Here a different device: the designed and sold by Rip Quinby at
I have neither seen nor test-flown it but the info on this webpage is a copy/paste from BeechTalk that explains it well:
Robert Briggs, the owner of a F33 Bonanza, summarized the calibration section of Rip's installation instructions to a single sheet that he carries in the airplane during calibration
1) CYA-100 AoA calibration should be performed at or above 3000 feet AGL in smooth air.
2) After clearing turns, establish a straight ahead climb at Vy with gear and flaps up.
3) Turn on the CYA-100 AoA and within 5 seconds, TAP THE PROGRAMMING BUTTON. The top GREEN LED AND bottom RED LED will illuminate, showing that the unit is waiting for upper and lower display limits.
4) When satisfied that you are at Vy (im my case: 96 knots), TAP THE PROGRAMMING BUTTON AGAIN. The upper GREEN LED will flash signifying that the upper airspeed limit (low angle of attack) has been programmed into the microprocessor.
5) Reduce airspeed and place the aircraft in landing configuration (gear down and half flaps).
6) When flying straight ahead at constant altitude, reduce airspeed to just above a stall. If the stall horn sounds, increase airspeed to just turn off the stall horn and TAP THE PROGRAMMING BUTTON AGAIN.
7) The lower RED LED will flash for several seconds signifying that the lower airspeed limit (high angle of attack) has been programmed into the microprocessor.
8) The display will now go through the POST (Power On Self Test), and will then illuminate the LED appropriate to the current angle of attack.
9) Display interpretation: At speeds above Vy, the top green LED will be illuminated to let the pilot know that the CT AoA is on and working.
10) POST (Power On Self Test): the display will illuminate all LEDs from minimum to maximum brightness, and then back to minimum. Then one LED will be lit indicating the current AoA. |