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Navigation: Nathan

Airplane: HB-TDR (C182S)

Planning speed: 120kts (climb: 90kts)

Variation: 3°E

Mass [kg]:

Front: 330
Rears: #1=176
Luggages: #1=11 kg - #2=0 kg - #3=0 kg

Waypoint	TC	MC	Dist.	Altitude	EET	Wind		MH	GS	EET	ETO	ATO	Notes
Waypoint	[°]	[°]	[NM]	[ft]	[min]	[°]	[kts]	[°]	[kts]	[min]	ETO	ATO	Notes
LSGE

TOD:

120kts (2NM/min) 500 ft/min (children -12: 300)
3deg makes descent rate = GS x5
1NM attitude change
2NM speed decrease
2NM approach check (if needed)

Compute TH with wind:

α1 = (360 + TC - WH) % 360 and sign=1
if α1 > 180: α1 = (360 + WH - TC) % 360 and sign=-1
α2 = arcsin(WS/TS sin(α1))
α3 = 180 - α1 - α2
TH = TC + sign α2
GS = sin(α3) / sin(α1) TS

Fuel	Fuel consumption: 13 USG/h
	No wind		Wind
	time	fuel [USG]	time	fuel [USG]
Trip:
Alternate:
Reserve:
Unusable:
Minimum fuel:
Extra +5%:
Ramp fuel:

Fuel	Unusable	Usable	Total
Tank #1	2 USG	0 USG	2 USG
Tank #2	2 USG	0 USG	2 USG

Mass and balance	Mass	Arm	Moment
Mass and balance	[lbs]	[in]	[in lbs]
Dry+Empty (2020-04-01)	1974		75174
Front	330	37	12210
Rear #1	176	74	13024
Luggage #1	11	97	1067
Luggage #2	0	116	0
Luggage #3	0	129	0
Unusable fuel #1=2USG	11.99	46.5	557.535
Unusable fuel #2=2USG	11.99	46.5	557.535
ZeroFuel		min=40.9	102590.07
	2514.98	40.792
	MLdgW=2950	max=46
Fuel #1	0	46.5	0
Fuel #2	0	46.5	0
TakeOff		min=40.9	102590.07
	2514.98	40.792
	MTOW=3100	max=46

1 USG = 3.785 liters

1 Imp.G = 4.55 liters

1 l Avgas = 0.72 kg

1 USG Avgas = 6 lbs

H C F G I