Solves #48 issue.

data/aircrafts/v22.3d

@@ -3718,7 +3718,7 @@ end_quads
 end_model rotor
 # Left Rotor
 #         blades  x    y   z    h   p   b    r    prop_wash? flw_con? blur? pitchable? no_pitch_landed? no_spin? blades_offset
-rotor_new 3       -7.0 0.3 0.6  0.0 0.0 0.0  5.7  1          0        1     1          1                0        2.3
+rotor_new 3       -7.0 0.3 0.6  0.0 0.0 180.0  5.7  1          0        1     1          1                0        -2.3
 #                r   g   b   a
 rotor_blur_color 0.1 0.1 0.1 0.75
 begin_model rotor
@@ -3727,54 +3727,54 @@ translate -7.000000 0.300000 0.600000
 color 0.050000 0.050000 0.050000 1.000000 1.000000 1.000000 1.000000 0.200000 0.000000
 # Blades
 begin_quads
- normal 0.150368 0.097590 0.983802
- -0.175877 5.700000 2.436808
- normal 0.517187 0.097590 0.850291
- 0.575877 5.700000 2.163192
- normal 0.517187 -0.097590 0.850291
- 0.763816 0.600000 2.094788
- normal 0.150368 -0.097590 0.983802
- -0.363816 0.600000 2.505212
- normal -0.523118 -0.100000 -0.852495
- -0.363816 0.600000 2.505212
- normal -0.147241 -0.100000 -0.989303
- 0.763816 0.600000 2.094788
- normal -0.147241 0.100000 -0.989303
- 0.575877 5.700000 2.163192
- normal -0.523118 0.100000 -0.852495
- -0.175877 5.700000 2.436808
- normal 0.009331 -0.179018 0.983802
- 5.024283 -2.697686 2.436808
- normal -0.174078 -0.496692 0.850291
- 4.648406 -3.348724 2.163192
- normal -0.343109 -0.399102 0.850291
- 0.137707 -0.961484 2.094788
- normal -0.159700 -0.081428 0.983802
- 0.701523 0.015074 2.505212
- normal 0.174957 0.503034 -0.852495
- 0.701523 0.015074 2.505212
- normal -0.012982 0.177515 -0.989303
- 0.137707 -0.961484 2.094788
- normal 0.160223 0.077515 -0.989303
- 4.648406 -3.348724 2.163192
- normal 0.348162 0.403034 -0.852495
- 5.024283 -2.697686 2.436808
- normal -0.159700 0.081428 0.983802
- -4.848406 -3.002314 2.436808
- normal -0.343109 0.399102 0.850291
- -5.224283 -2.351276 2.163192
- normal -0.174078 0.496692 0.850291
- -0.901523 0.361484 2.094788
- normal 0.009331 0.179018 0.983802
- -0.337707 -0.615074 2.505212
- normal 0.348162 -0.403034 -0.852495
- -0.337707 -0.615074 2.505212
- normal 0.160223 -0.077515 -0.989303
- -0.901523 0.361484 2.094788
- normal -0.012982 -0.177515 -0.989303
- -5.224283 -2.351276 2.163192
- normal 0.174957 -0.503034 -0.852495
- -4.848406 -3.002314 2.436808
+ normal -0.842100 0.538500 -0.028400
+ -0.175877 5.700000 -2.436810
+ normal 0.716200 0.354800 0.601000
+ 0.575877 5.700000 -2.163190
+ normal 0.675700 0.343200 -0.652400
+ 0.763816 0.600000 -2.094790
+ normal 0.319600 0.947100 -0.028000
+ -0.363816 0.600000 -2.505210
+ normal 0.319600 0.947200 -0.028000
+ -0.363816 0.600000 -2.505210
+ normal 0.374100 0.926800 -0.032700
+ 0.763816 0.600000 -2.094790
+ normal 0.775700 0.353100 0.523100
+ 0.575877 5.700000 -2.163190
+ normal 0.953600 0.289300 -0.083400
+ -0.175877 5.700000 -2.436810
+ normal -0.683200 -0.131700 -0.718300
+ 5.024283 -2.697686 -2.436810
+ normal -0.520400 0.753000 0.402700
+ 4.648406 -3.348724 -2.163190
+ normal -0.010100 0.907400 0.420200
+ 0.137707 -0.961484 -2.094790
+ normal 0.025900 0.968700 -0.247000
+ 0.701523 0.015074 -2.505210
+ normal -0.097600 0.820500 -0.563200
+ 0.701523 0.015074 -2.505210
+ normal -0.486900 0.788000 -0.376900
+ 0.137707 -0.961484 -2.094790
+ normal -0.746900 0.648200 0.148500
+ 4.648406 -3.348724 -2.163190
+ normal -0.346100 0.839000 0.420000
+ 5.024283 -2.697686 -2.436810
+ normal -0.363300 0.043100 0.930700
+ -4.848406 -3.002314 -2.436810
+ normal -0.234900 -0.028700 0.971600
+ -5.224283 -2.351276 -2.163190
+ normal 0.412700 0.143500 0.899500
+ -0.901523 0.361484 -2.094790
+ normal -0.169500 0.846300 0.505000
+ -0.337707 -0.615074 -2.505210
+ normal -0.048200 0.626300 0.778100
+ -0.337707 -0.615074 -2.505210
+ normal 0.339000 0.642300 0.687400
+ -0.901523 0.361484 -2.094790
+ normal -0.656500 0.543200 0.523400
+ -5.224283 -2.351276 -2.163190
+ normal -0.403100 0.087600 0.910900
+ -4.848406 -3.002314 -2.436810
 end_quads
 end_model rotor
 # Right Nacelle (as a rotor)