2.8
W
EIGHTS
E
MPTY
W
EIGHT
:
522,5
KG
1151
LBS
M
AX
G
ROSS
W
EIGHT
:
816
KG
1800
LBS
A
EROBATIC
G
ROSS
W
EIGHT
: 725
KG
1600
LBS
M
AX
B
AGGAGE
:
45
KG
100
LBS
2.9
C
ENTRE OF
G
RAVITY
D
ATUM
T
HE
D
ATUM PLANE ON THIS AIRPLANE IS A VIRTUAL PLANE
,
NORMAL TO THE LONGITUDINAL AXIS OF THE FUSELAGE
,
AT A
DISTANCE OF
70
IN FORWARD OF THE WING LEADING EDGES
.
C
ENTER OF
G
RAVITY
L
IMITS
T
HE
C
ENTER OF
G
RAVITY
(CG)
FOR FLIGHT CONDITIONS MUST
MEET THE FOLLOWING CONDITIONS
:
F
ORWARD
CG
L
IMIT
:
15%
OF CHORD OR
78.7”
AFT OF DATUM
.
A
FT
CG
L
IMIT
:
29%
OF CHORD OR
86.82”
AFT OF DATUM
.
A
EROBATIC
A
FT
CG
L
IMIT
:
25%
OF CHORD OR
84.5”
AFT OF
DATUM
.
WARNING
Exceeding the CG limits will reduce controllability and stability of this
airplane. This situation is dangerous to flight and must be avoided by
careful M&B
calculations. Refer to
chapter 6 “Mass and
Balance” for more information.
Van’s RV7
Aircraft Flight
Manual
Rev 0.1
S/N 74141
Aircraft Flight
Manual
I-MKLK
LIMITATIONS
I-MKLK AIRCRAFT FLIGHT MANUAL 2.0 30
