ASTM-F2245 2012

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F2245-12c Standard Specification for Design and Performance of a Light Sport Airplane

Published By	Publication Date	Number of Pages
ASTM	2012	30

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Category: ASTM

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Description

1.1 This specification covers airworthiness requirements for the design of powered fixed wing light sport aircraft, an airplane.

1.2 This specification is applicable to the design of a light sport aircraft/airplane as defined by regulations and limited to VFR flight.

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.

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PDF Pages	PDF Title
1	Scope Referenced Documents Terminology
2	Flight
3	TABLE 1
4	Structure
5	FIG. 1
8	TABLE 2
9	FIG. 2
10	FIG. 3 FIG. 4 FIG. 5
11	Design and Construction FIG. 6
12	Powerplant
13	Required Equipment Operating Limitations and Information Pilot’s Operating Handbook Keywords
14	A1. ADDITIONAL REQUIREMENTS FOR LIGHT SPORT AIRPLANES USED TO TOW GLIDERS A1.1 Applicability A1.2 Minimum Climb Performance While Towing A1.3 Controllability and Maneuverability A1.4 Stability A1.5 Structure and Strength Requirements A1.6 Design and Construction
15	A1.7 Operating Limitations A2. LIGHT SPORT AIRCRAFT TO BE FLOWN AT NIGHT A2.1 Applicability A2.2 Flight A2.3 Structure A2.4 Design and Construction A2.5 Powerplant A2.6 Required Equipment A2.7 Lighting Requirements
16	FIG. A2.1
18	A2.8 Avionics A2.9 Electrical Requirements A2.10 Operating Instructions (AOI) A2.11 Learning Documents
19	X1. SIMPLIFIED DESIGN LOAD CRITERIA FOR LIGHT SPORT AIRPLANES X1.1 Abbreviations X1.2 Flight Loads X1.3 Flight Conditions TABLE X1.1
20	FIG. X1.1 FIG. X1.2
21	X1.4 Control Surface Loads FIG. X1.3
22	X1.5 Control System Loads TABLE X1.2
23	X2. ACCEPTABLE METHODS OF WING AND FUSELAGE LOAD CALCULATIONS X2.1 Symmetrical Wing Loads FIG. X1.4 FIG. X1.5
24	X2.2 X2.3 Unsymmetrical Wing Loads X2.4 Rear Fuselage Loads X2.5 Forward Fuselage Loads FIG. X2.1
25	X3. ACCEPTABLE MEANS OF GUST LOAD FACTOR CALCULATIONS X3.1 X3.2 X4. ACCEPTABLE MEANS FOR CALCULATING GUST LOADS ON STABILIZING SURFACES X4.1 X4.2 FIG. X2.2
26	X5. ACCEPTABLE MEANS FOR CALCULATION OF WATER LOADS X5.1 Water Load Conditions X5.2 Design Weights and Center of Gravity Positions X5.3 Application of Loads X5.4 Hull and Main Float Load Factors X5.5 Hull and Main Float Landing Conditions
27	X5.6 Hull and Main Float Takeoff Condition X5.7 Hull and Main Float Bottom Pressures X5.8 Auxiliary Float Loads
28	FIG. X5.1 FIG. X5.2
29	FIG. X5.3
30	X5.9 Seawing Loads X6. IMPERIAL AND METRIC UNITS X6.1

Additional information

Standard Title	F2245-12c Standard Specification for Design and Performance of a Light Sport Airplane
Published Code	ASTM
Publication Date	2012
Pages Count	30

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ASTM-F2245 2012

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