F37.30 - Power Parachute

ABSTRACT
This specification covers design and performance requirements for powered parachute aircraft. It also applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Each of the performance requirements shall be met at the maximum takeoff weight and most critical center of gravity (CG) position. To the extent that CG adjustment devices may be adjusted for flight, these components will be evaluated in the least favorable recommended position as it affects either performance or structural strength. All performance requirements apply in and shall be corrected to International Civil Aviation Organization (ICAO) defined standard atmosphere in still air conditions at sea level. Speeds shall be given in indicated (IAS) and calibrated (CAS) airspeeds in miles per hour (MPH). The wing performance, climb performance, controllability and maneuverability, and reference parameters shall be carefully determined and evaluated. Stability requirements of the aircraft such as longitudinal stability, lateral stability, and directional stability shall be discussed as well. In terms of structural requirements, the load and proof of structure of the aircraft shall be considered.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements 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, health, and environmental practices and determine the applicability of regulatory requirements 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.

ABSTRACT
This specification covers the minimum requirements for production acceptance testing of a powered parachute aircraft. The test includes ground and flight testing. In ground testing, the aircraft shall undergo inspection verification and engine break-in. In flight testing, on the other hand, the aircraft shall be inspected for performance while on a specified flight time, including takeoff and landing, and shall undergo instrument verification. In addition, this specification also provides for post flight acceptance testing, which shall include a review of all flight critical attachments and structures.
SCOPE
1.1 The following requirements apply for the manufacture powered parachute aircraft. This specification includes the production acceptance test requirements 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, health, and environmental practices and determine the applicability of regulatory requirements 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.

ABSTRACT
This guide covers the manufacture of powered parachute aircraft and their qualification for certification. This guide applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Interface documentation is the data necessary for the aircraft manufacturer to complete overall certification to ASTM powered parachute standards. The data represents a guide to recommended type, detail, and general format for data transfer from a major subcontractor to the aircraft manufacturer.
SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.  
1.2 This guide 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, health, and environmental practices and to 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.

ABSTRACT
This specification covers the requirements that apply for the manufacture of powered parachute aircraft; it includes pilot operating handbook requirements for powered parachute aircraft. This applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other similar documentation. Each light sport aircraft must include an aircraft operating instructions which includes: operating limitations, operating data, format, supplements, and data location and contact information. Each aircraft shall have a maintenance manual provided for the aircraft that covers the minimum of the requirements as defined by the aircraft manufacturer.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured in accordance with ASTM standards.  
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first end user.  
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers.  
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, health, and environmental practices and determine the applicability of regulatory requirements 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.

ABSTRACT
This specification covers design and performance requirements for powered parachute aircraft. It also applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Each of the performance requirements shall be met at the maximum takeoff weight and most critical center of gravity (CG) position. To the extent that CG adjustment devices may be adjusted for flight, these components will be evaluated in the least favorable recommended position as it affects either performance or structural strength. All performance requirements apply in and shall be corrected to International Civil Aviation Organization (ICAO) defined standard atmosphere in still air conditions at sea level. Speeds shall be given in indicated (IAS) and calibrated (CAS) airspeeds in miles per hour (MPH). The wing performance, climb performance, controllability and maneuverability, and reference parameters shall be carefully determined and evaluated. Stability requirements of the aircraft such as longitudinal stability, lateral stability, and directional stability shall be discussed as well. In terms of structural requirements, the load and proof of structure of the aircraft shall be considered.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements 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 requirements prior to use.

ABSTRACT
This specification covers design and performance requirements for powered parachute aircraft. It also applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Each of the performance requirements shall be met at the maximum takeoff weight and most critical center of gravity (CG) position. To the extent that CG adjustment devices may be adjusted for flight, these components will be evaluated in the least favorable recommended position as it affects either performance or structural strength. All performance requirements apply in and shall be corrected to International Civil Aviation Organization (ICAO) defined standard atmosphere in still air conditions at sea level. Speeds shall be given in indicated (IAS) and calibrated (CAS) airspeeds in miles per hour (MPH). The wing performance, climb performance, controllability and maneuverability, and reference parameters shall be carefully determined and evaluated. Stability requirements of the aircraft such as longitudinal stability, lateral stability, and directional stability shall be discussed as well. In terms of structural requirements, the load and proof of structure of the aircraft shall be considered.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements 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 requirements prior to use.

