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ASTM F2626-12

(Terminology)

Standard Terminology for Light Sport Aircraft (Withdrawn 2018)

Standard Terminology for Light Sport Aircraft (Withdrawn 2018)

SCOPE
1.1 This terminology standard covers definitions of terms and concepts related to light sport aircraft. It is intended to ensure the consistent use of terminology throughout all F37 documents.
WITHDRAWN RATIONALE
This terminology standard covers definitions of terms and concepts related to light sport aircraft. It is intended to ensure the consistent use of terminology throughout all F37 documents.
Formerly under the jurisdiction of Committee F37 on Light Sport Aircraft, this terminology was withdrawn in November 2018 and replaced by Terminology F3060 for Aircraft.1

General Information

Status
Withdrawn
Publication Date
31-Oct-2012
ICS
01.040.49 - Aircraft and space vehicle engineering (Vocabularies)
49.020 - Aircraft and space vehicles in general
Technical Committee
F37 - Light Sport Aircraft
Drafting Committee
F37.91 - Terminology
Current Stage
Ref Project

Relations

Replaced By
ASTM F3060-20 - Standard Terminology for Aircraft
Effective Date
07-Nov-2018

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ASTM F2626-12 - Standard Terminology for Light Sport Aircraft (Withdrawn 2018)ASTM F2626-12 - Standard Terminology for Light Sport Aircraft (Withdrawn 2018)
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ASTM F2626-12 - Standard Terminology for Light Sport Aircraft (Withdrawn 2018)
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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NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.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: F2626 − 12
Standard Terminology for
1
Light Sport Aircraft
This standard is issued under the fixed designation F2626; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope Light Sport Gyroplane Aircraft
F2425SpecificationforContinuedAirworthinessSystemfor
1.1 This terminology standard covers definitions of terms
Weight-Shift-Control Aircraft
and concepts related to light sport aircraft. It is intended to
F2426GuideonWingInterfaceDocumentationforPowered
ensure the consistent use of terminology throughout all F37
Parachute Aircraft
documents.
F2427Specification for Required Product Information to be
Provided with Lighter-Than-Air Light Sport Aircraft
2. Referenced Documents
F2449Specification for Manufacturer Quality Assurance
2
2.1 ASTM Standards:
Program for Light Sport Gyroplane Aircraft
F2241SpecificationforContinuedAirworthinessSystemfor
F2457Specification for Required Product Information to be
Powered Parachute Aircraft
Provided withWeight-Shift-Control Aircraft
F2242Specification for ProductionAcceptanceTesting Sys-
F2483Practice for Maintenance and the Development of
tem for Powered Parachute Aircraft
Maintenance Manuals for Light Sport Aircraft
F2243Specification for Required Product Information to be
F2506SpecificationforDesignandTestingofFixed-Pitchor
Provided with Powered Parachute Aircraft
Ground Adjustable Light Sport Aircraft Propellers
F2244Specification for Design and Performance Require-
F2507Specification for Recreational Airpark Design
ments for Powered Parachute Aircraft
F2563Practice for Kit Assembly Instructions of Aircraft
F2245Specification for Design and Performance of a Light
Intended Primarily for Recreation
Sport Airplane
F2564Specification for Design and Performance of a Light
F2279Practice for QualityAssurance in the Manufacture of
Sport Glider
Fixed Wing Light Sport Aircraft
F2295Practice for Continued Operational Safety Monitor-
3. Terminology
ing of a Light Sport Aircraft
aircraft make—name assigned to the aircraft by the aircraft
F2316Specification for Airframe Emergency Parachutes
manufacturer when each aircraft was produced.
F2317/F2317MSpecification for Design of Weight-Shift-
Control Aircraft
aircraft model—aircraft manufacturer’s designation for an
F2352Specification for Design and Performance of Light
aircraft grouping with similar design or style of structure.
Sport Gyroplane Aircraft
airport elevation—highest point on an airport’s usable
F2354SpecificationforContinuedAirworthinessSystemfor
runway. F2507
Lighter-Than-Air Light Sport Aircraft
F2355Specification for Design and Performance Require-
airship—engine-driven lighter-than-air aircraft that can be
ments for Lighter-Than-Air Light Sport Aircraft
steered. F2354, F2356, F2427
F2356Specification for ProductionAcceptanceTesting Sys-
airship—engine-driven lighter-than-air aircraft that can be
tem for Lighter-Than-Air Light Sport Aircraft
steered, and that sustains flight through the use of either gas
F2415Practice for Continued Airworthiness System for
buoyancy or an airborne heater, or both. F2355
annual condition inspection—detailed inspection accom-
1
This terminology is under the jurisdiction of ASTM Committee F37 on Light
plishedonceayearonaLSAinaccordancewithinstructions
Sport Aircraft and is the direct responsibility of Subcommittee F37.91 on Termi-
nology. provided in the maintenance manual supplied with the
Current edition approved Nov. 1, 2012. Published December 2012. Originally
aircraft. The purpose of the inspection is to look for any
approved in 2007. Last previous edition approved in 2007 as F2626 – 07. DOI:
wear, corrosion, or damage that would cause an aircraft to
10.1520/F2626-12.
2 not be in a condition for safe operation. F2483
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
AOI—aircraft operating instructions F2279, F2317/F2317M,
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website. F2352, F2425, F2427, F2449, F2457, F2564
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F2626 − 12
A&P—airframe and powerplant mechanic as defined by 14 design maximum aircraft weight, n— aircraft design maxi-
CFR Part 65 in the U.S. or equivalent certification in other mum weight W shall be the sum of W + W .
MAX WING SUSP
countries. F2483 F2317/F2317M
2
AR—aspect ratio = b /S F2245, F2564 design maximum trike carriage weight,n—designmaximum
trike car
...

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