This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Landing Gear Servicing
- Aerospace Standard
- ARP5908A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber (also known as dual stage and two stage) shock struts. This document should be considered as landing gear industry recommended practice but in no way is meant to supersede the shock strut OEM’s published procedures.
Rationale
This ARP has been revised as part of the Five-Year Review policy to include more detailed considerations for the servicing of dual chamber landing gear. The revision also ensures that the document reflects the latest industry practice and is representative of a wide a range of landing gear and airframe approaches.
Recommended Content
Aerospace Standard | Landing Gear Common Repair |
Aerospace Standard | Aerospace Hydraulic Fluids Physical Properties |
Aerospace Standard | Landing Gear Component Heat Damage |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Table 1 | Lessons learned |
Issuing Committee
Reference
Number | Title |
---|
* 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.