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Navigation: ZALuG Dents du Midi
Airplane: HB-KHV (DR400-180)
Planning speed: 110kts (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 7 ©5+5
Martigny V 7 ©5
Troistorrents V 8 ©5
Martigny V 15 8
W V 8 4
LSGS VAC 6 3+5
51 40
Alternate
Fill fuel tank V 80 44+5
LSTA VAC 22 12+5
102 66
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: 0:40 27
Alternate: 1:06 44
Reserve: 0:45 30
Unusable: 1
Minimum fuel: 102
Extra +5%: 6
Ramp fuel: 108
Fuel Unusable Usable Total
Tank #1 1 l 109 l 110 l ALL
Tank #2
Tank #3
Mass and balance Mass Arm Moment
[kg] [m] [m kg]
Dry+Empty (2020-12-02) 639 202.048
Front 120 0.41 49.2
Rear #1 85 1.19 101.15
Luggage #1 5 1.9 9.5
Unusable fuel #1=1l 0.72 1.12 0.806
Unusable fuel #2 0 0.1 0
Unusable fuel #3 0 0.1 0
ZeroFuel min=0.428 362.704
849.72 0.427
MLdgW=1045 max=0.564
Fuel #1=109l 78.48 1.12 87.898
Fuel #2 0 0.1 0
Fuel #3 0 0.1 0
TakeOff min=0.428 450.602
928.2 0.485
MTOW=1100 max=0.564
1 USG = 3.785 liters
1 Imp.G = 4.55 liters
1 l Avgas = 0.72 kg
1 USG Avgas = 6 lbs
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