sonex work log
|
DATE |
PAGE OR PART N0. |
DESCRIPTION |
TIME |
||||
|
Total recorded time-------------> |
950.20 |
||||||
|
2/5/11 |
E01 P01 |
tap and mount oil temp sender in sump plate, fabricate breather pipe from engine through rear baffle fence |
2.00 |
||||
|
2/4/11 |
E01 P01 |
Purchased 14 X 1.5 tap for oil temp sender and 5/8 tubing bender |
|||||
|
2/2/11 |
E01 |
Install 2 stud mounts for fuel level sender control unit, install lead for oil pressure sender |
3.00 |
||||
|
2/1/11 |
E01 |
troubleshoot master switch- had to move keyway up- schematic of switch shows off position up, wire and label charge relay, charge light, verify mag switch wiring, temporarily install tank, make 4 brackets for radio |
2.50 |
||||
|
1/31/11 |
P01 |
clean out inside of exhaust pipes, mark and drill holes for exhaust thermocouples |
1.50 |
||||
|
1/27/11 |
E01 |
Install 2 cht probes on left cylind head, route mag kill wires |
0.60 |
||||
|
1/26/11 |
E01 |
Install 2 right side temp sensors, broke screw off in head and had to remove |
1.00 |
||||
|
1/25/11 |
E01 |
solder ground wires and route 27 and 27- mag kill wires, cleco 3 firewall wire clamps, clean up firewall wiring |
1.50 |
||||
|
1/24/11 |
E01 |
install wire 38 to switch, work on wire list |
1.50 |
||||
|
1/23/11 |
P01 E01 |
make return line for oil separator to engine, wire up terminal block on firewall, modify schematic for 4 more wires- 2 more wires through firewall |
1.50 |
||||
|
1/22/11 |
E01P01 |
work on tidying harness, install clamps to run coax to rear on left and right, drill and rivet oil separator |
4.00 |
||||
|
1/20/11 |
E01 |
wire stroe, nav, and pfd power leads to panel switches- all switch wiring done |
2.00 |
||||
|
1/19/11 |
E01 |
Complete 5 switches connections at panel |
1.50 |
||||
|
1/18/11 |
E01 |
fabricate wires for mag switch conns, install several clamps for harness |
2.00 |
||||
|
1/17/11 |
E01 |
start cleaning up wire harness |
1.50 |
||||
|
1/16/11 |
E01 |
install all wiring in molex connector for radio tray, install comm antenna, install coax tray connector |
3.00 |
||||
|
1/12/11 |
E01 |
assemble and solder TED 9-20-10 right angle coax tray connector to rg400 coax- had to make custom bushing for cable in connector, ordered more molex conns from steinair and coax conns from aircraft spruce |
1.50 |
||||
|
1/11/11 |
E01 |
bought rj59 that was too stiff, screw around with several coax connectors, terminate a couple wires to radio tray |
1.50 |
||||
|
1/10/11 |
E01 |
start assembling radio harness connectors |
2.00 |
||||
|
1/8/11 |
P13 P30 |
trim oil cooler baffle, finally got cowl to fit over all baffling, clean shop, cut out 2 fuel filler doors, drill and cleco to cowl |
3.00 |
||||
|
1/5/11 |
P13 |
trim oil cooler baffles |
1.00 |
||||
|
1/3/11 |
P13 |
trim front upper baffles |
3.00 |
||||
|
1/1,2/11 |
P13 |
work on fitting baffles- cowl on and off a million times |
5.00 |
||||
|
12/31/10 |
P13 |
remove cowling and lay in inner patches on left and right bottom corners |
1.00 |
||||
|
12/30/10 |
P13 |
prepare surfaces and apply patches to cowl bottom corners |
2.00 |
||||
|
12/28/10 |
P13 |
remove cowl, fit front baffle seal, refit cowl onto fuse, rt side too low on bottom piece, hangs out at corner |
1.00 |
||||
|
12/27/10 |
P13 |
cut slices in bottom corners of cowl and refit onto fuselage |
0.50 |
||||
|
12/26/10 |
P13 |
start fine tuning of cowl and baffle fit |
4.00 |
||||
|
12/24/10 |
P13 |
finish riveting cowl hinges (day off work) |
5.00 |
||||
|
12/23/10 |
P13 |
prep cowling for rivets into hinges |
1.00 |
||||
|
12/22/10 |
P13 |
fit side baffles back onto engine with seals installed |
1.50 |
||||
|
12/21/10 |
P30 |
install baffle for oil cooler |
0.50 |
||||
|
12/20/10 |
P30 |
Cut 2 strips for oil cooler and rough fit seal |
1.00 |
||||
|
12/18,19/10 |
P30 |
work on engine baffle seals |
5.00 |
||||
|
12/17/10 |
P30 |
make pattern and mark piece p30-36 |
0.30 |
||||
|
12/16/10 |
P30 |
Fabricate 3 more strips for baffle, left p30-42,44,46 |
1.50 |
||||
|
12/15/10 |
P30 |
work on 2 strips for baffle seal p30-39,43 |
1.00 |
||||
|
12/14/10 |
E01 |
clean up wire harness for PTT, mount 3 clamps on headphone harness and bundle with shrinkwrap tape |
1.00 |
||||
|
12/13/10 |
E01 |
assemble PTT switches and control sticks |
1.00 |
||||
|
12/12,12/10 |
headset bracket fabricate and install, wire harness to headset jacks, terminal block on firewall, file seat pan, cleco control rod cover, cut control sticks 2 inches |
5.00 |
|||||
|
12/7/10 |
P13 |
add more layers to cowl tab |
0.50 |
||||
|
12/6/10 |
e01,p13 |
order wire for headsets and terminal block parts, fabricate fiberglass tab for cowling |
1.00 |
||||
|
12/4-5/10 |
cut panel for radio and LRI, dissassemble molex connector for radio, review wiring for headsets |
5.00 |
|||||
|
11/30/11 |
E01 |
work on fitting wiring harness |
1.00 |
||||
|
11/25-29/10 |
P30 |
continue to work on fitting baffle inside cowling, fitting seals |
8.00 |
||||
|
11/24/10 |
P30 |
work on baffle pieces bending and trimming, cut for intake pipes and seals |
0.50 |
||||
|
11/22/10 |
P30 |
start making bends on fence baffle, remake rt side baffle P30-32 |
2.00 |
||||
|
11/20-21/10 |
E01 |
mount rdac, charge relay, install most of wiring for start and charge, CD ignition, xpdr, mag ground, ground G3, work on wire numbering and labels, revised schematic with numbers |
12.00 |
||||
|
1/19/10 |
E01 |
work on wiring |
2.00 |
||||
|
11/15/10 |
E01 |
make new b and c order for relay new master switch, other electrical items |
|||||
|
11/14/10 |
E01 |
revise schematic, mount G2 ground on firewall |
2.00 |
||||
|
11/13/10 |
E01 |
update website, build order from b and c for relays, cable, wire, etc |
4.00 |
||||
|
11/12/10 |
E01 |
review schematic |
|||||
|
11/8/10 |
set cowling aside, remove glareshield, start laying out electrical components |
1.00 |
|||||
|
11/7/10 |
P13 |
mate cowl halves, pilot drill and cleco all hinge halves except lt and rt rear bottom, cut fuel filler and oil cooler and exhaust openings |
6.00 |
||||
|
11/6/10 |
P13 |
cut rt cowl bottom centerline and exhaust and windshield bow |
2.00 |
||||
|
11/4/10 |
P13 |
cut rt cowl centerline top and bottom rear edges, grind clearance on windshield bow for 3 dzeus receptacles |
0.50 |
||||
|
11/3/10 |
P13 |
refit rt cowling, drill holes for dzeus fasteners- need to clearance windshield bow holes for dzeus, marked cut lines for top and rear edges, need to mark bottom centerline thru prop and nose gear and frewall |
2.00 |
||||
|
11/2/10 |
P13 |
fit lt cowl, mark and cut side |
1.00 |
||||
|
10/31/10 |
P13 |
ordered southco fasteners |
|||||
|
10/30/10 |
P13 |
fit side hinge on rt cowl |
0.80 |
||||
|
10/29/10 |
P13 |
mixed epoxy, patched in back side of rt cowl |
0.50 |
||||
|
10/28/10 |
P13 |
trimmed rt side of cowling too much! |
0.50 |
||||
|
10/27/10 |
P13 |
cut and drill all hinge halves for cowling, lay out hinges on hinge pins |
2.00 |
||||
|
10/25/10 |
P13 |
work on rt cowl, ordered fuse panel and connectors from b and c |
1.00 |
||||
|
10/24/10 |
P01 P13 |
dismount, remount engine two times to correct thrust angle, start trimming back edges of cowl |
4.00 |
||||
|
