Rev: 2
Date: 11/15/18
13-10
I
NSTALLATION
:
1. Installation procedure is reverse of the removal procedure. Use thread sealant
on the threads when re-installing the quick-drain valve.
C
OARSE FUEL TANK SCREEN REMOVAL
Expendable
pipe thread sealant
Replaceable
None
Service Rating
Line
Minimum Certification
LSA-RM or A&P
Additional References
KAI
1. Drain the Fuel System. (13-17)
2. Remove the screws (4) and center access cover plate from the fuselage bottom
skin. (3-4)
3. Disconnect the fuel line (aft most fitting) from the fuel strainer on the bottom of
the tank.
4. Unthread the fuel strainer from the fuel tank.
5. Clean the screen and inspect same for breakage or separation from fitting.
Installation:
1. Installation procedure is reverse of the removal procedure. Apply thread sealant
paste to fuel strainer pipe threads before installation
.
F
UEL
P
RESSURE
/R
ETURN
A
SSEMBLY
R
EPLACEMENT
(ULS)
Special Tools
torque wrench(in-lb)
Protective Gloves
Expendable
Plastic tie-wrap 8in
Replaceable
VA-216 Fuel Pressure/Return Assembly
Service Rating
Line
Minimum Certification
LSA-RM with Rotax Service certification of A&P
with Rotax Service Certification
Additional References
KAI
NOTE:
W
HEN LOOSENING OR TIGHTENING THE BANJO BOLT SUPPORT THE CLAMP BLOCK
(
FUEL MANIFOLD
)
APPROPRIATELY
.
1. Drain fuel system forward of fuel valve. (13-4)
2. Disconnect both ends of Fuel Pressure/Return Assembly.
3. Remove banjo bolt M8X1X17 from top of clamp block.
4. Cut tie-wraps and remove Fuel Return Assembly.
■
W
ARNING
:
E
XPECT SOME FUEL DRAINAGE TO OCCUR AS THE HOSE CONNECTIONS ARE
REMOVED
.
U
SE PROTECTIVE GLOVES AND HAVE SHOP RAGS CLOSE BY
.
Summary of Contents for RV 12iS
Page 1: ...Rev 2 Date 11 15 18 i MAINTENANCE MANUAL Aircraft Serial Number ___________________________...
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Page 145: ...Rev 2 Date 11 15 18 13 1 Chapter 13 FUEL SYSTEM ULS SYSTEM iS SYSTEM...
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