Mi-28N
9M127 launcher jettisoning enabled
APU-8/4-U 8 Ataka modification – Tier I → II
FAB-250 modification – Tier II → I
9M123 modification – Tier II → III
FAB-500 modification – Tier III → II
Replacing helicopter blades modification – Tier III → II
9M127 modification – Tier III → IV
9M39V modification – Tier III → IV
B-13L modification – Tier IV → I
EFS modification – Tier IV → III
automatic EFS modification – Tier IV → III
Mi-35M
Gunpod modification – Tier II → III
New 23 mm cannons modification – Tier III → II
NVD modification – Tier III → IV
Replacing helicopter blades modification – Tier III → II
automatic EFS modification – Tier IV → III
Apache AH. Mk. 1
MAW modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
Rooivalk Mk. 1
engine IR brightness multiplier – 1 → 0.7
added a cockpit
Replacing helicopter blades modification – Tier III → II
added 20 mm belts as Tier I modification
added MAW as Tier I modification
added ZT-6 Mokopa as Tier II modification
added New 20 mm cannons as Tier III modification
added EFS as Tier III modification
added NVD/Thermal as Tier III modification
added Mistral SATCP as Tier IV modification
added its basic and custom loadouts
new skin – white
AH-1S (all), Tzefa
M200A1 modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
SA 342 L
Replacing helicopter blades modification – Tier III → II
HF7D modification – Tier II → I
single HJ8A options removed from both pylons (they still have the dual options)
Z10
aileron power loss – 2 → 1
rudder power loss – 2 → 1
elevator power loss – 2 → 1
length – 16 → 14.15 m
modifications can now change longitudinal balance
aileron max dynamic viscosity – 9 → 10
rudder max dynamic viscosity – 9 → 10
elevator max dynamic viscosity – 9 → 10
rip speed – 310 → 340 km/h
moment of inertia increased
gear drag coefficient – 0.135 → 0.115
"wing" and fuselage span, area and angle increased
aileron angles – 0.2° → 15°
aileron sensitivity – 0.2 → 0.099
elevator angles – 0.1° → -7.7° / 12.5°
elevator sensitivity – 0.7 → 0.23
rudder angles – 0.1° → 14.5°
rudder sensitivity – 0.5 → 0.25
engine weight – 187 → 207 kg
min engine RPM – 4600 → 12.500
max engine RPM – 6100 → 20.900
min shaft RPM – 4600 → 11.000
max shaft RPM – 6100 → 20.900
turbine time constant – 0.6 → 1.26
power – 940 → 1280
takeoff thrust – 90 → 110 N
torque increased at 2-4 km at all speeds
main propeller:
radius – 6 → 6.5
blades – 4 → 5
max blade angle – 0.4° → 0.25°
roll and pitch damping lowered
weight – 110 → 270 kg
diameter – 12 → 13 m
moment of inertia coefficient – 1 → 0.7
governor min pitch – 4° → 0°
governor max pitch – 16° → 14°
tail propeller:
radius – 0.55 → 1.4
blades – 11 → 4
max blade angle – 0° → 0.95°
roll and pitch damping increased
lift coefficient increased
drag coefficient lowered
Oswald's efficiency number – 57.78 → 7.7
weight – 8 → 30 kg
diameter – 0.69 → 3.5 m
moment of inertia coefficient – 1 → 0.7
governor min pitch – -18° → -14°
governor max pitch – 32° → 26°
propeller rip speed – 510 → 480 km/h
empty weight – 2510 → 5050 kg
max fuel weight – 820 → 1660 kg
oil weight – 45 → 50 kg
full weight – 4250 → 7500 kg
center of gravity changed
gear sink rate multiplier – 1.02395 → 1.04088
nose gear:
spring height – 0.135 → 0.6
spring coefficient – 190.000 → 200.000
spring damping coefficient – 2 → 1
spring damping force max multiplier – 3 → 1
wheel radius – 0.625 → 0.9
steering – fixed → manual
wing gears:
spring height – 0.212 → 0.6
spring coefficient – 190.000 → 200.000
spring damping coefficient – 2 → 1
spring damping force max multiplier – 3 → 1
wheel radius – 0.625 → 0.9048
added a laser designator
radar display removed from the MFD
Replacing helicopter blades modification – Tier III → II
HJ8A modification removed
new skin – twitch
Z11WA
HF7D modification – Tier II → I
HJ8A modification – Tier III → IV
Replacing helicopter blades modification – Tier III → II
HJ8C modification removed
HJ8C options removed
new skins – 2color, 3color
Z19 (all)
moment of inertia increased
vertical stabiliser angle – -8° → -4°
engine max "allowed" RPM – 7600 → 7900
engine moment of inertia increased
main propeller max blade angle – 0.4° → 0.32°
main propeller roll and pitch damping lowered
optic angular limits – -60° / 60° / -40° / 10° → -115° / 115° / -80° / 30°
HF7D modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
A109
12.7 mm belts modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
New 12.7 mm MGs modification – Tier IV → II
EFS modification – Tier IV → III
A129 (ATP)
Replacing helicopter blades modification – Tier III → II
New 12.7 mm MGs modification – Tier IV → III
EFS modification – Tier IV → III
A129 CBT
12.7 mm belts modification – Tier III → II
Replacing helicopter blades modification – Tier IV → II
New 12.7 mm MGs modification – Tier IV → III
EFS modification – Tier IV → III
AB205A-1
New 7.62 mm MGs modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
I.A.R.316 B
New 7.62 mm MGs modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
SE 313 B
New 7.62 mm MGs modification – Tier III → I
Replacing helicopter blades modification – Tier III → II
Tigre HAD, Tigre HAP
New 30 mm cannons modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
Hkp 3C
Replacing helicopter blades modification – Tier III → II
added automatic EFS as Tier III modification
Tzefa B
M200A1 modification – Tier III → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
Tzefa D/E
M261 LWL modification – Tier II → I
Replacing helicopter blades modification – Tier III → II
EFS modification – Tier IV → III