10/23/10 |
P01 P13 |
work on cowl fit, find thrust line down, make fuel line from firewall to carb |
1.50 |
||||
|
10/21/10 |
P13 |
test fit rt cowl |
0.50 |
||||
|
10/20/10 |
P13 |
cut prop hub holes in cowl, sent email to kerry about fitting cowl around hub |
1.00 |
||||
|
10/19/10 |
order fittings for fuel line with -06 hose |
||||||
|
10/18/10 |
P30 |
re do oil cooler lines, clean shop |
2.00 |
||||
|
10/17/10 |
P01 |
construct oil cooler baffle, fittings, lines for cooler assy to engine, trim neck of fuel tank, build prop alignment spacer |
5.00 |
||||
|
10/16/10 |
E01 |
connect wiring from transponder to encoder, shop b and c for connectors |
1.50 |
||||
|
10/12/10 |
E01 |
ordered rdac and egt sensors, figure out thread sizes for strainier |
|||||
|
10/10/10 |
E01 |
study wiring for transponder and encoder, ordered crimpers |
1.00 |
||||
|
9/29/10 |
finish installing nutserts on panel brackets |
2.50 |
|||||
|
9/28/10 |
work on nutserts panel bracket |
0.50 |
|||||
|
9/27/10 |
cleco in glareshield to finish drilling glareshield to panel brackets |
0.50 |
|||||
|
9/23/10 |
finish installing nutserts in lower crosstie |
0.50 |
|||||
|
9/22/10 |
install most of rivnuts in lower crosstie, rivet and rivnut switch bracket |
1.50 |
|||||
|
9/21/10 |
make spacers for rivnuts on panel mountings |
1.00 |
|||||
|
9/20/10 |
install rivnuts in left bracket |
0.50 |
|||||
|
9/19/10 |
install rivnuts in right bracket for instrument panel lower crosstie |
1.00 |
|||||
|
9/16/10 |
remake switch bracket |
1.00 |
|||||
|
9/15/10 |
cut, drill, bend switch bracket |
1.50 |
|||||
|
9/14/10 |
P30 |
rivet control mounting bracket to lower dash crosspiece, fit in throttle lever, pitch wheel and mixture cable |
1.00 |
||||
|
9/13/10 |
P30 |
fit lower dash crosspiece support for center control quadrant, drill and dimple |
1.00 |
||||
|
9/12/10 |
P30 |
cut drill and polish bracket for throttle and mixture |
2.00 |
||||
|
9/11/10 |
P30 |
remove exh studs, install exhaust, install intake and carb, start fitting throttle quadrant to panel |
3.00 |
||||
|
9/10/10 |
P30 |
fit intake pipe, grind mount area to clear lower magneto, mark and drill bolt hole for mounting bolt |
1.50 |
||||
|
9/9/10 |
P30 |
clean shop, review plans for baffles, oil cooler |
|||||
|
9/5/10 |
P01 |
adjust valves, gap and install plugs, cut studs, install intake elbows, clean out intake tube, start fitting intake manifold |
3.00 |
||||
|
9/4/10 |
P01 |
refit left brake/wheel, fit brake cables, hang engine on mount |
3.00 |
||||
|
9/2/10 |
P01 |
install engine accessory adapter plate, install trigger shaft, alternator stator, test fit alternator mount plate/statr assembly |
1.00 |
||||
|
8/31/10 |
P01 |
install rear main seal, install flywheel, install oil cooler block off plate |
2.50 |
||||
|
8/30/10 |
P01 |
install prop lugs, fuel pump block off and breather plate |
1.00 |
||||
|
8/29/10 |
P01 |
Cut 4 pushrod tubes, install 2nd rocker arm, install oil screen and pump |
2.00 |
||||
|
8/23/10 |
P01 |
cut three studs on Lt. Side of engine and start fitting rocker shaft |
1.50 |
||||
|
8/19/10 |
P01 |
finish shimming and making pushrods for one side of engine and assemble |
1.00 |
||||
|
8/16/10 |
P01 |
emailed Kerry about shimming rocker shafts, he sent me new pages of assembly manual detailing rocker arm install and pushrods |
|||||
|
8/15/10 |
P01 |
cut head studs for rocke3r arm clearance one side |
1.50 |
||||
|
8/14/10 |
P01 |
install both cylinder heads |
3.00 |
||||
|
8/10/10 |
P01 |
gapped rings and re-install piston in #1 cylinder, locate and prepare heads, shims,gaskets, pushrod seals, washers and nuts, install shims and head gaskets |
1.50 |
||||
|
8/9/10 |
P01 |
received replacement cylinder, fit cylinder #2, set deck height, need to grind fin for clearance for case nut |
1.00 |
||||
|
8/5/10 |
P01 |
set deck height on Lt. Cylinders 3,4 |
1.00 |
||||
|
8/4/10 |
P01 |
resolved cylinder issue with Kerry, installed fittings on gascolator |
0.50 |
||||
|
8/3/10 |
P01 |
discovered pits in cyl #2, send email to Kerry, update website |
1.50 |
||||
|
8/2/10 |
P01 |
set up and measure deck height in cyl #1 |
1.00 |
||||
|
8/1/10 |
P14 |
Re-make battery top strap and rivet box to firewall, sand down bases of three cylinders to fit case |
4.00 |
||||
|
7/31/10 |
P14 |
drive to wick's for battery and bolts and misc, finish battery box, fit,drill,cleco, install contactor, cut and finish batt top strap |
4.50 |
||||
|
7/30/10 |
P14 |
locate, drill, and mount voltage regulator, locate, drill, and mount ign. Coils and gascolator, mark and cut battery box, shop online for fuel and oil fittings |
4.50 |
||||
|
7/27/30 |
oshkosh- last time staying at Waynes |
||||||
|
7/15/10 |
search fot throttle installations |
||||||
|
Study plans for firewall preparation |
0.50 |
||||||
|
7/10/10 |
fabricate, fit, dril and cleco brackets for xpdr which protrudes from panel 1/2 ", fit, drill, and cleco mounting plate for encoder bracket with room for AHRS unit in future |
3.00 |
|||||
|
7/6/10 |
read electrical schematics for xpdr and encoder hookups, consider changing mounting of xpdr for better fuel tank clearance |
2.50 |
|||||
|
6/29/10 |
G01 |
fit fuel tank to check clearance with xpdr- very very close, fit and pilot drill cross tie support for rear of xpdr |
1.00 |
||||
|
6/28/10 |
ordered replacement connector pins for rewiring connector for xpdr |
||||||
|
6/27/10 |
F07 |
cut panel hole for transponder, work on support for rear of xpdr |
2.00 |
||||
|
6/20/10 |
F07 |
fit and pilot drill lower panel cross tie, mark panel for instruments, cut 1st hole for stratomaster |
5.00 |
||||
|
6/15/10 |
F07 |
fit and pilot drill 3 panel mount angles, fit and pilot drill inst. Panel blank |
2.50 |
||||
|
6/14/10 |
F07 |
cut 2nd inst panel blank, mark and cut 3 panel mount angles |
2.00 |
||||
|
6/13/10 |
F07 |
cut 1st panel blank, deburr glareshield, fit and drill lower panel cross tie |
3.00 |
||||
|
6/8/10 |
F07-07 |
cut out panel suppot angles, clamp fit lower panel cross tie |
0.70 |
||||
|
6/7/10 |
F07-06RL,07RL |
clean shop, marked new panel support angles- remaking shapes for lowered panel, make replacement pieces for panel cross tie |
1.50 |
||||
|
5/25/10 |
Received replacement set of pistons |
||||||
|
5/13/10 |
Sonex rec'd pistons |
||||||
|
5/10/10 |
P01 |
sent piston set back to Sonex |
|||||
|
5/8/10 |
P01 |
work on installing 1st cylinder, chipped finish on bottom of jug |
2.50 |
||||
|
5/7/10 |
P01 |
ordered engine parts from Jegs and Wicks |
|||||
|
5/4/10 |
P01 |
mount engine block on stand, pull one jug, measure ring end gap- good |
0.50 |
||||
|
5/3/10 |
P01 |
bolt engine case together |
2.00 |
||||
|
5/1/10 |
P01 |
install crankshaft and cam into case |
0.50 |
||||
|
4/29/10 |
P01 |
installed connecting rods onto crankshaft |
1.00 |
||||
|
4/27/10 |
P01 |
assemble cam gear |
1.00 |
||||
|
4/26/10 |
start cleaning engine case |
1.50 |
|||||
|
4/25/10 |
F06 |
fit drill cleco glareshield, fit and mark inst panel |
3.00 |
||||
|
4/24/10 |
F07 |
cut firewall angles -09 center, -10 side (2), -08 tank stop angles, -05 crosstie, fit drill and cleco cross tie assembly, test fit tank straps |
5.00 |
||||
|
4/20/10 |
