2.15
F
UEL
T
ANK CAPACITY
:
21
U.S.
GAL EACH
79
L
T
OTAL
F
UEL
:
42
U.S.
GAL
157
L
U
SABLE
F
UEL
:
41
U.S.
GAL
153
L
U
NUSABLE
F
UEL
:
1,2
U.S.
G
AL
4
L
F
UEL
G
RADES
:
A
VGAS
100LL
MOGAS
95/98UL
M
AX
E
THANOL
10%
2.16
E
LECTRIC
B
OTH ALTERNATORS MUST BE FULLY FUNCTIONAL WHEN
COMMENCING A FLIGHT
.
F
OR EXTENDED DEMONSTRATIONS OF THE AVIONICS ON GROUND
,
AN
EXTERNAL GROUND POWER SUPPLY IS REQUIRED TO KEEP A GOOD
STATE OF BATTERY
.
2.17
C
ROSSWIND
M
AX RECOMMENDED CROSSWIND COMPONENT FOR T
.
O
.
AND
LANDING
15
KTS
.
2.18
M
AXIMUM
P
ASSENGER
S
EATING
O
NE EXTRA SEAT IS AVAILABLE FOR A PASSENGER
.
F
OR
M
ASS AND
B
ALANCE CALCULATIONS REFER TO CHAPTER
6
“M
ASS AND
B
ALANCE
”
OF THIS
AFM.
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 33
