This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge
- Aerospace Standard
- ARP5543A
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the recommended design, construction, performance and testing requirements for aircraft wheel inflation valves incorporating an inflation pressure gauge which are mounted on the aircraft wheel. These valve/gauge assemblies should be appropriate for use on all aircraft types supported by tubeless tire/wheel assemblies.
Rationale
This document provides design recommendations for aircraft wheel inflation valves which incorporate an inflation pressure gauge. This specific kind of inflation valves with pressure gauges have not changed over the last several years and is not expected to change in the future. Therefore, stabilization has been recommended.
Recommended Content
| Aerospace Standard | Tube, Pneumatic Tire, Aircraft |
| Aerospace Standard | Wheel and Hydraulically Actuated Brake Design and Test Requirements for Military Aircraft |
| ARINC Standard | 673 Guidance for the Use of UHF Radio Frequency Identification (RFID) |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | ||
| TABLE 2 | ||
| TABLE 3 | VIBRATION RESISTANCE | |
| TABLE 4 | SINUSOIDAL VIBRATION Sinusoidal Vibration Sweep Levels (Sweep Rate: one octave per minute or less) Up-sweep and Down-sweep |
Issuing Committee
Welcome to the SAE International A-5C Aircraft Tire Committee public forum. The SAE A-5C Aircraft Tires Committee develops standards for the design, testing, qualification, and effective utilization of aircraft tires and tubes. The Committee promotes the safe integration of tires into the larger context of landing gear, wheel, and brake operations.
Reference
| Number | Title |
|---|---|
| ANSI/NCSLZ540-1 | This document is not part of the subscrption. |
| AS33514 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL |
| AS5202 | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD |
| MIL-STD-810 | This document is not part of the subscrption. |
| RTCA/DO-160 | 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.