F07 |
cut glare shield |
0.70 |
||||
|
4/19/10 |
F07 |
mark glare shield |
0.30 |
||||
|
4/14/10 |
routed rt brake cable, pulled tape off engine case, updated website |
1.50 |
|||||
|
4/13/10 |
P01 |
clean, tape, and paint engine case |
1.50 |
||||
|
4/11/10 |
L02 L01-02 |
fit and install nose wheel, temp install mount, set fuse on gear, fit and mount 2/3 of seat belt bolts, install main gear brace thru bottom of fuse |
6.00 |
||||
|
4/10/10 |
L01 |
fit brake backing plates, work on fitting wheels and bearing races on main gear wheels |
10.00 |
||||
|
4/9/10 |
engine delivered |
||||||
|
4/7/10 |
L01 |
bend and drill out cable guide tubes R,L |
0.75 |
||||
|
4/3/10 |
C01 |
assemble and install control stick assembly |
4.50 |
||||
|
3/30/10 |
L01 |
mark and drill pilot holes for axles thru gear legs, 3rd tech inspection by Gale |
1.00 |
||||
|
3/29/10 |
L01 |
got v-block from wicks, drilled axles for cotter pins, drill fronts of axles for hole in leg |
0.50 |
||||
|
3/25/10 |
made wicks order for v-block, grommets for brake cables, c-sunk rivets for spar box, tap 10-32 holes in end of axles |
1.50 |
|||||
|
3/24/10 |
L01 |
update website (1.0), finish bolting gear mounts into fuselage, start working on method to set gear spindle height and toe-in |
3.50 |
||||
|
3/23/10 |
L04 |
finish rivetting fwd fuse bottom skin, start installing bolts on main gear mounts |
1.00 |
||||
|
3/22/10 |
L04 L01 |
finish drilling out gear leg bolt holse, drill out mount holes, start refitting mounts into fuselage, mailed check for balance of engine and prop |
2.50 |
||||
|
3/21/10 |
L01 |
drill pilot holes (upper) in gear legs, mount and start updrilling legs to 1/4 |
3.00 |
||||
|
3/20/10 |
L04 L01 |
cut holes in bottom skin for gear legs, drill holes for main gear mount strut braces, rivet bottom of cross tie box, study plans for leg installation |
5.00 |
||||
|
3/18/10 |
cleco bottom onto cross tie box |
||||||
|
3/17/10 |
sold goldwing to pay for engine, prop |
||||||
|
3/14/10 |
F15 |
make vent door latches, install vent doors, make nose gear boot, fit rt. Main gear |
3.00 |
||||
|
3/13/10 |
F02 F13 F15 |
run out of ccc-44 flush rivets, refit rudder pedals, rivet brake cable mount, set the 3 20470-AD5 rivets in top of spar tunnel, fabricate, fit, and cleco vent doors and latches, fit seat- 1st time to sit in plane! |
5.00 |
||||
|
3/10/10 |
F01 |
rivet more on spar tunnel and rt inside flush rivets |
1.50 |
||||
|
3/9/10 |
F01 |
drill holes for brake cable thru spar tunnel, cleco and start rivetting spar tunnel and aft vertical angles and gussets, mailed deposit and order for engine and prop |
2.50 |
||||
|
3/8/10 |
F16-04 F02 |
install rudder pedals- too tight, countersink 6 holes in upper support angle F16-04, file edges at rt. Side of tunnel spar box opening(dress the edges scarring from wing install and removal) |
1.50 |
||||
|
3/7/10 |
L01 F16-06,04 |
finish updrilling main gear mounts, disassemble aft tunnel web, counter sink, deburr, start rivetting pieces to web F16-06 vertical angles and F16-04 support angle |
4.00 |
||||
|
3/6/10 |
fly 407EV |
||||||
|
3/3/10 |
L01 |
start pilot drilling Rt. Main gear, update website |
2.50 |
||||
|
3/1/10 |
C08 L04 |
deburr, rivet aft seat hinge |
1.50 |
||||
|
2/28/10 |
C09 |
assemble flap drive tube, rivet rear spar carrythrough and forward seat hinge, work on brake pulley pivot link L05-11 (2 attempts), fit drill cleco flap and brake detent |
5.00 |
||||
|
2/25/10 |
C09 L04 |
cut bushing C09-05 for flap handle, drill flap handle for bolts and bushing, assemble flap handle, deburr hole for nosegear pushrod, start setting up L main gear mount, deburr forward seat hinge, clean shop |
3.00 |
||||
|
2/24/10 |
finsih drilling and bolt nosegear stop plate |
0.50 |
|||||
|
2/23/10 |
sand down inside of both bushings for fork tube clearance, grind down nosegear stop plate, fit and drill one side |
1.50 |
|||||
|
2/22/10 |
drill and tap and install set screws in nosegear bushings, drill nosegear forktube for drive horn |
2.00 |
|||||
|
2/21/10 |
rivet top edges of root doublers, fit nosegear into bushings, test fit into motor mount, remove wings and re-hang in garage, rearrange shop |
6.00 |
|||||
|
2/20/10 |
drill and countersink engine mount, deburr, sand down nosegear and engine mount for springs and bushing |
4.00 |
|||||
|
2/16/10 |
F02 |
cut and sand down wing root doublers LR |
2.00 |
||||
|
2/15/10 |
fit shims and level motor mount, drill top pilot holes LR, take pictures of mount holes and email Kerry to make sure holes are not too close to edge of the SS plate |
2.00 |
|||||
|
2/14/10 |
finish nose gear pushrod hole, test fit engine mount, mark lt and rt wing root doublers, update website |
4.00 |
|||||
|
2/13/10 |
F02 |
drill main wing bolts--yeah baby-- remove straps and clamps from fuselage, wings now fully fitted |
4.00 |
||||
|
2/10/10 |
F02 |
remove aft tunnel web and supports to prepare for starting to drill spars to foreward vertical support |
1.50 |
||||
|
2/9/10 |
F02 F03 |
rivet in rear spar carry through, re-check level and squareness and adjust, cleco carry through attach angles, update web site |
2.50 |
||||
|
2/8/10 |
F02 F03 |
prime, deburr, partially cleco carry through assy., fit drill deburr shear web to lower aft fuselage cross tie |
2.00 |
||||
|
2/7/10 |
F02 F03 |
build jig to hold wing trailing edges at correct incidence |
2.00 |
||||
|
2/6/10 |
F02 F03 |
make some 3/16 to 1/4 inch pins to align rear spar attach holes in carrythrough, start fitting shear web to carrythrough, fit carry thru to rear spar attach fittings |
5.00 |
||||
|
2/5/10 |
F02 F03 |
pin main spars together, set water level on wingtips, level fuselage, measure tail to wingtip length, strap down and secure fuselage to table |
4.00 |
||||
|
2/2/10 |
update web site |
1.50 |
|||||
|
2/1/10 |
F02 |
attempt to line ujp the 3 pilot holes in the main wing spars, found I had missed removing one cleco that was interfering with the root rib , removed cleco |
1.00 |
||||
|
1/31/10 |
F02 |
carry wings down into shop and fit into fuselage--exciting day for me! |
1.00 |
||||
|
1/30/10 |
move shelves in shop |
3.00 |
|||||
|
1/28/10 |
F03-06RL |
cut drill and finish R and L hand attach fittings, broke bandsaw blade |
2.00 |
||||
|
1/27/10 |
F03 |
finish pilot drill and cleco LR angle fittings on rear spar carry through |
2.00 |
||||
|
1/26/10 |
F02,F03 |
pilot drill and finish shear angle F03-08, rough cut spacer F03-04, cut 2 pieces from 1 1/2X1 1/2X3/16 angle, start working out steps for getting wings brought down into the shop for rigging, lay out pieces for rear spar carry through |
2.00 |
||||
|
1/25/10 |
F03-08 |
cut rear spar carry through shear angle from Z02-03 angle stock, review plans |
1.00 |
||||
|
1/24/10 |
strip paint from pushrod, assemble nose gear pushrod, clean shop, move fuselage onto worktable, move shelving against wall for clearance for fitting wings inside shop |
4.00 |
|||||
|
1/23/10 |
C02 |
fabricate rudder pedal pivot blocks, strip paint on pedals and fit pedals |
4.00 |
||||
|
1/21/10 |
