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
Reduced price!
View larger
View larger
More info
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design of flanges on temperature sensors intended for use in gas turbine engines. Three figures detail the configuration of standard size flange mounts with bolt holes, slotted flanges, and miniaturized flanges for small probes.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Cancellation date | 2018-05-03 |
| Confirmation date | 2018-05-03 |
| ICS | 49.080 : Aerospace fluid systems and components
|
| Number of pages | 5 |
| Replace | SAE ARP 465A:1992-02-01 |
| Replaced by | SAE ARP 465B (2018-05-03) |
| Set | AEROPAKS10U-10 |
| Year | 2018 |
| Document history | SAE ARP 465A:1992-02-01 |
| Country | USA |
| Keyword | SAE 465;SAE ARP465B;SAE ARP465B;SAE ARP 465 |