This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Landing Gear Fatigue Tests with Equivalent Damage Spectra
- Aerospace Standard
- ARP5429
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Recommended Practice (ARP) applies to fatigue testing of landing gear and landing gear components.
Rationale
ARP5429 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 | Typical Block Loading | |
TABLE 2 | Analytical Spectrum (Block Loading) | |
TABLE 3 | Typical Section Analysis | |
TABLE 4 | Section Fatigue Analysis Sample | |
TABLE 4 | Section Fatigue Analysis Sample | |
TABLE 5 | Analytical Versus Test Spectrum Military Aircraft | |
TABLE 6 | Analytical Versus Test Spectrum Damage Regional Business Jet |
Issuing Committee
Reference
Number | Title |
---|---|
FAA Advisory Circular 25.571-1C | This document is not part of the subscrption. |
FAAAdvisoryCirc | This document is not part of the subscrption. |
FAR Part 25, Paragraph 25.571 | This document is not part of the subscrption. |
FARPart25,Parag | This document is not part of the subscrption. |
* Redlines comparisons are available for those standards
listed in the Revision History that contain a radio button. A
redline comparison of the current version against a revision is
accomplished by selecting the radio button next to the standard and
then selecting 'compare'. At this time, Redline versions only exist
for some AMS standards. SAE will continue to add redline versioning
with ongoing updates to SAE MOBILUS.