L#  value        Brief description
-- ------------- ----------------------------------------------
1. F-16 Falcon   Planes name.
2.     3         wing type. 0=biplane, 1=hi-wing, 2=low wing, 3=jet
3.    -0.05      roll due to sideslip angle
4.    -0.100     Roll stability
5.     0.1       roll due to ailerons
6.     0.020     roll due to rudder
7.    -0.0001    Engine torque
8.     0.0004    pitch due to velocity
9.    -0.2       Pitch Stability
10.   -0.2       pitch due to elevators
11.   -0.300     pitch due to angle of attack
12.   -0.020     pitch reaction to gear up/down. 0.0=gear always down
13.    0.15      Yaw due to sideslip angle
14.   -0.2       Yaw stability 
15.    0.10      Yaw due to rudder
16.    0.005     Yaw due to nose wheel
17.   -0.10      Drag from flaps
18.   -0.0160    Drag from airframe
19.   -0.02      Drag due to angle of attack 
20.   -0.46      Side force due to sideslip
21.    0.019     Side force due to rudder
22.    0.044     adjustment for angle of attack=0 speed
23.   -4         Lift with flaps down
24.   -3         Lift with flaps up
25.    0.2       Lift due to change in pitch
26.    0.0       Nose heaviness
27.    0.7       Braking effiency
28.  500.0       Flap pressure limit
29.   30.0       Wing strength, +G's
30.    0.5       Landing gear friction
31.    60        Thrust constant
32.   -0.003     thrust loss due to velocity
33.   25.0       Dummy
34.    0.5       Pitch limit on landing
35.    0.5       Sideslip limit on landing
36.    0.5       Roll limit on landing
37.   40.0       Ground impact limit on landing
38.    0.0       Dummy
39.   -0.001     yaw due to aileron
40. 9999         Engine duration inverted
41.  -20.0       Wing Strength, -G's
42.   -8.0       Pilot Red-out, -G's
43.   14.0       Pilot Black-out, +G's
44.  2000        Max Speed warning
45.   -0.75      Roll stability on ground
46.  -30.5       Roll spring force on ground
47.   -0.95      Pitch stabilty on ground
48.   -5.8       Pitch spring force on ground
49.    0.01      0 speed ground attitude
50    -0.01      forward pitch limit when landing
51.   50.0       Dummy
52.    0.0       Dummy
53.    0.025     Dummy
54.    0.025     Dummy
55.    0.01      Limit on steering

56.    3.0       ?
57.    1.2       ?
58.    1.5       ?