make list of extra hardware needed for center controls, updrill center flap pivot block mount, un-cleco aft spar tunnel, pilot drill flap drive mount gusset (the 1 hole I couldn't reach from outside), deburr foreward spar tunnel inside and outside(seat hinge) and fuselage crosstie box(seat hinge holes) |
2.00 |
|||||
|
1/20/10 |
F15-05 |
fit center pivot block mount, gusset, pilot drill and cleco- there is 1 hole in gusset I can't reach from outside of spar tunnel |
1.50 |
||||
|
1/19/10 |
F15-05 |
remake 2 outer flap pivot phenolic blocks and drill center block, remove powder coating from flap drive, pilot drill outer blocks for attach bolts |
2.00 |
||||
|
1/18/10 |
work on fitting flap drive to pivot blocks- not happy with alignment of blocks, ordered phenolic, bolts, and al. sheet (for inst. Panel) from Wicks |
1.50 |
|||||
|
1/16/10 |
F15-15 |
drill flap drive mount bolt holes in mount phenolic blocks, update website |
2.00 |
||||
|
1/13/10 |
update website |
2.50 |
|||||
|
1/12/10 |
file out clearance hole in seat sling for control rod cover |
0.50 |
|||||
|
1/10/10 |
finish -02 seat assembly, fit, pilot drill, cleco seat sling into cockpit, need to adjust fit for slap/brake detent mounting and control rod cover |
6.00 |
|||||
|
1/9/10 |
work on seat sling and attach hinges |
2.50 |
|||||
|
1/6/10 |
C09-02,-03 |
study plans re: landing gear, make flap and brake handles |
1.50 |
||||
|
1/5/10 |
C09-19, -16 |
read drawing revisions, make 2 -19 brackets, finish 2nd bracket, rivet flap/brake detent |
2.00 |
||||
|
1/4/10 |
C09 |
finish flap detent bracket, cut and finish brake detent bracket |
2.00 |
||||
|
1/3/10 |
C06, C06-08,12 |
cut holes in seat skin, make 1st attempt at bending control rod cover, make 2nd copy of cover, rough cut and mark flap detent bracket |
5.00 |
||||
|
1/2/10 |
C07 |
rivet lowered seat details and idler arm assembly |
3.00 |
||||
|
1/1/10 |
C06, C07 |
deburr lowered seat details, fit, drill, deburr idle arm assembly |
3.00 |
||||
|
12/29/09 |
C07 |
re-make, fit, drill, and cleco LR support channels and gussets |
2.50 |
||||
|
12/28/09 |
C07 |
remove rivets on seat belt attach bracket on -02 assembly for clearance for drilling RL seat belt attach channel onto brackets, fit and start drilling LR support channels and center support channel |
2.00 |
||||
|
12/27/09 |
C07 |
construct C07-02 cap assembly, fit, drill, cleco assembly. F24 gussets and spacers, fit,drill, cleco cap ssembly, partial deburr |
5.00 |
||||
|
12/26/09 |
F10, C03-06 |
make F10-05-08-11 clips (6 pieces), cut seat sling to size, mark cut outs for control sticks |
3.00 |
||||
|
12/25/09 |
F10-16 |
finish boring bushings for idler assembly |
1.00 |
||||
|
12/24/09 |
F10-06,16 |
cut pieces for idler assembly F10-16, make hook mount F10-06 |
4.00 |
||||
|
12/22/09 |
C06-06, F10 |
finish rivetting and drilling cap assembly, clean shop, study plans, make brackets for seat belt attach- F10-05RL |
1.50 |
||||
|
12/21/09 |
F10, C07 |
cut C06-07 angle from 1X1X1/8 angle, pilot drill, fit, snd finish drill hinge half, Carly and Jason rivetted upper firewall |
1.00 |
||||
|
12/20/09 |
F11 |
fit and rivet forward tunnel zee, fit, cleco aft tunnel support and gussets |
5.00 |
||||
|
12/19/09 |
F10, C06 |
make C06-05 angle, F10-10RL, 12, 13RL, C06=-4 rear spar carry throuth channel |
3.00 |
||||
|
12/16/09 |
F10, C06 |
fit, drill, install pushrod supports, rough mark all pieces from Z02-04 channel, cut C06-12,13 , rough cut C06-05 angle |
2.00 |
||||
|
12/15/09 |
F11 |
remove aft fuselage elevater pushrod supports |
1.50 |
||||
|
12/14/09 |
F11 |
start fitting forward tunnel zee, flatten dimples made with simple dimple die, review plans for lowered seat option |
1.00 |
||||
|
12/13/09 |
F11 |
assemble and rivet fwd fuselage assembly |
4.00 |
||||
|
12/12/09 |
F11, P13-08RL |
fit and drill lower firewall hinges (fo rcowling attach) |
4.00 |
||||
|
12/9/09 |
F11 |
deburr fwd fuselage |
1.50 |
||||
|
12/8/09 |
F11 |
deburr fwd fuselage details, counter sink and dimple, review plans for starting lower seat/center controls |
3.00 |
||||
|
12/7/09 |
F11 |
disassemble fwd fuselage, start deburring |
1.00 |
||||
|
12/6/09 |
F11 |
fit and pilot drill upper firewall, up drill complete fwd fuse assy for fasteners |
2.00 |
||||
|
12/5/09 |
F11 |
fit,pilot drill, cleco floor and firewall stiffeners and gusset and clip, start up drilling fwd fuselage |
4.00 |
||||
|
12/3/09 |
F11 |
locate and pilot drill aft tunnel web to aft wing support angles, clean work area |
1.50 |
||||
|
12/2/09 |
F11 |
finish drilling forward tunnel zee to wing attach angles, pre-fit aft tunnel web assy |
1.00 |
||||
|
12/1/09 |
F11 |
drill and cleco upper and lower lonngeron splice plates, fit and drill forward tunnel zee to floor, removed Land R aft wing attach angle to access inner tunnel zee, pilot drill holes for forward wing attach angle |
2.50 |
||||
|
11/30/09 |
F11 |
locate, drill, and cleco lower firewall, turn fuse right side up |
1.00 |
||||
|
11/29/09 |
F11 |
pilot drill upper and lower cross ties, fit firewall |
1.00 |
||||
|
11/24/09 |
F11 |
pilot drill lower cockpit skin to longerons |
0.40 |
||||
|
11/23/09 |
F11 |
pilot drill and cleco fwd fuselage onto aft fuselage, turn over assy, cleco bottom skin, drill out and re-rivet F24-09 lower crosstie- had been installed backwards, pilot drill lower skin to crosstie, added lower shelf to work table |
2.50 |
||||
|
11/22/09 |
F12-01L |
bolt and rivet Lt side panel assy |
2.00 |
||||
|
11/19/09 |
F12-01L |
deburr skin and all angles, reassemble, flip over, and pilot drill firewall clips and doubler |
3.00 |
||||
|
11/18/09 |
F12 |
complete Lt panel drilling thru step 22, ready to pull off table and fit doubler and firewall clips |
2.00 |
||||
|
11/17/09 |
F12 |
locate and pilot drill angles onto Lt fuse side panel |
1.50 |
||||
|
11/16/09 |
F13-02L |
cut slots in Lt fwd longeron and phenolic sheets, drill and c/sink for holes in phenolic |
2.00 |
||||
|
11/15/09 |
F13-02RL |
cut oblong holes in both new upper longeron pieces, re-rivet Rt longeron to panel |
2.50 |
||||
|
11/14/09 |
F13-02R |
remove and slice upper longeron from Rt side panel, drilled holes into new angle |
1.00 |
||||
|
11/12/09 |
F13-02RL |
realized I had mis-drilled obling holes for canopy bow, ordere 2 new angles from wicks |
0.30 |
||||
|
11/11/09 |
F13-02L |
realized I had screwed up slots in Lt upper longeron, ordered new angle from wicks |
0.30 |
||||
|
11/10/09 |
F12 |
install bolts for engine mount, rudder pedal mt, and seat belt mt, cut naca vent into Lt fuse side panel |
2.00 |
||||
|
11/9/09 |
F12-01R |
rivet fwd fuse cockpit side wall |
1.50 |
||||
|
11/7/09 |
F12 |
up drill fuse side panel, cut out naca vent, deburr and cleco F12-01R |
3.50 |
||||
|
11/6/09 |
F14-05,06 F15-06 |
fit and drill firewall attach angles and doubler |
0.80 |
||||
|
11/4/09 |
F12 |
pilot drill flap drive mount and seat belt clip, redrill upper motor mount with .032 space, jremake 063 angle on rudder pedal mount and pilot drill |
2.00 |
||||
|
11/3/09 |
F12 |
pilot drill Rt forwar side panel gussets, motor mounts, anfle, draw cutout for vent |
2.70 |
||||
|
11/2/09 |
F12 |
pilot drill upper and lower longerons, forward angle, rudder pedal support, for and aft attach angles, horizontal angles, gear support angles |