ABSTRACT
This specification covers the continued airworthiness requirements that apply to the manufacture of powered parachute aircrafts and their qualification for possible civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.
SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.  
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 requirements prior to use.

ABSTRACT
This specification covers the requirements that apply for the manufacture of powered parachute aircraft; it includes pilot operating handbook requirements for powered parachute aircraft. This applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other similar documentation. Each light sport aircraft must include an aircraft operating instructions which includes: operating limitations, operating data, format, supplements, and data location and contact information. Each aircraft shall have a maintenance manual provided for the aircraft that covers the minimum of the requirements as defined by the aircraft manufacturer.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured in accordance with ASTM standards.  
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first end user.  
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers.  
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 requirements prior to use.

ABSTRACT
This specification covers the minimum requirements for production acceptance testing of a powered parachute aircraft. The test includes ground and flight testing. In ground testing, the aircraft shall undergo inspection verification and engine break-in. In flight testing, on the other hand, the aircraft shall be inspected for performance while on a specified flight time, including takeoff and landing, and shall undergo instrument verification. In addition, this specification also provides for post flight acceptance testing, which shall include a review of all flight critical attachments and structures.
SCOPE
1.1 The following requirements apply for the manufacture powered parachute aircraft. This specification includes the production acceptance test requirements 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 requirements prior to use.

ABSTRACT
This guide covers the manufacture of powered parachute aircraft and their qualification for certification. This guide applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Interface documentation is the data necessary for the aircraft manufacturer to complete overall certification to ASTM powered parachute standards. The data represents a guide to recommended type, detail, and general format for data transfer from a major subcontractor to the aircraft manufacturer.
SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.  
1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

ABSTRACT
This specification covers the requirements that apply for the manufacture of powered parachute aircraft; it includes pilot operating handbook requirements for powered parachute aircraft. This applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other similar documentation. Each light sport aircraft must include an aircraft operating instructions which includes: operating limitations, operating data, format, supplements, and data location and contact information. Each aircraft shall have a maintenance manual provided for the aircraft that covers the minimum of the requirements as defined by the aircraft manufacturer.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured in accordance with ASTM standards.
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first end user.
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers.
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 requirements prior to use.

ABSTRACT
This specification covers design and performance requirements for powered parachute aircraft. It also applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Each of the performance requirements shall be met at the maximum takeoff weight and most critical center of gravity (CG) position. To the extent that CG adjustment devices may be adjusted for flight, these components will be evaluated in the least favorable recommended position as it affects either performance or structural strength. All performance requirements apply in and shall be corrected to International Civil Aviation Organization (ICAO) defined standard atmosphere in still air conditions at sea level. Speeds shall be given in indicated (IAS) and calibrated (CAS) airspeeds in miles per hour (MPH). The wing performance, climb performance, controllability and maneuverability, and reference parameters shall be carefully determined and evaluated. Stability requirements of the aircraft such as longitudinal stability, lateral stability, and directional stability shall be discussed as well. In terms of structural requirements, the load and proof of structure of the aircraft shall be considered.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements 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 requirements prior to use.

ABSTRACT
This specification covers design and performance requirements for powered parachute aircraft. It also applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Each of the performance requirements shall be met at the maximum takeoff weight and most critical center of gravity (CG) position. To the extent that CG adjustment devices may be adjusted for flight, these components will be evaluated in the least favorable recommended position as it affects either performance or structural strength. All performance requirements apply in and shall be corrected to International Civil Aviation Organization (ICAO) defined standard atmosphere in still air conditions at sea level. Speeds shall be given in indicated (IAS) and calibrated (CAS) airspeeds in miles per hour (MPH). The wing performance, climb performance, controllability and maneuverability, and reference parameters shall be carefully determined and evaluated. Stability requirements of the aircraft such as longitudinal stability, lateral stability, and directional stability shall be discussed as well. In terms of structural requirements, the load and proof of structure of the aircraft shall be considered.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes design and performance requirements 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 requirements prior to use.

