S-AA5A-0 Engine Mount & Fuselage Substantation

Description

Digitl Download of the PDF file from American Aviation, AA-5A Engine Mount & Fuselage Structural Analysis Reports. 28 pages

Structures Report # S-AA5A-0

 

References

Symbols and Abbreviations

Introduction

Summary of General Data

Three-View

Section I, Aircraft Mass Distribution

Introduction

Aircraft C.G. Envelope

Aircraft Weight Summary

Panel appoint Weight Distribution

General

Arrangement, Seating, & Baggage

Section II, Aircraft Geometry

Introduction

Wing Geometry

Vertical Tail Geometry

Horizontal Tail Geometry

Fuselage Geometry

Section III, Landing Gear Geometry & Landing Loads

Introduction

Summary of Landing Gear Loads

Nose Gear Geometry

Main Gear Geometry

Landing Gear Static Reactions

Level Landing – Nose Wheel Contacting

Two Point Level Landing – Nose Wheel Clear

One Wheel Landing

Two Point – Tail Down Landing

Braked Roll – Nose Wheel Contacting

Braked Roll – Nose Wheel Clear

Side Load Condition

Nose Tire Dynamic Load

Supplementary Conditions for Nose Wheel

Section IV, Aerodynamic Characteristics

Introduction

Aerodynamic Characteristics – Flaps Retracted (0 degrees)

Aerodynamic Characteristics – Flaps Deflected (45 degrees)

Section V, Load Factors, Design Speeds, and Aircraft Tail Loads

Introduction

Summary of Design Speeds

Summary of Maximum Tail Loads & Loaf Factors

Maneuvering Load Factors

Determination of Design Speed

Aircraft Tail Loads

APPENDIX – A Input Data for Computer Program “STRU02”

APPENDIX B – Verification of Result Produced By Computer Program STRU02 “Balance Tail Loads”, Balancing Tail Loads

 

REFERENCES

 

1. “Airworthiness Standards: Normal, Utility, and Acrobatic Category Airplanes”, Federal Aviation Regulation, Volume III, Part 23 dated February 1965, Inclusive Amendment 23-8.
2. “Basic Data”, American Aviation Report S-AA5-0, 22 September 1970.
3. “Vertical Tail Analysis”, American Aviation Report, S-AA5-4
4. “Theory of Wing Sections”, Abbot, Ira H. and Von Doenhoff, Albert E., Dover Publications, 1959.
5. American Aviation Drawings:
   • 5298001, “Wing Master Dimensions”
   • 5200003, “Wing Assembly”
   • 5202035, “Aileron Assembly”
   • 5203018, “Flap Assembly”
   • 5398003, “Master Dimensions Vertical Tail”
   • 5302040, “Dorsal Fin Assembly & Installation”
   • 5302050, “Horizontal Tail Installation”
   • 5201006, “Panel Assembly – Inboard Wing”
6. “Airfoil Section Characteristics As Affected By Vibrations of The Reynolds Number”, NACA TR 586, 1937.
7. “Test In The Variable-Density Wind Tunnel Of The N.A.C.A. 23012 Airfoil With Plain And Split Flaps”, NACA TR 661, 1939.

 

SYMBOLS AND ABBREVIATIONS