Up Home

Nav: Valentin Thomas: Cervin

LaTeX - PDF
Navigation: Valentin Thomas: Cervin
Airplane: HB-KHV (DR400-180)
Planning speed: 100kts (climb: 92kts)
Variation: 2°E
Mass [kg]:
Waypoint TC MC Dist. Altitude EET Wind MH GS EET ETO ATO Notes
[°] [°] [NM] [ft] [min] [°] [kts] [°] [kts] [min]
LSGS
NW VAC 6 ©4+5
Martigny 244 242 7 ©5
Mauvoisin 122 120 15 8000 ©10
C. Bertol 051 049 13 12500 ©8
Gornergrat 095 093 12 7
C. Hérens 275 273 9 5
Evolène 321 319 8 11000 5
E1 009 007 12 3000 7
E2 V 5 3
LSGS VAC 5 2700 3+5
92 67
Alternate
Circuits + fuel V 40 24
LSTA VAC 22 3700 13+5
62 42
TOD:
Compute TH with wind:
  1. α1 = (360 + TC - WH) % 360 and sign=1
    if α1 > 180: α1 = (360 + WH - TC) % 360 and sign=-1
  2. α2 = arcsin(WS/TS sin(α1))
  3. α3 = 180 - α1 - α2
  4. TH = TC + sign α2
  5. GS = sin(α3) / sin(α1) TS
Fuel Fuel consumption: 40 l/h
No wind Wind
time fuel [l] time fuel [l]
Trip: 1:07 45
Alternate: 0:42 28
Reserve: 0:45 30
Unusable: 1
Minimum fuel: 104
Extra +5%: 6
Ramp fuel: 110
Mass and balance Mass Arm Moment
[kg] [m] [m kg]
Dry+Empty (2020-12-02) 639 202.048
Front 180 0.41 73.8
Rear #1 70 1.19 83.3
Luggage #1 5 1.9 9.5
Unusable fuel #1=1l 0.72 1.12 0.806
Unusable fuel #2=0l 0 0.1 0
Unusable fuel #3=0l 0 0.1 0
0-fuel 0.428 369.454
894.72   0.413
MLDGW=1045 0.564
Fuel #1=109+1l 78.48 1.12 87.898
Fuel #2=40+0l 28.8 0.1 2.88
Fuel #3=0+0l 0 0.1 0
Take-off 0.428 460.232
1002   0.459
1100 0.564
1 USG = 3.785 liters
1 Imp.G = 4.55 liters
1 l Avgas = 0.72 kg
1 USG Avgas = 6 lbs
login
H C F G I