
MODIFICATIONS
Installation of an auto fuel STC on a low compression 80/87 octane engine
is an uncomplicated procedure. No major modifications are needed on this
type of engine. We supply all placards and paperwork. An IA mechanic must
"install" the STC by adding the new fuel placards and an engine
placard. He then fills out a log book entry and form 337. The whole process
takes approximately 30 minutes. No additional modification is required on
this type of engine.
The same holds true generally for the higher compression Lycoming 0-360
and 0-320 engines depending upon the airframe in which they are installed.
Generally speaking when these engines are mounted in an airframe equipped
with a gravity feed fuel system (no fuel pumps), installation of the STC's
consists only of paperwork and placards, with no modifications made. Some
people then reason why buy an STC if it's only paperwork and placards. Installing
the STC makes it possible for you to use an octane different than what was
called for on the original Type Certificate while remaining in compliance
with FAA regulations. Insurance companies expect you to be in compliance
with the FAR's and we are able to contact you if we become aware of any
changes in the fuel which could effect your airplane. For more info on this
check out FAR's: Part 43, App. A (2) (vi), 43.3 (a), 43.12, and 21.183 (d)
(1).
In some airframes equipped with suction lift fuel systems (pump fed systems),
different electric fuel pumps may need to be installed to insure adequate
fuel flow, and/or the fuel pump locations must be moved. The STC for the
PA-28-160, -161, -180, -181 requires
the removal of the factory installed electric pump. This pump is replaced
with two completely different pumps and the fuel system is rebuilt. Installation
on this airplane takes between four and six hours, approximtely double that on 24 volt PA-28's.
Click here for more info on the Piper PA-28, -160 thru -181
