[Vasya]

Фм к Баффало МК.1.

[Aircraft]
  Type 1
  Crew 1
  Wingspan 10.72
  Length 7.55
  Seaplane 0
  Canard 0
  Jet 0
  JetHiV 0
[Mass]
  Empty 2080.0
  TakeOff 3036.0
  Oil 24.0
  Fuel 300.0
[Controls]
  CAileron 1
  CAileronTrim 1
  CElevator 1
  CElevatorTrim 1
  CRudder 1
  CRudderTrim 1
  CFlap 1
  CFlapPos 3
  CDiveBrake 0
  CInterceptor 0
  CEngine 1
  CVectoredThrust 0
  CUndercarriage 1
  CLockTailwheel 1
  CStabilizer 1
  CArrestorHook 0
  CWingFold 0
  OnlineCockpitDoor 0
  CCockpitDoor 1
  CockpitDoorPeriod 2.0
  CAileronThreshold 440.0
  CRudderThreshold 420.0
  CElevatorThreshold 440.0
  CDifferentialBrakes 1
  DefaultAileronTrim 0.021
  DefaultElevatorTrim -0.0
  DefaultRudderTrim 0.0881
[Squares]
  Wing 19.40
  Aileron 1.42
  Flap 1.4
  Stabilizer 1.60
  Elevator 1.57
  Keel 1.00
  Rudder 0.83
  Wing_In 4.35
  Wing_Mid 1.0
  Wing_Out 4.35
  AirbrakeCxS 0.0
[Arm]
  Aileron 3.18
  Flap 1.0
  Stabilizer 4.2
  Keel 4.3
  Elevator 4.55
  Rudder 4.78
  Wing_In 1.31
  Wing_Mid 1.0
  Wing_Out 3.5
  Wing_V 0.5
  GCenter 0.00
  GCenterZ 0.00
  GC_AOA_Shift 0.35
  GC_Flaps_Shift 0.10
  GC_Gear_Shift -0.35
[Toughness]
  AroneL 70
  AroneR 70
  CF 400
  Engine1 250
  Engine2 150
  Engine3 100
  Engine4 100
  GearL2 200
  GearR2 200
  Keel1 150
  Keel2 150
  Nose 100
  Oil 150
  Rudder1 70
  Rudder2 70
  StabL 70
  StabR 70
  Tail1 150
  Tail2 150
  Turret1B 50
  Turret2B 50
  Turret3B 50
  Turret4B 50
  Turret5B 50
  Turret6B 50
  VatorL 70
  VatorR 70
  WingLIn 150
  WingLMid 150
  WingLOut 150
  WingRIn 150
  WingRMid 150
  WingROut 150
  Flap01 30
  Flap02 30
  Flap03 30
  Flap04 30
[Engine]
  Engine0Family Wright_Cyclone-1820(MOD):Buffalo_Brewster 
  Engine0SubModel Wright-Cyclone-GR-1820G-105A
[Gear]
  H 1.54
  Pitch 16.8
  SinkFactor 1000.0
  SpringsStiffness 0.8
  TailStiffness 0.5
[Params]
  CriticalAOA 16.00
  CriticalCy 01.50
  CxCurvature 00.80
  CxStraightness 00.15
  CriticalAOAFlap 15.50
  CriticalCyFlap 01.65
  SpinTailAlpha 17.00
  SpinCxLoss 0.10
  SpinCyLoss 0.04
  Vyfac 1.0
  Tfac 1.09
  Vmin 140.0
  Vmax 428.0
  VmaxAllowed 750.0
  VmaxH 480.0
  HofVmax 4750.0
  VminFLAPS 120.0
  VmaxFLAPS 230.0
  Vz_climb 15.0
  V_climb 260.0
  T_turn 18.0
  V_turn 300.0
  K_max 11.0
  Cy0_max 0.12
  FlapsMult 1.0
  FlapsAngSh 4.0
  G_class_coeff 26.0
  G_class 12.0
  ReferenceWeight -18.0
  Range 675.0
  CruiseSpeed 180.0
  SensYaw 0.4
  SensPitch 0.62
  SensRoll 0.32
[Polares]
  lineCyCoeff 0.082
  AOAMinCx_Shift 0.207
  Cy0_0 0.13
  AOACritH_0 16.0
  AOACritL_0 -12.5
  CyCritH_0 1.23
  CyCritL_0 -0.788
  CxMin_0 0.0253
  parabCxCoeff_0 3.6E-4
  Cy0_1 0.62
  AOACritH_1 14.0
  AOACritL_1 -22.0
  CyCritH_1 1.547
  CyCritL_1 -0.73
  CxMin_1 0.072105
  parabCxCoeff_1 4.7E-4
  parabAngle 5.0
  Decline 0.008
  maxDistAng 40.0
  draw_graphs 0
  mc3 -13.929,-13.199,-8.3176,40.495,-78.44,-9.34,-0.78,-15.482
  mc4 36.966,41.96,256.62,-131.69,550.09,89.944,41.96,144.86
  mm 0.652,0.714,0.743,0.753,0.718,0.672,0.622,0.563
  mz 0.252,0.231,0.064,0.078,0.09,0.124,0.136,0.103
[SOUND]
  Engine Std

Хотел поставить вес 2030 кг., добавив на потяжелевшуую ВМГ,
но в дефолте пишут 2080 кг.
Склоняюсь к большему весу, потому как для жаркого климата могли чего либо засунуть в фюзеляж ещё - кондишн, например.