Project: F-Bug   -  
            All Modified Project Activities / Entries :
    (Please mouse-over any icon to get a description of that function).


  
Builder Name:Stephen Oberrecht   -  
Project:   Not a Kit, Plans   -   VIEW REPORTS
Total Hours:733
Total Flight Time:
Start/Last Date:Feb 16, 2020 - No Finish Date
Engine:Continental A-65
 
Friendly URL: https://eaabuilderslog.org?s=F-Bug

Home or Last Project Picture

Apr 02, 2022     Fuel system testing - (10 hours) Category: Engine
Tubing filter valves priming pump hoses tested. An6
 
Apr 02, 2022     Bendix mag rebuild and timing - (30 hours)       Category: Engine
Bendix mag rebuild and timing


 
Sep 05, 2021     Nose Gear Support Structure - (35 hours) Category: Landing Gear
 
Jan 31, 2021     Engine assembly - (16 hours)       Category: Engine
Assembled the engine case and cylinders per Continental overhaul manual. Torque seals applied.


 
Jan 19, 2021     Balance pistons and rods - (2 hours)       Category: Landing Gear
Weigh and balance piston and rod sets


 
Jan 19, 2021     Prepare engine for assembly - (8 hours)       Category: Landing Gear
Finish polishing cam and crankshaft to 1500 grit and buff. Prepare case surfaces and thoroughly clean. Inspect and check threads on through bolts. Perform 3 step dye penetrant inspection


 
Feb 16, 2020     Inspect Prep and Prime Nose Gear - (10 hours)       Category: Landing Gear
Stripped and sand blasted to bare steel. Used disc sander to prep surface, cleaned and primed-then shrink wrapped to prevent corrosion to un-oiled exposed steel prior to final painting and assembly into forward fuselage frame.


 
Mar 24, 2020     Sand blast fuselage and struts - (30 hours)       Category: Engine
Sand blasted parts to remove old paint and surface corrosion. These photos show weld and tubing quality for structural assessments.


 
Mar 24, 2020     Sand blast fuselage and struts - (22 hours) Category: Engine
Sand blasted parts to remove old paint and surface corrosion. These photos show weld and tubing quality for structural assessments.
 
Apr 05, 2020     Prep engine parts - (8 hours)       Category: Engine
Prep engine parts


 
Nov 01, 2020     Low end fit up. - (6 hours) Category: Engine
Need new conn rod bushing for late model a-65. The next step after today's fit up is to evaluate the camshaft, cam followers, hydraulic lifters, and crank for clearances. I need to purchase some parts prior to engine assembly.
 
Dec 12, 2020     Work on refinishing propllers - (10 hours)       Category: Engine
Stripped aluminum prop to polish and paint tips. Did cosmetic work on wood prop and test fit to a-65 taper shaft hub.


 
Dec 12, 2020     Making progress on engine rebuild. - (65 hours)       Category: Engine
I ground and lapped valves and painted jugs and block. Inspected and reassembled the valve springs rockers. Inspected Polished (and ground) crank and cam. Test fit. Waiting for new (used ) lifters to arrive fir bottom end assembly. New certified hydraulic lifters arrived.


 
Jul 15, 2020     Began rebuild of canopy with new plexiglass. - (8 hours)       Category: Fuselage
I began the rebuild of the canopy.


 
Apr 11, 2020     High temp paint - (7 hours) Category: Engine
Painted engine parts with high temp engine paint.
 
Mar 15, 2020     Took 4 cylinders to One Stop Aviation bore 0.015 - (2 hours)       Category: Engine
Dropped off cylinders with rick at One Stop to bore all 4 cylinders to plus 0.015


 
Mar 15, 2020     VSI, turn coordinator, Parts Transponder, Parts Transceiver - (3 hours) Category: Avionics
Acquired more used instruments.
 
Mar 01, 2020     Backup engine disassembly and cleanup - (25 hours) Category: Engine
The engine was disassembled and cleaned up. New pistons and rods were purchased.
 
Mar 01, 2020     Backup engine disassembly and cleanup - (25 hours) Category: Engine
The engine was disassembled and cleaned up. New pistons and rods were purchased.
 