2.00 |
||||
|
11/1/09 |
F13-03RL |
cut oblong holes and slots in upper longerons- found out later they w3ere wrong, c/sink and rivet upper ongerons doublers, lay out some pieces on Rt forward side panel |
3.00 |
||||
|
10/31/09 |
F16-03, F13-03 |
finish dimpling and counter sinking aft tunnel web assy, cut upper longerons and start drilling |
1.00 |
||||
|
10/27/09 |
F17, F16-03 |
dimple and rivet upper firewall assembly, updrill aft tunnel web assy. |
2.50 |
||||
|
10/26/09 |
F17 |
rivet filler box assy, fit windshield strap to upper firewall |
2.50 |
||||
|
10/25/09 |
F14-06RL |
finish lower longerons, order new 1 in angle |
1.50 |
||||
|
10/24/09 |
F14-09RL |
mark, cut, file, drill and finish aft wing attach angles |
2.50 |
||||
|
10/22/09 |
F14-01RL, F14-09RL |
assemble 02,03,04 to make o1 RL assemblies, open up angles to 94 using hydraulic press at work |
2.00 |
||||
|
10/21/09 |
F14-03,04RL |
make cowling attach hinge and firewall attach angles |
1.50 |
||||
|
10/20/09 |
F14-04,05,06RL |
mark and cut fwd fuselage angles, upper and lower firewall attach angles |
2.00 |
||||
|
10/19/09 |
F14-13RL |
cut, file, drill, finish horizontal angles |
1.50 |
||||
|
10/18/09 |
F14 |
pilot drill gear attach angles, cut, file,drill rudder attach angles, mark,cut, filt,drill fuselage forward angles |
3.00 |
||||
|
10/8/09 |
F14-11RL |
cut gear attach angles |
0.50 |
||||
|
10/7/09 |
F14-08RL,12RL |
finished forward wing attach angles, makr for drilling, finish seat belt attach angles |
2.50 |
||||
|
10/6/09 |
F14-08,12RL |
cut one piece and finish, cut second wing attach angle, work on bending to 94, these didn't work either |
2.50 |
||||
|
10/5/09 |
F14-08,09 |
adjust pieces to 86 degrees, mark for cutting, tried working on 94 degree pieces- didn't work |
1.50 |
||||
|
10/1/09 |
F15-12, F14-02,03 |
rough cut other seat belt attach angle, lay out all 1 in angle and cut up according to cutting list in manual- F14-02RL, 07RL,11RL,F13-03RL |
1.50 |
||||
|
9/30/09 |
F15 |
make spacers F15-08, mark seat belt attach angles, rough cut one angle |
1.50 |
||||
|
9/29/09 |
F15 |
dinish rudder pedal support assemglies |
2.00 |
||||
|
9/28/09 |
F16-01,02,07RL |
finish upper and lower motor mounts, and flap drive mounts, cut rudder pedal support angle and start bending |
3.00 |
||||
|
9/27/09 |
F15 |
mark and cut lower motor mounts RL and flap drive mounts RL |
2.00 |
||||
|
9/24/09 |
F15-01,04RL, F16-01 |
finish rudder pedal mount angles, mark pieces and drill holes for upper motor mounts |
2.00 |
||||
|
9/23/09 |
F15-12RL, 04RL |
make angle clips, mark and drill rudder pedal mounts |
2.50 |
||||
|
9/22/09 |
T16-02,03 |
finish cutting and drilling forward tunnel zee, fit/drill aft tunnel web assy, ready to dimple and c/sink, read ahead in plans pages |
3.25 |
||||
|
9/21/09 |
F16-05,02 |
make aft tunnel angle and start on forward tunnel zee |
2.50 |
||||
|
9/19/09 |
F16, F17 |
set up table saw to rip down horizontal angle, make upper and lower forward crosstie and support angle make rt and lt vertical angles and floor and firewall stiffeners |
5.50 |
||||
|
9/18/09 |
F17 |
finish drilling for southco fasteners |
1.00 |
||||
|
9/17/09 |
F17 |
re-work flutes on upper firewall and start fitting southco fasteners |
1.00 |
||||
|
9/16/09 |
F17 |
jig up and start drill windshield bow to firewall |
1.00 |
||||
|
9/15/09 |
F17 |
finish F17-11 gusset, make upper clips, aft clip, fit/drill filler box to firewall F17-03 and fit bottom and top double |
3.00 |
||||
|
9/9/09 |
cut 12 ft worktable down to 6 ft |
1.50 |
|||||
|
8/29/09 |
F18 |
finish rivetting turtle deck and tailcone box, bolt and torque upper vertical splices |
4.00 |
||||
|
8/27/09 |
F21 |
rivet lower #1 crosstie, rivet crosstie box, bolt and torque upper horizontal splices |
1.00 |
||||
|
8/26/09 |
F21 |
finish rivetting tail cone box, rivet turtle deck formers 5,4,3,2 and splice channel, fit crosstie box and lower crosstie 1 |
1.50 |
||||
|
8/25/09 |
F21 |
start rivetting tail cone box |
2.00 |
||||
|
8/24/09 |
F21 |
finish deburring aft fuse box details, start re-assembling for rivetting |
2.00 |
||||
|
8/23/09 |
F23-09,11 |
fit fore and aft pushrod supports, deburr aft fuselage box horiz. Channels |
4.00 |
||||
|
8/22/09 |
F20-03RL, F20-02RL |
drill former 3RL, fit/drill former 2 RL, updrill turtle deck to formers 1-5, deburr aft fuse floor and turtle deck skins RL |
5.00 |
||||
|
8/20/09 |
F20-03RL |
file down seat belt brackets to help fit former 3 |
1.00 |
||||
|
8/19/09 |
F20-03, F20-04 |
fit/drill former 4 LR, start to fit former 3, interferes with seat belt mount |
1.00 |
||||
|
8/18/09 |
F19 |
fit and pilot drill former 1 Lt and Rt, fit and drill splice plate for former 1, fit/drill attach plates to former 1, fit/drill forward clip to former 1 |
2.00 |
||||
|
8/17/09 |
F19, F20-05 |
pilot drill turtle deck skin, pilot drill former 5 |
2.50 |
||||
|
8/13/09 |
F19 |
rivet clips onto splice channel, start pg F19- turtle deck installation, fit turtle deck onto aft fuse box for first time |
1.50 |
||||
|
8/12/09 |
F20 |
finish drilling lower horizontasl splice plate on Rt, drill clips for crosstie box |
1.00 |
||||
|
8/11/09 |
F20-07,10 |
drilled clips onto turtledeck splce channel |
0.25 |
||||
|
8/10/09 |
F20-07 |
make splice plate for skin splice channel piece- recut channel and pilot drill to Rt turtle deck skin (cut channel backwards) |
1.50 |
||||
|
8/5/09 |
F21, F23-05, F24-01 |
re-fit and drill cross tie box, fit and drill seat belt brackets |
2.00 |
||||
|
8/4/09 |
F21, F22-02,F24-01 |
fit and drill shear web and cross tie box |
1.50 |
||||
|
8/3/09 |
F21 |
start fitting splice plates, fit aft shear web assy. Into place |
1.00 |
||||
|
8/2/09 |
F21 |
fit spring mount, aft lower angle, forward lower angle and bulkhead, drill aft upper angle |
2.50 |
||||
|
8/1/09 |
F21-02 |
fit, pilot drill and up drill upper aft cross ties, up drill lower aft cross ties, file out clearance for tail main spar to upper longerons, review plans |
3.00 |
||||
|
7/31/09 |
F21 |
set up, fit and pilot frill aft lower cross ties and bottom skin |
3.00 |
||||
|
Oshkosh Break |
|||||||
|
7/22/09 |
F21-02 |
found tail spring mount and made spacer, fitted and drilled tail spring mount to aft channel and vertical fin main spar |
1.50 |
||||
|
7/21/09 |
search through workshop for F23-01 tail spring mount- didn’t find it - crap! |
1.50 |
|||||
|
7/20/09 |
widen table at one end and set up aft fuselage sides onto table |
2.00 |
|||||
|
7/16/09 |
F24-02,3,4 |
cut out upper cross ties 2,3,and 4 |
0.75 |
||||
|
7/15/09 |
F25-01R |
assemble and rivet Rt aft side panel |
1.00 |
||||
|
7/14/09 |
F25-01L |
finish rivetting Lt aft side panel assy. |
0.30 |
||||
|
7/13/09 |
F23-03,06, F24-01 |
rivet rear shear web and seat belt webs, start rivetting Lt aft skin, rivet fairlead assys. To vertical channels |
1.50 |
||||
|
7/7/09 |
F19, F21 |
read plans |
0.50 |
||||
|
7/6/09 |
F20-11,12 |
cut and drill forward and aft clip |
0.40 |
||||
|
7/5/09 |
F20-06,-07-10 |
cut clips and pieces |
1.40 |
||||
|
6/16/09 |
F22-05, F22-04, F22-02, F22-06 |
finish aft angle, cust and finish 04 angle, updrill aft shear web assy., cut/finish forward angle |
