3 ms·
The 37 max was designed to change stabilizer pitch in a key moment of unstable flight and that trim is not able to be overridden by elevator input. You have to
by weaksauce 8y ago
The 37 max was designed to change stabilizer pitch in a key moment of unstable flight and that trim is not able to be overridden by elevator input. You have to disengage a thing a t a critical altitude when flaps 0 happens at only 1000’ or so agl on a system you didn’t know exsisted and only activates under a few uncommon parameters to counteract the large rotation moment that the forward engines give. You really don’t quite know what you are talking about. 1000’ per min vertical speed is not uncommon for a controlled descent.
- heavenlyblue 8y agoWhile you seem to know what you're talking about, you're not very good at expressing it at all (lack of proper grammar doesn't help).
- weaksauce 8y agoit was on mobile, sorry. perhaps this is more clear: The 37-max was designed to change the stabilizer to be more nose down in attitude in a key moment of unstable flight and that nose down stabilizer trim is not able to be overridden by elevator input on the yoke because of the design. To fix it, you have to disengage the runaway trimming of the stabilizer at a critical altitude when you disengage flaps at about 1000’ or so agl(above ground level) on a system you didn’t know existed. To further complicate this, it only activates under a few uncommon parameters(max thrust, high angle of attack, steep bank angle, flaps retracted, autopilot disengaged) to counteract the large rotation force that the forward engines give. 1000’ per min vertical speed is not uncommon for a controlled descent so you don't have much time to fix it. You really don’t quite know what you are talking about.