SAE AS 5562:2015-08-07

This SAE Aerospace Standard (AS) establishes minimum ice and rain performance criteria for electrically-heated pitot and pitot-static probes intended for use on the following classes of fixed-wing aircraft and rotorcraft. The classes of fixed-wing aircraft are defined by aircraft flight envelopes and are shown in Figure 1. The flight envelopes generally fall into the classes as shown below:

Author	SAE
Editor	SAE
Document type	Standard
Format	File
ICS	49.090 : On-board equipment and instruments
Number of pages	17
Set	AEROPAKS10U-10
Year	2015
Document history
Country	USA
Keyword	SAE 5562;SAE AS5562;SAE AS5562;SAE AS 5562