Feb 26, 2020     Second engine disassembled and ready for assessment - (25 hours)       Category: Engine
The second Continental A-65 engine has been fully disassembled down to splitting the crank case and all the parts have been cleaned. Any surface corrosion on parts has been removed. The crankshaft and cam shaft may need to be inspected. The new pistons are plus .015 in. The cylinders may need to be bored. A honing tool was bought and delivered.


 
Feb 27, 2020     Gyro Centuri Arrived Category: Avionics
Gyro Venturi arrived.
 
Feb 27, 2020     Gyro Centuri Arrived       Category: Avionics
Gyro Venturi arrived.


 
Feb 27, 2020     Tires Arrived       Category: Landing Gear
The ��ew��Condor 5.00-5 retread tires arrived


 
Feb 27, 2020     Paint Landing Gear White - (3 hours) Category: Landing Gear
Painted the previously primed nose and main gear white (Krylon Pure White).
 
Feb 27, 2020     Paint Landing Gear White - (3 hours)       Category: Landing Gear
Painted the previously primed nose and main gear white (Krylon Pure White).


 
Feb 26, 2020     See empannage. Category: Tail Feathers
See empannage
 
Feb 26, 2020     Tail prep - (7 hours)       Category: Empennage
Removed paint and corrosion. There's still more surface corrosion removal to be done.


 
Feb 26, 2020     Aileron link lever to external aileron control - (6 hours)       Category: Controls
The link was stripped to bare metal, corrosion was removed, and it was cleaned prior to priming and painting.


 
Feb 26, 2020     Fuel tank restoration - (8 hours)       Category: Fuel System
The tank was treated internally with corrosion inhibitor, it was lrepped and primed, and the cap was fully restored. The copper tube was removed straightened and re brazed.


 
Feb 16, 2020     Acquired gauges - (10 hours) Category: Avionics
Instruments acquired: tachometer, airspeed, pitot tubes, altimeter, engine oil pressure, engine oil temperature, whiskey compass, fuel. Since there is no electrical system, additional gauges will need to be battery powered. A Venturi vacuum gyro system is being considered.
 
Feb 16, 2020     Setup Fuselage stand       Category: Workshop
An fuselage stand was improvised with two inexpensive engine stands. It allows rotating the fuselage while working for ease of access.


 
Feb 16, 2020     Acquired more tools - (10 hours) Category: Fuselage
220v mig welder, engine stands (x3 also used to lift and rotate fuselage) clekos riveters pneumatic drill tubing notcher precision calipers inside and outside for pistons and cylinders tap and die set steel blade for niter saw wire brushes grinder high speed rotary grinder
 
Feb 16, 2020     Fuselage stripping and sanding. - (4 hours) Category: Fuselage
Continued fuselage stripping for corrosion and weld inspections.
 
Feb 08, 2020     Main gear stripped - (6 hours)       Category: Landing Gear
The main gear were stripped and inspected. There are some regions where plastic deformation is seen. It is not likely a structural concern but it is unsightly. I wonder if welding in half cylinder doublers is a good option?


 
Jan 18, 2020     Initial Entry - (80 hours)       Category: Research
Initial entry: Stits Flutterbug Project.

1. Starting with Plans built, never completed, project. Never registered.
2. Teardown to bare metal, spars, and ribs nearly complete
3. Controls Removed (all parts labeled and mapped).
4. Fuel tank removed (all parts labeled and mapped).
5. Gear removed Striped and sand blasted.
6. Wheels removed and overhaul in progress. Nose axel replaced. all bearings replaced. (all parts labeled and mapped).
7. Second (Backup) A-65 engine overhaul and rebuild in progress. New pistons, rods, and 3 new cylinders acquired.
8. Plans restored and transcribing to CAD begun.

Next steps: Complete Teardown paint stripping; perform structural inspection; perform design analysis.

Design considerations:
��Install alternative wing and brace mounting hard points and wing-root lugs two inches aft for improved weight and balance envelope
��Install optional tail-dragged hardpoints
��Lighten overdesigned wing by omitting or making aluminum internal shear struts which are heavy steel as designed.
��Wing tanks
��Improve trim controls for safety in event of ingle point structural or fastener failure. Improve failure configuration for control surface stability
��Lighten heavy steel wing struts using lighter steel and braced for buckling stability
��Rebuild main gear for 8��wider stance?


 


NOTE: This information is strictly used for the EAA Builders Log project within the EAA organization.     -     Policy     -     © Copyright 2024 Brevard Web Pro, Inc.