Bailey Moyes 912 Dragonfly, Maintenance Manual

Page: 76 / 191

Page 75
Section 27
Maintenance & Inspection
Dragonfly 912
912 FUEL SYSTEM
STEP INSTRUCTIONS
for Assembly, for Disassembly reverse the order!
PART NO. STAGE CERT.
1 Drill 3/32” hole through cap of fuel tank
or ventilation.
DFP 051
2 Insert Fuel Strainer
into Gates # 27348 Fuel Line 5/16” I.D.
making sure it is installed with the arrow pointing upwards, fasten with
hose clamp 1/4”.
G# 27348
DFO 051
3 Cut 2” length of Gates #27093 Submersible Fuel Line 5/16 “ I.D., install on
under side of cap, install fuel tank pick up tube
and fasten with hose clamps..
G# 27093
DFG 009
4 Route 5/16” Multi Fuel/Fuel Injection line
5 Cut 2” length of Gates # 27348 Fuel Line 5/16” I.D. , install onto fuel strainer
and fasten with hose clamp 1/4”
6
Install Gates # 27348 Fuel Line 5/16” I.D. from strainer to Shut-Off Valve ,
& from Shutoff valve to Tee (5/16” Brass) then to Electric Fuel Pump ,
(arrow pointing at engine) , then to second Tee, Then back to Engine Fuel
Pump on gearbox. Use fule line from Tees to
Check Valve
insuring arrow is pointed at engine, fasten all w/ hose clamps.
Add
Return Line of ¼” Superthane Tubing , from fuel bypass on top of
engine back along Fuel Supply line back to Fuel Tank Cap.
EASOV-120S
P60504
PA 5/16CV
(Lockwood)
NAPA
(1) Recommended Special Tools: None
(2) The parts needed to perform the task: Replace worn/damaged parts as needed, listed above. Max. Wear (defined 1.1.8.1)
(3) Type of maintenance: Inspection=Line & Replacement=Heavy
(when it involves replacement of structural components.) &
Replacement of Fuel System Components.
(4) Certification needed to accomplish the task: Line=LSRI Inspection or above, Heavy=LSRM Maintenance or above.
see:
3 Level of Certification in this manual
(5) Detailed instructions and diagrams as needed to perform the task, listed above and adjacent page.
Every Annual or 100 Hrs., Inspect for Cracks, Corrosion, Elongation of holes & Fasteners for Wear & Security.
(6) Method to test/inspect to verify the task was accomplished properly. Insure that all procedures were followed correctly and
there is proper non-binding movement to moving parts and that fasteners were tightened as instructed. When flight
controls are involved, assure that they are operating properly.
Section 27 912 Fuel System
Section 27