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ASTM F2240-05

(Specification)

Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft

Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft

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.

General Information

Status
Historical
Publication Date
28-Feb-2005
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

Replaces
ASTM F2240-03 - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
Effective Date
01-Mar-2005
Replaced By
ASTM F2240-08 - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
Effective Date
15-May-2008

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ASTM F2240-05 - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute AircraftASTM F2240-05 - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
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ASTM F2240-05 - Standard Specification for Manufacturer Quality Assurance Program for Powered Parachute Aircraft
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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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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: F 2240 – 05
Standard Specification for
Manufacturer Quality Assurance Program for Powered
1
Parachute Aircraft
This standard is issued under the fixed designation F 2240; 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 specification covers minimum requirements for a
material.
quality assurance program for powered parachute aircraft.
3.2.3 Awritten receiving procedure shall be in effect so that
1.2 This specification applies to powered parachute 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 subassem-
2.1 The purpose of this specification is to provide the
blies, for conformance with engineering specifications.
minimum requirements necessary for the establishment of a
4.2 Awritten procedure shall be in effect so that appropriate
written quality assurance program for a light sport aircraft
inspections are made on purchased components.
manufacturer, or component supplier.
4.3 A written procedure shall be in effect so that completed
2.2 Off-Site Final Assembly—Off-site final assembly or
units are inspected prior to delivery.
dividedproductionfacilities,orboth,arespecificallyallowedif
4.4 Nonconforming components shall be identified and
the QAprocedures provide for training, reporting, and tracking
evaluated for disposition as follows:
consistent with the overall QA system.
4.4.1 A component not suitable for use shall be altered or
3. Materials and Manufacture
disposed of to avoid accidental use.
4.4.2 Reworked compone
...

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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.  
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Standard Practice for Production Acceptance in the Manufacture of a Fixed Wing Light Sport Aircraft

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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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