SAE AIR 5914 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT
Hardcopy , PDF
02-03-2020
English
01-01-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
Specifies guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear.
| Committee |
A-5B
|
| DocumentType |
Standard
|
| Pages |
18
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AIR 5552 : 2015 | DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS |
| DEFSTAN 00-970(PT1)SEC4/2(1999) : 1999 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - DESIGN AND CONSTRUCTION |
| MIL-L-8552 Revision C:1965 | LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| MIL-A-8866 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
| SAE AIR 1489 : 2012 | AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY |
| SAE AS 8860 : 2012 | LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS |
| SAE ARP 1383 : 2013 | AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS |
| SAE ARP 5429 : 2017 | LANDING GEAR FATIGUE TESTS WITH EQUIVALENT DAMAGE SPECTRA |
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