It is getting a little confusing knowing which thread to use to continue this discussion now that there are three..... however....
Point 2 in the addendum is not entirely clear to me. Are they sayiing to jack up the airplane while doing the entire procedure, or just when ready to final torque the bolts? It seems to me that having the gear hanging with the outer bolts and U-1202 removed would put a lot of stress on the inner hardware.
Anybody else wonder about this?
Point 2 in the addendum is not entirely clear to me. Are they sayiing to jack up the airplane while doing the entire procedure, or just when ready to final torque the bolts? It seems to me that having the gear hanging with the outer bolts and U-1202 removed would put a lot of stress on the inner hardware.
Anybody else wonder about this?