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.

ABSTRACT
This guide covers the manufacture of powered parachute aircraft and their qualification for certification. This guide applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. Interface documentation is the data necessary for the aircraft manufacturer to complete overall certification to ASTM powered parachute standards. The data represents a guide to recommended type, detail, and general format for data transfer from a major subcontractor to the aircraft manufacturer.
SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.
1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

ABSTRACT
This specification covers the minimum requirements for production acceptance testing of a powered parachute aircraft. The test includes ground and flight testing. In ground testing, the aircraft shall undergo inspection verification and engine break-in. In flight testing, on the other hand, the aircraft shall be inspected for performance while on a specified flight time, including takeoff and landing, and shall undergo instrument verification. In addition, this specification also provides for post flight acceptance testing, which shall include a review of all flight critical attachments and structures.
SCOPE
1.1 The following requirements apply for the manufacture powered parachute aircraft. This specification includes the production acceptance test requirements 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 requirements prior to use.

ABSTRACT
This specification covers the continued airworthiness requirements that apply to the manufacture of powered parachute aircrafts and their qualification for possible civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.
SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.
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 requirements prior to use.

SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.
1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.
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 requirements prior to use.

SCOPE
1.1 The following requirements apply for the manufacture of Powered Parachute Aircraft. This specification includes design and performance requirements for powered parachute aircraft.
1.2 Applicability—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 requirements prior to use.

SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.
1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

ABSTRACT
This specification covers the requirements that apply for the manufacture of powered parachute aircraft; it includes pilot operating handbook requirements for powered parachute aircraft. This applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other similar documentation. Each light sport aircraft must include an aircraft operating instructions which includes: operating limitations, operating data, format; supplements, and data location and contact information. Each aircraft shall have a maintenance manual provided for the aircraft that covers the minimum of the requirements as defined by the aircraft manufacturer.
SCOPE
1.1 The following requirements apply for the manufacture of powered parachute aircraft. This specification includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured in accordance with ASTM standards.
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first end user.
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers.
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.
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.

SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.
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 requirements prior to use.

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.
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.

SCOPE
1.1 The following requirements apply for the manufacture powered parachute aircraft. This standard includes the production acceptance test requirements for powered parachute aircraft.
1.2 Applicability—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 requirements prior to use.

SCOPE
1.1 This guide covers the manufacture of powered parachute aircraft and their qualification for certification.
1.2 This guide 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 to determine the applicability of regulatory limitations prior to use.

SCOPE
1.1 The following requirements apply for the manufacture of Powered Parachute aircraft. This standard includes pilot operating handbook requirements for powered parachute aircraft that were designed and manufactured per ASTM Standards.
1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines or propellers as a part of the initial sale or transfer to the first end user.
1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines or propellers.
1.2 Applicability—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 requirements prior to use.

SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of Powered Parachute Aircraft and their qualification for possible certification.
1.2 Applicability—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 requirements prior to use.

SCOPE
1.1 The following requirements apply for the manufacture powered parachute aircraft. This standard includes the production acceptance test requirements for powered parachute aircraft.
1.2 Applicability—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 requirements prior to use.

SCOPE
1.1 This practice covers minimum requirements for a quality assurance program for powered parachute aircraft.
1.2 Applicability—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.

SCOPE
1.1 The following requirements apply for the manufacture of Powered Parachute Aircraft. This specification includes design and performance requirements for powered parachute aircraft.
1.2 Applicability—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 requirements prior to use.

ABSTRACT
This specification covers the continued airworthiness requirements that apply to the manufacture of powered parachute aircrafts and their qualification for possible civil aviation authority approval in the form of flight certificates, flight permits, or other like documentation.
SCOPE
1.1 The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.  
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 requirements prior to use.
WITHDRAWN RATIONALE
The following continued airworthiness requirements apply for the manufacture of powered parachute aircraft and their qualification for possible certification.
Formerly under the jurisdiction of Committee F37 on Light Sport Aircraft, this specification was withdrawn in January 2023 in accordance with Section 10.6.3 of the Regulations Governing ASTM Technical Committees, which requires that standards shall be updated by the end of the eighth year since the last approval date.

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.