Cart
0
Product
Products
(empty)
No products
To be determined
Shipping
$0.00
Total
Product successfully added to your shopping cart
Quantity
Total
There are 0 items in your cart.
There is 1 item in your cart.
Total products
Total shipping
To be determined
Total
Sale!
View larger
View larger
SAE AIR 6168A:2019-05-23
New product
SAE AIR 6168A:2019-05-23
Landing Gear Structural Health MonitoringMore info
This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber (servicing), opportunities for corrosion detection, methods for transient overload detection, techniques for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure. Landing gear tire condition and tire pressure monitoring are detailed in ARP6225, AIR4830, and ARP6137, respectively. Aircraft Brake Temperature Monitoring Systems (BTMS) are detailed in AS1145.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.045 : Structure and structure elements
|
| Number of pages | 16 |
| Replace | SAE AIR 6168:2012-04-12 |
| Year | 2019 |
| Document history | SAE AIR 6168:2012-04-12 |
| Country | USA |
| Keyword | SAE 6168;SAE AIR6168A;SAE AIR6168A;SAE AIR 6168 |