some cases, a component may be determined to be
related documents are utilized for each project.
“acceptable as is” or “as modified” after further evaluation. In
4. Material and Component Control Procedure
such cases, appropriate re
...
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1.1 This specification covers airworthiness requirements for the design of powered fixed wing light sport aircraft, an “airplane.”
1.2 This specification is applicable to the design of a light sport aircraft/airplane as defined by regulations and limited to VFR flight.
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1.1 The following requirements apply to the documentation of Light Sport Airplanes. This specification covers the Pilot’s Operating Handbook (POH), Flight Training Supplement (FTS), Maintenance Manual, Aircraft Kit Assembly Instructions (KAI), Component Original Equipment Manufacturer (OEM) manuals, Aircraft OEM’s Statement of Compliance, Registration, and Airframe Records information required for aircraft designed and manufactured in accordance with the ASTM Standards.
1.1.1 This specification covers the minimum requirements for information that shall be provided by the airplane OEM or seller of a new light sport airplane, light sport airplane kit, engines, propellers, or accessories (that is, radio, transponder, instruments, GPS, etc.) as a part of the initial sale or transfer to the first end-user.
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1.1 This specification provides the minimum requirements for a Pilot’s Operating Handbook (POH) for an aircraft designed, manufactured, and operated as a light sport aircraft.
1.2 This specification defines the POH information that shall be provided by the aircraft manufacturer of a new airplane or airplane kit as a part of the initial sale or transfer to the first-end user.
Note 1: The POH may also be referred to as an Aircraft Operating Instruction (AOI). However, POH is considered the approved nomenclature.
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SCOPE
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ABSTRACT
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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.
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.
1.4 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, health, and environmental practices and determine the applicability of regulatory requirements prior to use.
1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles fo...
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SIGNIFICANCE AND USE
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.
4.2 The purpose of this specification is to provide the minimum requirements for the establishment of a ground and flight test program for verifying the initial production aircraft meets certain operational performance requirements that have been set forth by the manufacturer in its Pilot’s Operating Handbook (POH).
4.3 In addition, this specification provides minimum requirements to verify that each subsequent production airplane has no obvious defects that would prevent the safe operation of the airplane.
4.4 All requirements given in this specification are to be performed in accordance with the manufacturer’s Specification F2972-compliant quality assurance system requirements.
4.5 The following criteria should not be construed as requirements for specific features to be included on a LSA. When a requirement specifies a feature that does not exist on a LSA, the requirement does not apply.
SCOPE
1.1 The following requirements apply for the manufacture of fixed wing aircraft, including gliders. This practice includes the production acceptance test requirements.
1.2 This practice applies to 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use.
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
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