EVEKTOR-AEROTECHNIK Harmony LSA, Operating Instructions Manual

Page: 90 / 132

AIRCRAFT OPERATING INSTRUCTIONS
Doc. No. HARMAOIUS
June 01, 2011
6-8
Section 6
Weight and
Balance
6.5 Airplane Loading Schedule Chart
Type/Model: Harmony LSA
Serial No.:
Registration:
Input data
Arm
(m)
Weight
(kg)
Moment
(kg.m)
Arm
(m)
W eight
(kg)
Moment
(kg.m)
No. Item
(1) (2) (3) = (1) x (2) (1) (2) (3) = (1) x (2)
1.
Empty Airplane
See Weight and Balance Record delivered
with your airplane
0,148 363,9 53,9 0,148 364 54
2.
Crew
0,489 172 84,1 0,489 172 84
3.
Baggage
Max.: 25 kg
55 lb
1,027 25 25,7 1,027 25 26
4.
Fuel
Max. 120 l
Density 0.72 kg/ l
0,623 39,6 24,7 0,623 40 25
TOTAL WEIGHT
(kg)
TOTAL MOMENT
(kg.m)
TOTAL WEIGHT
(kg)
TOTAL MOMENT
(kg.m)
(7) = SUM (1÷4) (8) = SUM (1÷4) (7) = SUM (1÷4) (8) = SUM (1÷4)
601 188 601 188
C.G. (m):
=
TOTAL MOMENT
-------------------------- =
TOTAL WEIGHT
0,314
=
TOTAL MOMENT
-------------------------- =
TOTAL WEIGHT
0,314
C.G.' (% MAC):
=
C.G. (m)
------------- x 100 =
MAC
26,4
=
C.G. (m)
------------- x 100 =
MAC
26,4
Explanation:
C.G. (m) Center of Gravity position from Datum origin (0,05615 m behind W ing leading edge)
C.G.' (%MAC) Center of Gravity position in percent of Mean Aerodynamic Chord
MAC (m)
Mean Aerodynamic Chord (m) 1,1855
Limits:
600 kg Maximum Takeoff Weight (with Vortex Generators - valid for the USA)
575 kg Maximum Takeoff Weight (No Vortex Generators - valid for the USA)
14
±
5 %MAC Empty Airplane C.G. Range
13 - 33 %MAC Operating C.G.range
Sample Aircraft Your Aircraft
LOADING SCHEDULE CHART