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ASTM F2745-11

(Specification)

Standard Specification for Required Product Information to be Provided with an Airplane

Standard Specification for Required Product Information to be Provided with an Airplane

SCOPE
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.
1.1.2 This specification does not apply to the sale or transfer of used light sport airplane, engines, propellers, or accessories.
1.2 This specification applies to airplanes seeking civil aviation authority approval, in the form of airworthiness certificates 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.

General Information

Status
Historical
Publication Date
31-May-2011
ICS
49.020 - Aircraft and space vehicles in general
Technical Committee
F37 - Light Sport Aircraft
Drafting Committee
F37.20 - Airplane
Current Stage
Ref Project

Relations

Referred By
ASTM F3060-20 - Standard Terminology for Aircraft
Effective Date
01-Jun-2011

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ASTM F2745-11 - Standard Specification for Required Product Information to be Provided with an Airplane
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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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:F2745 −11
StandardSpecification for
Required Product Information to be Provided with an
1
Airplane
This standard is issued under the fixed designation F2745; 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 F2563 Practice for Kit Assembly Instructions of Aircraft
Intended Primarily for Recreation
1.1 The following requirements apply to the documentation
of Light Sport Airplanes. This specification covers the Pilot’s
3. Terminology
Operating Handbook (POH), Flight Training Supplement
3.1 Definitions:
(FTS), Maintenance Manual, Aircraft Kit Assembly Instruc-
3.1.1 records—records of maintenance, alterations, and in-
tions (KAI), Component Original Equipment Manufacturer
spections for each aircraft subsequent to issuance of the
(OEM) manuals, Aircraft OEM’s Statement of Compliance,
manufacturer’s statement of compliance.
Registration, and Airframe Records information required for
aircraft designed and manufactured in accordance with the
3.2 Acronyms:
ASTM Standards.
3.2.1 FTS—flight training supplement
1.1.1 This specification covers the minimum requirements
3.2.2 KAI—kit assembly instructions
for information that shall be provided by the airplane OEM or
3.2.3 LSA—light sport aircraft (airplane)
seller of a new light sport airplane, light sport airplane kit,
3.2.4 OEM—original equipment manufacturer
engines, propellers, or accessories (that is, radio, transponder,
instruments, GPS, etc.) as a part of the initial sale or transfer to
3.2.5 POH—pilot’s operating handbook
the first end-user.
4. Significance and Use
1.1.2 This specification does not apply to the sale or transfer
of used light sport airplane, engines, propellers, or accessories.
4.1 The purpose of this specification is to provide the
minimum information necessary for the proper identification,
1.2 This specification applies to airplanes seeking civil
operation, and maintenance of each light sport airplane.
aviation authority approval, in the form of airworthiness
certificates or other like documentation.
4.2 This specification does not define the method for docu-
mentation delivery to the first end-user. Whether to provide
1.3 This standard does not purport to address all of the
paper, PDF, electronic records, access to the information on a
safety concerns, if any, associated with its use. It is the
website, or some combination shall be determined by the
responsibility of the user of this standard to establish appro-
aircraft OEM.
priate safety and health practices and determine the applica-
bility of regulatory limitations prior to use.
5. Minimum Information Requirements
2. Referenced Documents
5.1 The following information shall be furnished by the
2 manufacturer or seller at the time of sale of each airplane or
2.1 ASTM Standards:
airplane kit to the first end-user.
F2245 Specification for Design and Performance of a Light
5.1.1 The information plate specified in Section 6.
Sport Airplane
5.1.2 The placards specified in Section 7.
F2483 Practice for Maintenance and the Development of
5.1.3 The Pilot’s Operating Handbook (POH) specified in
Maintenance Manuals for Light Sport Aircraft
Section 8.
5.1.4 The maintenance manual specified in Section 9.
5.1.5 The component OEM’s manuals specified in Section
1
This specification is under the jurisdiction of ASTM Committee F37 on Light
10.
SportAircraft and is the direct responsibility of Subcommittee F37.20 on Airplane.
5.1.6 The aircraft OEM’s statement of compliance specified
Current edition approved June 1, 2011. Published September 2011. DOI:
10.1520/F2745-11.
in Section 11.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
5.1.7 The aircraft OEM’s product/component registration
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
information specified in Section 12.
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. 5.1.8 The aircraft records specified in Section 13.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F2745−11
5.2 The following information shall be furnished, as 10. Component Original Equipment Manufacturer’s
applicable, by the manufacturer or seller at the time of sale of (OEM) Manuals
each airplane or airplane kit to the first end-user.
10.1 If the aircraft OEM has not incorporated the following
5.2.1 The aircraft Flight Training Supplement (FTS) speci-
information into their aircraft manuals, the following compo-
fied in Section 14.
nent OEM documentation shall be pr
...

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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.  
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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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