EasyManua.ls Logo

sonaca aircraft S201 - Fuel System

Default Icon
283 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
S201 AFM
7 - AIRPLANE AND SYSTEMS
DESCRIPTION
7.10 - FUEL SYSTEM
27/06/2019
SONAIR-S2-D-MAN-006
Rev. : A
7.10 FUEL SYSTEM
The airplane has 2 fuel tanks located each in the inside leading edge of each wing.
Each tank is equipped with a vent with an internal inlet at the inboard top of the
tank and the outlet underneath the wing. The Fuel tank outlet is equipped with
an internal copper mesh finger screen acting as a filter.
A drain valve is located in the lowest point of the each tank.
Tank outlets lead to a fuel selector valve situated on the central console in the
cockpit.
Fuel return lines return excess fuel supplied by the fuel pump to the fuel tank in
use.
The system is configured as in the diagram below.
Fuel selector handle
with extension
Fuel selector
valve
Fuel tank
Fuel tank filler
cap
Fuel pressure
regulator
Fuel level
sender / sensor
Feed line
Fuel tank vent
Return line
2x Fuel flow meters
(feed & return,
behind engine)
Fuel tank outlet
with mesh screen
Fuel pumps
Fuel filter /
Gascolator
(behind engine)
Fuel pressure sensor

Table of Contents

Other manuals for sonaca aircraft S201