7.10.4
F
UEL
F
LOW
S
ENSORS
T
WO RED CUBE TYPE FUEL FLOW SENSOR ARE
PLUMBED RISPECTIVELY ON THE FEED AND ON
RETURN LINES
.
T
HEY ARE LOCATED FORWARD OF
THE FUEL PUMP MODULE JUST BEHIND THE
FIREWALL
.
T
HE FUEL FLOW INFORMATION IS FED
T O T H E
S
K Y V I E W
E M S ,
W H I C H H A S A
DETOTALIZER FUNCTION THAT CALCULATES
P R E D I C T E D F U E L R E M A I N I N G
.
T
H E F U E L
QUANTITY INFORMATION IN THE
S
KYVIEW MUST
BE UPDATED WHENEVER FUEL IS ADDED TO OR
DRAINED FROM THE FUEL TANKS
.
T
HE DISPLAYED
FUEL REMAINING VALUE DOES NOT TAKE INTO
ACCOUNT ANY POSSIBLE FUEL LEAKS
,
OR ERRONEOUS INPUT OF
STARTING FUEL QUANTITY
.
7.10.5
T
HROTTLE
B
ODY
T
HE AIR THROTTLE BODY CONTAINS
T H E B U T T E R F LY VA L V E T H AT
CONTROLS THE FLOW OF AIR TO THE
E N G I N E A S P O S I T I O N E D B Y T H E
COCKPIT THROTTLE CONTROL LEVER
.
I
T HAS AN
I
NTAKE AIR TEMPERATURE
SENSOR
,
ONE THROTTLE POSITION
S E N S O R W I R E T O T H E
E C U
S
.
F
URTHERMORE
I
T HAS TWO MAP PORT
CONNECTED TO TWO
MAP
SENSORS
.
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 7.0 132