2.00 |
||||
|
6/15/09 |
F23-02 |
make 2 F23-12 clips, drill 1 1/2 hole in aft angle |
0.60 |
||||
|
6/14/09 |
F23-02,9,11 |
drill holes for pushrod support, start/finish bulkhead |
1.00 |
||||
|
6/13/09 |
F23-05RL |
drill L and R seat belt mount angles |
0.30 |
||||
|
6/10/09 |
F23-04 |
meark, cut, and finish aft lower mount angle |
1.00 |
||||
|
6/8/09 |
F23-03 |
cut and finish lforward lower mount angle |
1.00 |
||||
|
5/30/09 |
F24-01 |
finish drilling cross tie box, dissasemble and deburr |
1.00 |
||||
|
5/29/09 |
F24-01 |
flip over cross tie box and clamp down for drilling bottom |
0.50 |
||||
|
5/28/09 |
F24-10,11,12,13 F24-01 |
set up cross-tie box and drill top side to channel F11-12 |
1.00 |
||||
|
5/27/09 |
F24-11,12 |
cut forward and aft cross tie box channel pieces, drill extra holes in lower cross tie box skin |
1.50 |
||||
|
5/26/09 |
F24-07,6,5 |
cut and finish lower cross ties 1,2,3 |
1.50 |
||||
|
5/19/09 |
F24-09,08 |
finish cut , cut and pilot drill #4 and 5 lower cross tie and finish |
1.25 |
||||
|
5/18/09 |
F24-09,8,7,6 |
rough cut lower cross ties from stock |
0.50 |
||||
|
5/17/09 |
F25-01R,L F24 |
updrill skin-longerons and vertical pieces, ready to deburr and rivet, search online for larger bushings and order from Wicks, deburr longerons, brackets, and vertical pieces, lay out angle stock for F24 |
2.50 |
||||
|
5/14/09 |
F25-01R F26-02R, 03R F26-08 |
fit and pilot drill 07,06,05,04R splice plates onto longerons |
0.75 |
||||
|
5/13/09 |
F25-01R F26-02R, 03R F26-08 |
fit and pilot drill upper and lower longerons to skin, fit rudder stop plate |
1.50 |
||||
|
5/12/09 |
F26-06L, 07L |
fit and pilot drill horiz and vertical lower splice plates |
1.00 |
||||
|
5/11/09 |
F26-05L, 04L F26-08L |
fit upper horizontal and upper vertical splice plates and pilot drill, fit and pilot drill rudder stop plate |
0.75 |
||||
|
5/7/09 |
clean downstairs, vacuum basement incl shop |
||||||
|
5/6/09 |
F25 F26-01L |
fit vertical cahhels to skin, fit fairlead assemblies |
1.50 |
||||
|
5/5/09 |
F25-01 F26-01 |
Drill skin to upper and lower longerons |
1.50 |
||||
|
5/2/09 |
F26-01 RL F26-02,03RL |
mark aft side skins for rudder cable hole and 4" access holes, cut cable slots L,R, finish angles on fronts of longerons F26-03,02RL , drill 4" access holes in side skins and bend 14 degree bend on forward edge of side skins |
3.00 |
||||
|
4/30/09 |
F26-06,05 F26-04 F26-03,02 |
bend and chanfer 06 and 05 splice plates, chamfer 04 plate, cut upper and lower longerons to length |
1.00 |
||||
|
4/29/09 |
F27-01RL F26-08 F27-07 |
finish vertical pieces 01RL for aft fuselage sides, make stop plates, bend lower splce plates and finish |
1.00 |
||||
|
4/28/09 |
F27-02,3,4 R,L F27-01R,L |
finish 6 vertical pieces, mark and pilot drill and mark notches for F27-01RL |
2.50 |
||||
|
4/27/09 |
F27-02,03,04 |
notch all 6 vertical pieces, make templates for details A,B pilot drill lower ends, detail B |
1.50 |
||||
|
4/25/09 |
F27-01RL |
cut to finished size |
0.50 |
||||
|
4/24/09 |
F27-04RL , F27-03RL, F27-02RL |
cut all F27-02,03,04 cut all pieces to finished length |
1.50 |
||||
|
4/23/09 |
F27-10 |
study plans, find Z03-04 channel |
0.50 |
||||
|
4/22/09 |
F27-10 F27-05L,R |
finish fairlead assemblies, mark and cut F27-05LR and finish pieces |
0.75 |
||||
|
4/21/09 |
F27-10 |
buy forstner bits, drilled 3/4 holes in fairlead blocks, finished one F27-09 assy. |
0.90 |
||||
|
4/20/09 |
F27-10 |
cut out finished mount blocks (4) and pilot drill for holes |
|||||
|
4/16/09 |
W02-01L |
finish fitting wing tip and light base |
0.30 |
||||
|
4/15/09 |
W02-01L |
start fitting wing tip |
1.00 |
||||
|
4/14/09 |
W02-01L |
vacuum out rivets from wing interior, clean, re-rivet skins- wing is closed up! |
1.00 |
||||
|
4/13/09 |
W02-01L |
drill out approx. 160 rivets on upper spar cap and 3 rows on LE and TE skins |
2.50 |
||||
|
4/12/09 |
W02-01L |
flip wing, level, cleco , rivet lower aft skin, slip wing, rivet upper aft and LE skin, discovered I had overlapped aft skin over LE skin on top of wing |
2.00 |
||||
|
4/11/09 |
W02-01L |
final torque Rt. Bellcrank, deburr Rt forward root rib, deburr Rt. Flap hinge, rivet rt. Hinge and rt. Lower aft skin |
5.00 |
||||
|
4/9/09 |
W02-01L |
finish deburring aft ribs, drive, drill out and redo 2 solid rivets to ribs 1 and 2, cleco upper aft skin |
2.00 |
||||
|
4/7/09 |
W23-01L W02-01L W18-01L |
finish dimpling lower LE skin, install nutplates for AOA mount, finish devvurring all parts for wing skins |
1.50 |
||||
|
4/6/09 |
W02-01L |
dimple upper LE skin |
0.50 |
||||
|
4/5/09 |
W02-01L |
updrill, deburr LE ribs, deburr spar cap, rear spar, inside upper edge aft ribs, install 2 solid rivets in ribs |
5.00 |
||||
|
4/1/09 |
W02-01L W23-07L W23-05L |
fit, drill, deburr tubing support brackets for AOA ribs 1-4, fit and drill AOA mount plate, deburr lower inner LE skin at spar cap, devurr lower outer spar cap |
1.50 |
||||
|
3/31/09 |
W02-01L W07-01L W19-02L |
devurr aft lower skin complete, drill tie-down bracket hole |
1.50 |
||||
|
3/30/09 |
W05-02L W02-01L |
fit and drill hinge for flap, deburred and fit to updrill |
1.50 |
||||
|
3/29/09 |
W17-01L |
deburr upper aft skin and wing walk, flip wing, drill root ribs to skin |
2.00 |
||||
|
3/28/09 |
W07-01L W20-02L W20-03L |
fit, drill, deburr root ribs, mark lower forward skin for location of AOA |
2.50 |
||||
|
3/26/09 |
Flew N407EV |
||||||
|
3/25/09 |
W07-01L |
start pilot drilling aft root rib |
|||||
|
3/24/09 |
W07-01L |
removed upper aft skin, mark lower aft skin for tie-down hole, fit and finall drill bellcrank support holes in lower aft skin, clean work area |
1.50 |
||||
|
3/23/09 |
W07-01L |
fit aileron hinge and pilot drill, test fit aileron |
1.50 |
||||
|
3/22/09 |
W19-02L W19-01L W06-06L |
updrill lower aft skin and spar cap, drill bellcrank support to upper skin, cut hinge for flap, flip wing over to top, start drilling aileron hinge, updrill upper skins to sparcap |
4.00 |
||||
|
3/18/09 |
W02-01L |
updrill wing walk area on top, flip wing over to bottom |
0.50 |
||||
|
3/17/09 |
W02-01L |
finish pilot drilling upper LE skin-rib, up drill aft upper skin-rib except doubler, clean up work area |
2.00 |
||||
|
3/15/09 |
W02-01L W18-01L |
finish drilling lower LE skin to ribs, flip over wing to top |
1.50 |
||||
|
3/12/09 |
W02-01L |
finish drilling lower aft skin to main spar cap |
0.40 |
||||
|
3/11/09 |
W02-01L W19-02L |
continue drilling lower skin to main spar cap |
1.30 |
||||
|
3/10/09 |
W02-01L W19-02L |
drill lower aft skin to ribs, rear spar, start main spar cap drilling |
2.00 |
||||
|
3/9/09 |
W02-01L W07-01L W19-02L |
flip wing, level, align, start pilot drilling lower skin to ribs |
1.00 |
||||
|
3/8/09 |
W19-01L |
start drilling spar cap for upper aft skin and finish upper aft |
1.50 |
||||
|
3/7/09 |
W19-01L |
drill upper aft skin |
1.00 |
||||
|
2/19/09 |
W02-01L W19-01L |
pilot drill upper aft skin |
1.00 |
||||
|
2/18/09 |
W02-01L |
levela nd square wing, clamp upper aft skin |
1.00 |
||||
|
2/17/09 |
W12-01L W13-01L W02-01L |
deburr and rivet rear spar onto ribs, level wing on bench to prep for pilot drilling upper aft skin to ribs |
