7.11.2
B
ATTERIES
O
NE
SB12V15P-EC
AND ONE
SB12V10P-DC
LITHIUM BATTERIES ARE INSTALLED ON THE
UPPER FIREWALL
.
T
HEIR CHARACTERISTICS
ALLOW TO POWER THE ESSENTIAL ELECTRICAL
SYSTEM FOR MORE THAN TWO HOURS
,
EVEN IF
L A N D I N G I S R E Q U I R E D W I T H I N S I X T Y
MINUTES
.
A
TEMPERATURE SENSOR IS
LOCATED ON THE BATTERIES AREA
.
O
NLY THE
SPECIFIC
S
UPER
-B/O
PTIMATE
TM290
LITHIUM
CHARGER MUST BE USED
.
7.11.3
A
LTERNATORS
T
WO ALTERNATORS ARE INSTALLED
.
T
HE PRIMARY ALTERNATOR IS A
70
A
BELT DRIVEN
P
LANE
P
OWER
AL12-EI70.
T
HE STANDBY
ALTERNATOR IS A
P
ANE
P
OWER
FS1-14
MECHANICALLY CONNECTED
TO THE VACUM PUMP ENGINE PORT
.
I
N NORMAL OPERATION ONLY
PRIMARY ALTERNATOR IS SUPPLYING THE SYSTEM
.
A
LTERNATORS
MUST NOT BE OPERATED IN PARALLEL
.
Van’s RV7
Aircraft Flight
Manual
Rev 0.1
S/N 74141
Aircraft Flight
Manual
I-MKLK
DESCRIPTION OF THE AIRPLANE
I-MKLK AIRCRAFT FLIGHT MANUAL 7.0 137