Extra 200 - Page 90

CHAPTER 08
PAGE 6
EXT
RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
PAGE DATE: 1. July 1996
Empty Weight and Center of Gravity Position
EXTRA 200
Data according to "TC Data-Sheet" and "Pilot´s Operating Handbook and LBA ap-
proved Airplane Flight Manual" Doc.-No.: EA - 07701
Equipment according to Equipment List dated:
. . . . . . . . . . . .
Legend:
X
1
= Arm: fire wall - main wheels
X
2
= Arm: fire wall - tail wheel
X
G
= Arm: fire wall - Center of Gravity
W
1
= Net weight main wheel LH
W
2
= Net weight main wheel RH
W
3
= Net weight tail wheel
W = Empty weight
Item Weight Arm Moment
Main wheel LH (W
1
)
. . . . . . . .
kg
.
(X
1
)
. . . . . . . .
cm =
. . . . . . . . . .
kgcm
Main wheel RH (W
2
)
. . . . . . . .
kg
.
(X
1
)
. . . . . . . .
cm =
. . . . . . . . . .
kgcm
Tail wheel (W
3
)
. . . . . . . .
kg
.
(X
2
)
. . . . . . . .
cm =
. . . . . . . . . .
kgcm
Empty weight (W)
. . . . . . . .
kg Total moment
. . . . . . . . . . . . . .
kgcm
W
1
.
X
1
+ W
2
.
X
1
+ W
3
.
X
2
W
X
G
= W = W
1
+ W
2
+ W
3
= X
G
Total moment
Empty weight
Empty weight is (W)
. . . . . . . . . .
kg
*
.W
min
: 545kg
W
max
: 606kg (acro II)
W
max
: 591kg (acro I)
W
max
: 646kg (Normal Cat.)
Center of Gravity is (X
G
)
. . . . . . . . . .
cm aft fire wall.
Weighing performed by:
. . . . . . . . . . . . . .
Aircraft Inspector:
. . . . . . . . . . . . . .
Sign:
. . . . . . . . . . . . . .
* If value exceeds the given tolerances, contact the manufacturer.
WEIGHING