1.50 |
||||
|
2/16/09 |
W21-10L W13-01L W02-01L |
rivet bell crank assy to rib #9, fit rear spar |
1.50 |
||||
|
2/15/09 |
W05-05L W02-01L |
rivet ribs to main spar ribs 1-12 |
2.00 |
||||
|
2/12/09 |
grind down riveter for angle |
0.50 |
|||||
|
2/10/09 |
W05-05L W02-01L |
deburr, drill hole for wiring, flatten and mark centerline for ribs 8-12, clecoed to spar for rivetting |
1.00 |
||||
|
2/9/09 |
W05-05L W02-01L |
deburr holes in ribs for spar, drill holes for wiring, flatten ribs and mark centerline for ribs 1-7, final clecoed ribs to spar |
1.50 |
||||
|
2/4/09 |
W01-01L |
dit and drill ribs onto main spar |
1.00 |
||||
|
1/31/09 |
W14-02L W08-01L |
drill center spacers onto main spar |
1.00 |
||||
|
1/22/09 |
W04-01L |
Lt aileron assy.- deburr all pieces, primer contact surfaces, cleco and rivet assembly |
2.00 |
||||
|
1/21/09 |
W06-01L |
finish deburring ribs, skin, hinge, primer mating surfaces, finish rivetting |
1.50 |
||||
|
1/20/09 |
W06-01R W06-01L |
rivetted rt flap assy. Deburr left skins, ribs |
1.75 |
||||
|
1/19/09 |
W06-01R |
paint ribs and skin mating surfaces |
0.20 |
||||
|
1/18/09 |
W06-01R |
deburr skin, hinge, ribs |
1.00 |
||||
|
1/15/09 |
W06-01R |
finish updrilling |
1.00 |
||||
|
1/14/09 |
W06-01R |
finish pilot drilling hinge and deburr for final drilling |
1.00 |
||||
|
1/13/09 |
W06-01L W06-01R |
finish updrilling ribs and hinge, ready to deburr and rivet, started pilot drilling rt hinge |
1.50 |
||||
|
1/12/09 |
W05 W05-01L W06-06L |
finish pilot drilling hinge, start cleaning up pieces for final drilling |
1.00 |
||||
|
1/11/09 |
W06-01L W06-06L,R W05-01L |
pilot drill ribs bottom, drill 1" holes in flap hinges, started pilot drilling hinges to flap |
1.50 |
||||
|
1/9/09 |
W06-01R WO5 |
pilot drill ribs on top and LE |
0.30 |
||||
|
1/8/09 |
W06-01R WO5 |
pilot drill flap ribs on LE and bottom |
1.00 |
||||
|
1/7/09 |
W06-01R,L W05-01R,L |
mark holes for ribs in skins, drill skins for ribs |
1.00 |
||||
|
1/5/09 |
W06-01R,L W05-01R,L |
file and sand edges of flap skins mark centerlines for rib holes |
1.00 |
||||
|
1/4/09 |
W06-05R,L W06-01R |
drill up drive ribs rt.and lt. start cutting skings |
2.00 |
||||
|
1/3/09 |
W04-01L W04-03 W03-03 W03-01L |
updrill all ribs and hinge for aileron, tip rib, center rib, counter balance assy. |
2.50 |
||||
|
1/2/09 |
W03-01L W04-01L W04-03 W04-05 |
Clean work area, drill hinge onto L aileron, drill bottom and aft of drive ribs and center rib |
2.50 |
||||
|
12/29/08 |
paint wingtip light fairings |
0.40 |
|||||
|
12/27/08 |
update website and time worksheet |
2.50 |
|||||
|
12/25/08 |
W02-01R |
finish closing rt wing |
0.50 |
||||
|
12/24/08 |
W02-01R |
rivetting upper skins |
0.50 |
||||
|
12/22/08 |
W02-01R |
set up and cleco upper aft skin, start closing up wing |
2.00 |
||||
|
12/21/08 |
W07 |
test fit control pushrods for aileron, install wiring and tygon tubing |
1.00 |
||||
|
12/20/08 |
W07 |
torque tie-down bracket, install tie-down bolt, install power supply on rt wing, sort through wicks hardware |
2.00 |
||||
|
12/17/08 |
second inspection by tech counselor before closing up rt wing |
||||||
|
12/15/08 |
W04-01L |
drill lt aileron skin for rib locations |
1.00 |
||||
|
12/14/08 |
clean shop |
1.00 |
|||||
|
12/8/08 |
W04-05L W03-03L W04-01L |
rivet lt aileron drive rib, rivet counterweight rib assy, start drilling skin |
1.00 |
||||
|
12/4/08 |
W03-01R,L |
grind bolt head for aileron counterweight clearance with rib, prep and prime aileron ribs, started marking lt aileron skin for ribs, clean work area, touch up body putty on light fairings |
2.00 |
||||
|
11/29/08 |
W02-01R W03-01R |
Flew N407EV!, flipped wing over with some help, fit aileron on hinge |
1.00 |
||||
|
11/27/08 |
W02-01R W03-01R |
rivet lower leading edge skin, install counterweight |
1.00 |
||||
|
11/25/08 |
W03-01R |
rivet aileron assy together |
1.00 |
||||
|
11/24/08 |
W04-05R W03-03 W04-01R |
rivet drive rib, rivet counter balance assy, and deburr rt aileron wing skin |
1.50 |
||||
|
11/22/08 |
make fairing, laid up forms, sand and drill finished fairing |
3.00 |
|||||
|
11/21/08 |
make sculpamold molds from body-filled fairing forms |
1.00 |
|||||
|
11/20/08 |
put body filler on fairings- 4 coats |
3.00 |
|||||
|
11/18/08 |
W03-01R |
deburr rt aileron parts, cut, fit and pilot drill rt tip |
2.00 |
||||
|
11/17/08 |
W02-01R,L |
lay up fiberglass in forms for light fairings |
1.50 |
||||
|
11/16/08 |
W03-01R,L |
break out fiberglass from fairing forms, still not dry |
0.20 |
||||
|
11/15/08 |
W03-01R |
fiberglass light fairing forms, drill rt aileron tip, updrill entire rt aileron |
2.50 |
||||
|
11/12/08 |
W03-01R |
drill ribs for rt aileron |
1.50 |
||||
|
11/11/08 |
W03-01R |
cut 2X4 rib shape to drill and punch skins, mark ribs centerlines |
0.50 |
||||
|
11/10/08 |
W03-01 |
mark upper aileron skin for ribs, found I had drilled lower skin with upper skin hole spacing |
0.50 |
||||
|
11/9/08 |
W03-01 |
up drill hinge, drill skin for ribs |
0.50 |
||||
|
11/8/08 |
W03-01 |
drill hinge for rt aileron, start drilling skin for rib locations |
1.50 |
||||
|
11/8/08 |
drive to Wicks for supplies |
3.50 |
|||||
|
11/4/08 |
W03-01L |
file and fit aileron skin, |
0.50 |
||||
|
11/3/08 |
W03-01L |
assemble, drill, deburr lt counterweight assy |
1.00 |
||||
|
10/29/08 |
W03-01R |
assemble and up drill counterweight rib assy. |
1.00 |
||||
|
10/28/08 |
W03-01L,R |
finish aileron skins, mark and drill counterweight ribs |
1.00 |
||||
|
10/27/08 |
W04-01L,R |
cut, file aileron skins |
1.00 |
||||
|
10/26/08 |
W04-01R |
cutting aileron skins |
0.50 |
||||
|
10/25/08 |
W04-05L,R W04-04 W04-11,12 W04-06L,R W04-01L,R |
fit, drill, deburr drive plate, measure drill deburr channel, drill aileron hinges, mark both aileron skins, start cutting |
4.00 |
||||
|
10/22/08 |
W19-01 W18-01R |
cleco rt aft wing skin |
0.50 |
||||
|
10/21/08 |
W19-02R |
rivet rt forward root rib, finish rivet rt lower aft skin, turn wing over to upper side |
1.00 |
||||
|
10/20/08 |
W21-10 W17-01R W06-06R W19-02 |
final torque Rt. Bellcrank, deburr Rt forward root rib, deburr Rt. Flap hinge, rivet rt. Hinge and rt. Lower aft skin |
2.50 |
||||
|
10/19/08 |
W18-02 W23-01 |
Clean workbench,, drill skin for inspection cover |
0.50 |
||||
|
10/10/08 |
W18-01R W23-01 |
Dimple upper and lower Rt. LE skin, rivet nutplates for P/S |
1.50 |
||||
|
10/9/08 |
W18-01R |
Deburr LE skin |
1.50 |
||||
|
10/8/08 |
W18-02 W18-01R W23-01 |
Dimple all Rt. Wing ribs, fit nutplates and drill pitot/static, drill hole for p/s in wing skin |
2.00 |
||||
|
10/7/08 |
W23-01 |
Deburr Rt. Wing ribs, start to fit pitot/static |
1.50 |
||||
|
10/6/08 |
W08-01R W14-01R |
Deburr Rt. Wing ribs and spars |
2.50 |
||||
|
10/5/08 |
Make new storage area for all wing skins, start deburring rear spar |
1.00 |
|||||
|
10/2/08 |
W19-02R |
Finish deburring Rt. Aft lower skin |
1.50 |
||||
|
9/30/08 |
W20-01R |
Fit and drill RH Root doubler on lower skin and start to deburr lower aft skin |
1.50 |
||||
|
9/29/08 |
NA |
FAA seminar on take offs and landings |
2.00 |
||||
|
9/25/08 |
W18-01R W23-05 |
