SAE AIR 5914 : 2014

Table of Contents

1. SCOPE
2. REFERENCES
3. GENERAL
4. SERVICE LIFE
5. GENERAL REQUIREMENTS
6. LANDING CONDITIONS
7. GROUND MANEUVERING
8. FREE EXTENSION/REBOUND (TAKEOFF TRANSITION)
9. FLIGHT LOADINGS (GUST AND MANEUVERING LOADS)
10. SUSTAINED ENGINE IMBALANCE CONDITIONS (IE.
    WIND MILLING ENGINE AND BLADE OUT VIBRATION
    CONDITIONS)
11. EXTENSION, RETRACTION, AND BRAKING WHEELS
    IN AIR
12. INTERNAL PRESSURES
13. GROUND-AIRGROUND CYCLES
14. NOTES

Abstract

Specifies guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	A-5B