Rebel Fuel Line Install
Posted: Sat Feb 18, 2012 2:29 pm
Hello Rebel Builders/Flyers:
I am in the process of installing an "under-floor" fuel system and
selector valve on Rebel 662. I took the Cessna approach with the layout,
and have been working on this for some time now.
The left and right lines will exit each tank going aft through (or
around?) the aft wing attach double bulkheads, then a 90 degree down
just aft of the door opening (bulkhead "F") through the angled ledge
channel, with a 90 degree forward through the door vertical bulkhead
then down through a "racetrack" slot in the sill (located just below the
door angled sill) forward through the double bulkhead to a 90 degree
inboard to the selector valve. Both left and right fuel lines will meet
here. A single line from the selector will go forward through both
square carrythroughs. The line will then run on the left side of the 5/8
square stiffener tube toward the firewall then to the gascolator which
will be mounted somewhere left of the aircraft centerline.
To date, the selector valve is mounted in the floor, between the seats ,
just right of centerline. Some of the lines on the right lower side have
been run. (See photos).
Last evening I took another long look at the installation and had some
questions in my pointed little head concerning my line routing. I have
never done this type of installation before so I am being cautious
(maybe too cautious). Unsure whether I am going at it in a sound and
correct manner, I thought it would be great to get some further opinions
and/or suggestions from others. To give you an idea of where I am at, I
have uploaded some installation photos to the archives for review.
Initially, I purchased some 3/8 tubing from my local hardware store for
mockup. This soft tubing seemed to make bending in place relatively
easy. Not realizing that the 3/8 fuel tubing received in my kit from MAM
was a LOT more rigid and made for some tough bending in place. I have
heard that some builders make runs all the way from the tanks to the
firewall with very few fittings! How the heck is that accomplished? Am I
doing something wrong here?
Note 1: As you can see from the photos, there is an access cover on the
outside of the bottom floor for selector access/maintenance (an access
cover on the inside was not an option as there is a lot going on the
inside in that area with float pump stuff, fuel valve mount, water
rudder mechanism, elevator cable pulleys, etc.). A hole will be drilled
in this access cover so the single, low point Saf-Air valve will
protrude making it accessible for pre flight. The cover plate will have
a watertight seal and there may be a streamlined "half" faring over the
drain valve for protection and make it water resistant from float spray.
Note 2: Wherever there is an "AN" fitting, there will be an access cover
for maintenance. (i.e. corner wraps).
Note 3: The selector valve handle will have a fiberglass safety cover
around it to prevent the possibility of accidentally moving it from its
intended position in flight.
A. Has anyone taken this approach to a fuel line installation?
B. Am I headed in the right direction with this installation?
C. If so, is it possible to accomplish this installation with less AN
fittings (longer tube runs)? How?
D. Is it acceptable to run the aluminum fuel lines through the "F"
double bulkheads, just below the wing fittings with grommets or should
the lines be routed around the wing fitting double bulkheads?
Suggestions, comments or criticism would be highly appreciated.
Thanks in advance.
Terry Dazey
Rebel 662
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I am in the process of installing an "under-floor" fuel system and
selector valve on Rebel 662. I took the Cessna approach with the layout,
and have been working on this for some time now.
The left and right lines will exit each tank going aft through (or
around?) the aft wing attach double bulkheads, then a 90 degree down
just aft of the door opening (bulkhead "F") through the angled ledge
channel, with a 90 degree forward through the door vertical bulkhead
then down through a "racetrack" slot in the sill (located just below the
door angled sill) forward through the double bulkhead to a 90 degree
inboard to the selector valve. Both left and right fuel lines will meet
here. A single line from the selector will go forward through both
square carrythroughs. The line will then run on the left side of the 5/8
square stiffener tube toward the firewall then to the gascolator which
will be mounted somewhere left of the aircraft centerline.
To date, the selector valve is mounted in the floor, between the seats ,
just right of centerline. Some of the lines on the right lower side have
been run. (See photos).
Last evening I took another long look at the installation and had some
questions in my pointed little head concerning my line routing. I have
never done this type of installation before so I am being cautious
(maybe too cautious). Unsure whether I am going at it in a sound and
correct manner, I thought it would be great to get some further opinions
and/or suggestions from others. To give you an idea of where I am at, I
have uploaded some installation photos to the archives for review.
Initially, I purchased some 3/8 tubing from my local hardware store for
mockup. This soft tubing seemed to make bending in place relatively
easy. Not realizing that the 3/8 fuel tubing received in my kit from MAM
was a LOT more rigid and made for some tough bending in place. I have
heard that some builders make runs all the way from the tanks to the
firewall with very few fittings! How the heck is that accomplished? Am I
doing something wrong here?
Note 1: As you can see from the photos, there is an access cover on the
outside of the bottom floor for selector access/maintenance (an access
cover on the inside was not an option as there is a lot going on the
inside in that area with float pump stuff, fuel valve mount, water
rudder mechanism, elevator cable pulleys, etc.). A hole will be drilled
in this access cover so the single, low point Saf-Air valve will
protrude making it accessible for pre flight. The cover plate will have
a watertight seal and there may be a streamlined "half" faring over the
drain valve for protection and make it water resistant from float spray.
Note 2: Wherever there is an "AN" fitting, there will be an access cover
for maintenance. (i.e. corner wraps).
Note 3: The selector valve handle will have a fiberglass safety cover
around it to prevent the possibility of accidentally moving it from its
intended position in flight.
A. Has anyone taken this approach to a fuel line installation?
B. Am I headed in the right direction with this installation?
C. If so, is it possible to accomplish this installation with less AN
fittings (longer tube runs)? How?
D. Is it acceptable to run the aluminum fuel lines through the "F"
double bulkheads, just below the wing fittings with grommets or should
the lines be routed around the wing fitting double bulkheads?
Suggestions, comments or criticism would be highly appreciated.
Thanks in advance.
Terry Dazey
Rebel 662
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