Rans COYOTE II S-6ES, Техническое руководство

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020240cg msw 06/15/2011
024-1
TOTAL=
TOTAL=
DATUM = BACKSIDE OF PROP; AIRCRAFT IN
ACCEPTABLE C.G. 62.5" TO 73" FROM DATUM O.
LEVEL ATTITUDE. (LEVEL REFERENCE TO
MTOW
(912UL /912ULS)
DATE WEIGHED
ENGINE TYPE
C.G. CONDITION
EMPTY WEIGHT
** 30 LBS. MAXIMUM BAGGAGE
= C.G.
TOTAL=
= C.G.
TOTAL MOMENTS
TOTAL WEIGHT
NOSE WHEEL
BAGGAGE *
AFT BAGGAGE **
WING TANKS 18 GAL.
TOTAL MOMENTS
TOTAL WEIGHT
MAIN RH
MAIN LH
6
7
5
4
PILOTS
2
3
1
#
ITEM
* 50 LBS. MAXIMUM BAGGAGE
WEIGHT
90"
105"
78"
78"
ARM
26"
72"
72"
951
66110
TOTAL=
BAGGAGE *
AFT BAGGAGE **
MAIN RH
MAIN LH
NOSE WHEEL
WING TANKS 18 GAL. 3
6
7
5
4
PILOTS
#
2
1
ITEM
N
0
1
3
2
108
951
50
0
168
170
WEIGHT
340
115
72"
90"
105"
78"
78"
ARM
26"
72"
LEVEL AT DOOR BOTTOM
BOTTOM OF DOOR.)
6 4
5
7
=
MOMENT
=69.5
7776
4500
66110
0
13260
13104
MOMENT
2990
24480
1320 lbs.