Standard Test Method for Aerodynamic Acceptance of SAE Ams 1424 and SAE Ams 1428 Aircraft Deicing/Anti-Icing Fluids

Standard:
Issued:
  • 2003-02-10
 
  • HISTORICAL Access the latest revision: AS5900C
Publisher:
  • SAE International
Pages:
30
Scope:

This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV. Fluids used to deice and/or anti-ice: a. Large transport type jet aircraft while on the ground where the takeoff rotation speeds generally exceed approximately 100 to 110 knots. (The procedure for this type of aircraft is referred to as the High Speed Ramp Tests). and/or b. Commuter type aircraft while on the ground and when no compensating measures are taken in the aircraft takeoff procedure where the takeoff rotation speeds generally exceed approximately 60 knots. (The procedure for this type of aircraft is referred to as the Low Speed Ramp Tests.) The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off aircraft lifting and control surfaces during the takeoff ground acceleration and climb.

History:
Standard Published Revision Status
AS5900C 2016-10-25 Latest Revised
2007-07-26 Historical Revised
2003-05-23 Historical Revised
2003-02-10 Historical Issued
AKA:
  • SAE AS 5900
Sector:
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$78.00
Add
Mail
$78.00
Members save up to 18% off list price.
Grade
If you are currently using this technical report:
Share
HTML for Linking to Page
Page URL

Related Items

Technical Paper / Journal Article
2011-06-13
Training / Education
2017-10-31
Training / Education
2017-10-31
Technical Paper / Journal Article
2011-06-13
Technical Paper / Journal Article
2011-06-13