Finish drill bottom forward sking to new ribs 6 and 8, cut out W23-05 for pitot and static and mark onto forward skin |
1.50 |
||||
|
9/23/08 |
W15-05 |
Drill Rt. Forward replacement ribs 6 and 8 to top skin |
0.50 |
||||
|
9/17/08 |
W15-05 |
Remove #8R forward rib, refit and cleco replacement rib |
0.50 |
||||
|
9/16/08 |
Clean and rearrange shop after basement work |
2.00 |
|||||
|
8/16/08 |
W15-05 |
Remove #6R forward rib, refit replacement, drill and cleco |
1.00 |
||||
|
Stop work on plane to finish out basement room |
|||||||
|
8/7/08 |
W19-01R |
Deburr upper aft. skin |
1.00 |
||||
|
8/6/08 |
W19-01R |
Deburr upper aft. skin |
|||||
|
8/2/08 |
W18-01R |
Vacuum form rt. LE |
|||||
|
7/29/08 |
W18-01R |
Clean up shop after doing finishing work on basement family room, running out of room in shop!, hang left LE in shop ceiling, set up to vaccum form rt. LE |
|||||
|
6/16/08 |
W18-01R |
Drill upper rt LE skin |
0.50 |
||||
|
6/11/08 |
W18-01R |
Drill rt upper LE and top of spar to LE |
2.00 |
||||
|
6/10/08 |
W18-01R |
Flip rt wing and set straps to fit LE |
1.50 |
||||
|
6/2/08 |
W19-01R W18-01R |
Drill up lower rt aft skin, start attaching LE skin (lower) |
1.50 |
||||
|
5/30/08 |
W19-02R |
Drill Rt wing skin lower |
1.00 |
||||
|
5/27/08 |
W19-02R |
Drill Rt wing skin lower |
1.00 |
||||
|
5/26/08 |
W19-01R |
Drill Rt wing skin upper |
2.00 |
||||
|
5/25/08 |
W19-01R |
Drill Rt wing skin upper |
1.00 |
||||
|
5/24/08 |
W16-01R W12-01 |
Rinish riveting rear spar and rib #1, lay out 1st skin on ribs |
1.00 |
||||
|
5/22/08 |
W17-01R W17-04 |
Remake W17-04 gusset, deburr and rivet root rib |
1.50 |
||||
|
5/21/08 |
W17-01R W17-04 |
Fit and drill Rt root rib, remove lower gusset- holes too close to edge of piece |
1.50 |
||||
|
5/20/08 |
W12-01R |
Drill and deburr rear spar |
1.00 |
||||
|
5/19/08 |
W12-01R |
Drill rear spar to ribs, set wing on table to level and square |
1.00 |
||||
|
5/15/08 |
W21-01R |
Reinstall Rt bellcrank, set up on sawhorses, align rear spar |
1.00 |
||||
|
5/13/08 |
W21-01R |
Remove Rt bellcrank, redrill with jig setup |
2.00 |
||||
|
5/12/08 |
W21-01R |
Rework Rt bellcrank, remount on rib |
1.50 |
||||
|
5/11/08 |
W21-01L W21-01R |
Rework Lt bellcrank, remove Rt crank from rib |
2.50 |
||||
|
1/30/08 |
W23-07 |
TUBING SUPPORT (4) |
0.50 |
||||
|
1/9/08 |
W17-02 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-03 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-04 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-05 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-06 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-07 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-08 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/9/08 |
W17-09 |
REINFORCEMENT ANGLE |
0.25 |
||||
|
1/6/08 |
W15-01 |
FORWARD RIB ASSY |
0.50 |
||||
|
1/6/08 |
W15-02 |
FORWARD RIB ASSY |
0.50 |
||||
|
1/6/08 |
W15-03 |
FORWARD RIB ASSY |
0.50 |
||||
|
1/6/08 |
W15-04 |
FORWARD RIB ASSY |
0.50 |
||||
|
1/6/08 |
W16-01R |
AFT RIB ASSY #1R |
0.50 |
||||
|
1/6/08 |
W16-01L |
AFT RIB ASSY #1L |
0.50 |
||||
|
1/6/08 |
W16-02 |
AFT RIB ASSY #2 (2) |
0.50 |
||||
|
1/6/08 |
W16-03 |
AFT RIB ASSY #3 (2) |
0.50 |
||||
|
1/6/08 |
W16-04 |
AFT RIB ASSY #4 (2) |
0.50 |
||||
|
1/6/08 |
W16-05 |
AFT RIB ASSY #5 (2) |
0.50 |
||||
|
1/6/08 |
W14-03 |
WEB SPACER (16) |
0.70 |
||||
|
1/1/08 |
W15-06 |
GUSSET (8) |
1.50 |
||||
|
12/30/07 |
W15-07 |
GUSSET (8) |
1.50 |
||||
|
12/30/07 |
W15-08 |
GUSSET STOCK |
NA |
||||
|
12/30/07 |
W15-09 |
GUSSET STOCK |
NA |
||||
|
12/30/07 |
W16-09 |
ANGLE |
0.25 |
||||
|
12/27/07 |
W21-02R |
RT BELLCRANK ASSY |
10.00 |
||||
|
12/23/07 |
W21-02L |
LT BELLCRANK ASSY |
5.00 |
||||
|
12/22/07 |
W21-13 |
FORWARD VERT CHANNEL |
NA |
||||
|
12/22/07 |
W21-14 |
AFT VERT CHANNEL |
NA |
||||
|
12/19/07 |
W21-05 |
SPACER BLOCK |
NA |
||||
|
12/19/07 |
W21-08 |
SPACER BLOCK |
NA |
||||
|
12/18/07 |
W21-09 |
CLIP (8) |
NA |
||||
|
12/17/07 |
W21-04 |
LOWER ANGLE |
NA |
||||
|
12/17/07 |
W21-06 |
UPPER ANGLE |
NA |
||||
|
12/17/07 |
W21-07 |
LOWER ANGLE |
NA |
||||
|
12/13/07 |
W13-05R |
RT TIP RIB ATTACH ANGLE |
0.20 |
||||
|
12/13/07 |
W13-05L |
LT TIP RIB ATTACH ANGLE |
0.20 |
||||
|
12/13/07 |
W12-01R |
RT REAR SPAR ASSY |
1.00 |
||||
|
12/13/07 |
W12-01L |
LT REAR SPAR ASSY |
1.00 |
||||
|
12/10/07 |
W13-03 |
RADIUS BLOCK (4) |
1.00 |
||||
|
12/9/07 |
W13-01R |
RT HAND ATTACH PLATE |
0.20 |
||||
|
12/8/07 |
W13-02R |
RT ROOT RIB ATTACH ANGLE |
1.00 |
||||
|
12/8/07 |
W13-02L |
LT ROOT RIB ATTACH ANGLE |
1.00 |
||||
|
12/8/07 |
W12-03R |
RT OUTBOARD REAR SPAR CHANNEL |
0.30 |
||||
|
12/8/07 |
W12-03L |
LT OUTBOARD REAR SPAR CHANNEL |
0.30 |
||||
|
12/7/07 |
W21-03 |
UPPER ANGLE |
NA |
||||
|
12/7/07 |
W12-O2R |
RT HAND REAR SPAR CHANNEL |
1.00 |
||||
|
12/7/07 |
W12-02L |
LT HAND REAR SPAR CHANNEL |
1.00 |
||||
|
12/4/07 |
W08-01L |
LT MAIN SPAR ASSY |
25.00 |
||||
|
12/3/07 |
W08-01R |
RT MAIN SPAR ASSY |
20.00 |
||||
|
11/13/07 |
W14-02 |
CENTER SPACER (20) |
0.40 |
||||
|
9/26/07 |
W11-09 |
VERTICAL STIFFENER ANGLE (2) |
0.50 |
||||
|
9/26/07 |
W11-10R |
RT TIE DOWN FITTING |
0.30 |
||||
|
9/26/07 |
W11-10L |
LT TIE DOWN FITTING |
0.30 |
||||
|
9/26/07 |
W11-11 |
OUTBOARD VERT STIFFENER ANGLE |
0.50 |
||||
|
9/26/07 |
W11-02 |
END WING ATTACH ASSY (2) |
2.00 |
||||
|
9/26/07 |
W11-06 |
ROOT WING ATTACH ASSY (2) |
2.00 |
||||
|
9/23/07 |
W11-08 |
UPPER STIFFENER ANGLE (2) |
0.50 |
||||
|
9/20/07 |
W11-05 |
END ATTACH ANGLE (2) |
0.30 |
||||
|
9/20/07 |
W11-07 |
ROOT ATTACH ANGLE (2) |
0.50 |
||||
|
9/16/07 |
W11-03 |
WING ATTACH BLOCK (4) |
0.50 |
||||
|
9/15/07 |
W11-01 |
LOWER ANGLE (2) |
3.00 |
||||
|
8/24/07 |
T02-02 |
STABILIZER ASSY |
|||||
|
8/24/07 |
T02-01 |
HORIZONTAL TAIL ASSY |
|||||
|
7/31/07 |
T02-03 |
ELEVATOR ASSY |
|||||
|
5/20/07 |
T03-05 |
FORWARD SPAR ASSY |
|||||
|
5/19/07 |
T09-01 |
MAIN SPAR ASSY |
|||||
|
5/19/07 |
T09-02 |
FORWARD SPAR ASSY |
|||||
|
5/19/07 |
T03-01 |
MAIN SPAR ASSY |
|||||
|
5/5/07 |
T03-04 |
MAIN SPAR CHANNEL (2) |
|||||
|
5/5/07 |
T03-06 |
FORWARD SPAR CHANNEL (2) |
|||||
|
5/3/07 |
T03-03 |
ATTACH ANGLE (2) |
|||||
|
5/1/07 |
T09-03 |
SPACER |
|||||
|
4/25/07 |
T07-05 |
TRIM TAB ASSY |
|||||
|
4/24/07 |
T12-09 |
CLIP |
|||||
|
4/24/07 |
T12-10 |
CLIP |
|||||
|
4/23/07 |
T07-06 |
TRIM TAB |
|||||
|
4/23/07 |
T07-07 |
CABLE ATTACH PLATE |
|||||
|
4/23/07 |
T07-08 |
ELEVATOR HINGE HALF |
1.00 |
||||
|
4/20/07 |
T12-07 |
FORWARD SPAR FITTING |
|||||
|
4/20/07 |
T12-08 |
FORWARD SPAR CHANNEL |
|||||
|
4/20/07 |
T06-04 |
ELEVATOR HINGE HALF (2) |
1.00 |
||||
|
4/20/07 |
T06-05 |
FORWARD ROOT RIB CLIP (2) |
1.00 |
||||
|
4/20/07 |
T04-03 |
RIB (2) |
|||||
|
4/20/07 |
T04-04 |
RIB (2) |
|||||
|
4/18/07 |
T04-01 |
RIB (2) |
|||||
|
4/18/07 |
T04-02 |
RIB (2) |
|||||
|
4/15/07 |
T06-06 |
CLIP (2) |
|||||
|
4/10/07 |
T10-01 |
ROOT RIB |
0.50 |
||||
|
4/10/07 |
T10-02 |
RIB #2 |
0.50 |
||||
|
4/10/07 |
T10-03 |
RIB #3 |
0.50 |
||||
|
4/5/07 |
T12-06 |
CLIP |
|||||
|
4/4/07 |
T12-03 |
UPPER SPAR CHANNEL |
0.50 |
||||
|
4/4/07 |
T12-04 |
LOWER SPAR CHANNEL |
0.50 |
||||
|
4/1/07 |
T13-06 |
ANGLE |
|||||
|
4/1/07 |
T13-07 |
HINGE |
0.30 |
||||
|
4/1/07 |
T13-02 |
RUDDER DRIVE HORN ASSY |
2.00 |
||||
|
4/1/07 |
T12-05 |
ANGLE |
|||||