Old 27th Dec 2018, 16:08
  #22 (permalink)  
Join Date: Sep 2018
Location: Laredo, TX
Posts: 123
Originally Posted by Capt Quentin McHale View Post

Many thanks, you are indeed correct.

Upon a bit of further investigation I have been led to believe that the AoA sensors are calibrated at the factory and are interchangeable between L/R and attach directly onto the fuselage with screws and can't be misaligned. The respective sensor vane has a resolver/s attached to it (internally) and sends an electrical signal to the SMYD's (SMYD1 for L(Capt) and SMYD2 for R(F/O)) which alerts the respective SMYD as to what position (L/R) the AoA sensor is in (vane has to move through 180deg when swapped from L to R or R to L positions). The respective SMYD's then recalibrate vane angle and transmit to Capt/FO screens.

There is a ground test function on the SMYD's for AoA sensor test/chk, but as you mentioned NOT mandatory upon installation which I find rather odd. This info pertains to the B738 and I would assume (very dangerous in aviation) that the MAX would be similar if not the same.

Rgds McHale.
I don't know what became of this NPRM but it would seem that a test should be mandatory: https://www.regulations.gov/document...2012-1041-0001
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