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Section 6
Weight & Balance
LANCAIR COLUMBIA 400 (LC41-550FG) WEIGHT AND BALANCE
ENVELOPE
WEIGHT AND CG ENVELOPE LC41-550FG
3900
3800
3700
3600
3500
3400
3300
3200
3100
3000
2900
2800
2700
2600
2500
2400
2300
103
104
1. Airplane basic empty weight must be below Maximum Empty Weight (M.E.W.) and above
Minimum Flight Weight (M.F.W.).
2. Weight must be below Maximum Landing Weight (M.L.W.) for landing. (If overweight
landing occurs, see maintenance manual for required inspection prior to further flight.)
3. Weight and Center of Gravity (CG) without fuel must be below the Maximum Zero Fuel
Weight (M.Z.F.W.) line.
4. See Section 2 for a listing of weight limitations.
RC050002
6-18
2
M.E.W.
1
M.F.W.
105
106
107
108
CG FS (INCH)
Figure 6 - 20
Columbia 400 (LC41-550FG)
Max. Landing Weight
Max Zero Fuel Weight
3
109
110
111
112
Initial Issue of Manual: November 10, 2004
Latest Revision Level/Date: -/11-10-2004
113
114
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