Revert trim "fix"

PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg

@@ -243,8 +243,7 @@ yaw_moment_roll_rate_mach_table = 0:0
 elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
 aileron_scaling_table = -0.785:1 ;0:1
 rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
-//KH From 3
-elevator_lift_coef=4
+elevator_lift_coef=3
 rudder_lift_coef=2
 aileron_load_factor_effectiveness_table = 0:1
 lift_coef_at_drag_zero = 0.1

README.MD

@@ -35,11 +35,6 @@ unchanged to allow to see the differences more easily.
 - SDK conformance
   - Affected by `fuel_flow_gain`
     - Set to zero as the SDK indicated one ought to
-- Full AND trim on climb and certain cruise conditions (aft CG, light weight)
-  - Affected by `elevator_lift_coef`
-    - Adjusted to increase AND trim effectiveness
-      - I am unsure if this is truly a fix or my tests lead me astray
-      - Adjustment is not a complete fix
 - Slat drag and approach N1
   - Affected by slat drag
     - Lowered `drag_scalar`
@@ -100,7 +95,9 @@ pitch kept rising. These flights were conducted with differing payloads, all of
 which set by the EFB, thus ensuring a valid CG.  
 Given the MD-11 far back placement of the wing and the subsequent 1° AND vs.
 15.5° ANU trim limits, most flights would never use all of the AND trim
-authority. There seems to be some issue here.
+authority. There seems to be some issue here.  
+I had tried a lot, but nothing conclusive. I see this as a limit of my
+understanding for MSFSs flight model configurations.
 
 ## Slat drag
 Users reported a strong pitch up momentum upon slat retraction, strong enough