ASTM F2242-05(2018)
(Specification)Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft
Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft
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.
General Information
- Status
- Published
- Publication Date
- 31-Oct-2018
- Technical Committee
- F37 - Light Sport Aircraft
- Drafting Committee
- F37.30 - Power Parachute
Relations
- Effective Date
- 01-Nov-2018
- Effective Date
- 01-Nov-2018
- Effective Date
- 01-Nov-2018
- Effective Date
- 01-Nov-2018
- Effective Date
- 01-Nov-2018
Overview
ASTM F2242-05(2018) - Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft defines the minimum requirements for production acceptance testing of powered parachute aircraft. Developed by ASTM International, this standard ensures that every manufactured powered parachute undergoes rigorous ground and flight testing before receiving civil aviation authority approval. The specification covers procedures for inspection verification, engine break-in, flight performance assessment, instrument verification, and post-flight review, emphasizing both quality assurance and safety in light sport aviation.
Key Topics
Scope of Application
The standard applies to powered parachute aircraft seeking flight certificates, flight permits, or similar documentation from civil aviation authorities.Ground Testing Requirements
- Inspection verification: All aircraft must pass top-level inspection procedures, ensuring no outstanding discrepancies remain.
- Engine break-in: Written procedures must be followed to verify engine performance, including the operation of all engine gauges.
Flight Testing Requirements
- Minimum 15 minutes of flight time per aircraft, including takeoff, landing, and maneuvers such as left and right turns.
- Verification of control response and performance characteristics.
- Instrument verification: All onboard instruments must operate within specified ranges; compass calibration is to be performed if applicable.
Post-Flight Acceptance Procedures
- All critical attachments and structures are reviewed for integrity.
- Documentation and sign-off by responsible personnel ensure traceability and accountability.
Documentation and Test Failure Handling
- Written procedures for documenting test results linked to each aircraft.
- Protocols for reviewing and correcting failures before retesting.
Applications
ASTM F2242-05(2018) is widely used by manufacturers of powered parachute aircraft to demonstrate compliance with regulatory requirements and obtain airworthiness certificates. Key practical applications include:
- Manufacturer Quality Assurance:
Ensuring that each production aircraft meets operational and safety benchmarks before delivery. - Regulatory Compliance:
Supporting manufacturers in achieving acceptance by aviation authorities for flight certificates or permits. - Inspection and Maintenance Protocols:
Establishing procedures for ongoing inspection, engine maintenance, and structural integrity verification, which are essential for safety and long-term operation. - Fleet Safety in Light Sport Aviation:
Supporting operators and owners with standardized methods to verify aircraft readiness and performance.
Related Standards
ASTM F2242-05(2018) aligns with international principles on standardization as set forth by the World Trade Organization Technical Barriers to Trade (TBT) Committee. Related standards and references include:
- ASTM Committee F37 on Light Sport Aircraft – Oversees standards development for light sport aviation, including powered parachutes.
- ASTM F2972 – Standard Specification for Light Sport Aircraft Design and Performance
- FAA Special Airworthiness Certificate Requirements
- International Civil Aviation Organization (ICAO) guidelines
- Other ASTM standards pertaining to flight testing, inspection procedures, and documentation requirements for light sport and ultralight aircraft.
Keywords: powered parachute aircraft, production acceptance testing, light sport aircraft, ASTM F2242-05, flight test protocol, civil aviation approval, engine break-in, inspection verification, flight certificate, airworthiness.
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Frequently Asked Questions
ASTM F2242-05(2018) is a technical specification published by ASTM International. Its full title is "Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft". This standard covers: 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 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.
ASTM F2242-05(2018) is classified under the following ICS (International Classification for Standards) categories: 49.020 - Aircraft and space vehicles in general. The ICS classification helps identify the subject area and facilitates finding related standards.
ASTM F2242-05(2018) has the following relationships with other standards: It is inter standard links to ASTM F2242-05(2013), ASTM F2426-13(2018)e1, ASTM F3060-20, ASTM F2244-14(2022), ASTM F2563-16. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
ASTM F2242-05(2018) is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
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.
Designation:F2242 −05 (Reapproved 2018)
Standard Specification for
Production Acceptance Testing System for Powered
Parachute Aircraft
This standard is issued under the fixed designation F2242; 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 flight test program for verifying the initial (first run) production
aircraft meets certain operational performance requirements
1.1 The following requirements apply for the manufacture
that have been set forth by the manufacturer in its Aircraft
powered parachute aircraft. This specification includes the
Operating Instructions.
production acceptance test requirements for powered parachute
aircraft. 3.2 In addition, this specification provides minimum re-
quirements to verify that each subsequent production airplane
1.2 This specification applies to powered parachute aircraft
has no obvious defects that would prevent the safe operation of
seeking civil aviation authority approval, in the form of flight
the airplane.
certificates, flight permits, or other like documentation.
1.3 This standard does not purport to address all of the
4. Production Acceptance Testing, Ground Testing
safety concerns, if any, associated with its use. It is the
4.1 Inspection Verification—There shall be a written proce-
responsibility of the user of this standard to establish appro-
dure in effect to verify all top-level inspections have been
priate safety, health, and environmental practices and deter-
completed and no discrepancies remain open.
mine the applicability of regulatory requirements prior to use.
1.4 This international standard was developed in accor-
4.2 Engine Break-In—There shall be a written procedure in
dance with internationally recognized principles on standard-
effect to perform the engine break-in. This procedure may
ization established in the Decision on Principles for the
include all engine gage verification of operation. All engine
Development of International Standards, Guides and Recom-
readings shall achieve the normal accepted range of readings
mendations issued by the World Trade Organization Technical
commensurate with a new engine. If not performed during
Barriers to Trade (TBT) Committee.
engine break-in, then this verification must be performed under
separate procedures. All engine gages shall be verified to be
2. Terminology
operating.
2.1 Definitions:
2.1.1 powered parachute, n—aircraftcomprisedofaflexible
5. Production Acceptance Testing, Flight Testing
or semi-rigid wing connected to a fuselage in such a way that
5.1 Every production aircraft shall be flight tested to the
the wing is not in position for flight until the aircraft is in
following minimums:
motion. This aircraft has a fuselage with seats, engine, and
5.1.1 Powered Parachutes—Fifteen minutes flight time,
wheels (or floats), such that the wing and engine cannot be
including at least one takeoff and landing, trimming of flight
flown without the wheels (or floats) and seat(s). Unique to the
controls, and verification of control for left turn, right turn, and
powered
...
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