|
MM-DD-YYYY |
Hours |
Photos |
Scope of work |
|
07-05-2004 |
4.0 |


|
Marked rib
centerlines on left wing
Aligned top rear skin
and drilled and clecoed skin to main spar of left wing
Aligned rib center
lines and drilled and clecoed skin to the rear ribs of left wing
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|
07-06-2004 |
6.0 |



|
Cut, bent and shaped
8 false ribs for the top rear skin
Cut, bent and shaped
6 false ribs for the bottom rear skin
Marked, drilled and
clecoed the rear channel to the top rear skin of the left wing
Drilled and clecoed
the fuel tank rear channel to the top rear skin.
Marked the inboard
end of the left wing top rear skin for the cutout area
Drilled all holes in
ribs, rear channel and fuel tank rear channel up to size.
Countersunk the six
rivet holes at the main spar to top rear skin and installed flush rivets
Marked, drilled,
aligned and clecoed the 4 false ribs to the top rear skin of the left wing |
|
07-07-2004 |
5.0 |

|
Turned left wing over
and leveled the wing with a 1”X6” 12’ board holding up the trailing edge
Positioned and
aligned the lower rear skin
Drilled and clecoed
the skin to the main spar and rear ribs
Drilled and clecoed 3
false ribs to the lower rear skin
Used a 1”X6” 10’ long
MDF board painted white to help hold the skin flat
Made cutout in the
inboard lower trailing edge
Marked, drilled and
filed the 2 slots for the flaperon brackets in the inboard trailing edge
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|
07-08-2004 |
4.5 |


|
Marked, drilled and
filed the 3rd slot for the flaperon bracket in the outboard trailing edge
Drilled and clecoed
the trailing edge to the rear channel and lower rear skin
|
|
07-09-2004 |
5.0 |



|
Marked, drilled and
filed the 4 slots for the slat brackets in the nose skin of the left wing
Aligned, drilled and
clecoed the nose skin to the bottom of the left wing spar
Aligned nose ribs,
drilled and clecoed them to the nose skin
Used piano hinge wire
thru the slat attachment bracket hos to help hold down the nose skin and a
1”X6” MDF board to hold the nose skin flat against the nose ribs
Marked, drilled,
nibbled and filed the slot for the forward lift strut attachment fitting
Laid out rivet
pattern for the angle support at the lift strut fitting
|
|
07-10-2004 |
7.0 |



|
Drilled and clecoed
the angle support and the lift strut fitting
Laid out rivet
pattern for jury strut fittings at rib #2
Drilled and clecoed
on half of the jury strut fittings at rib #2
Fabricated the
flaperon bracket alignment tool
Cut, filed, drilled
and clecoed the 4 flaperon attachment arms to the bottom of the left wing
Drilled all remaining
holes to #40 on the bottom of the left wing and clecoed with silver clecos
Drilled all the holes
on the bottom of the left wing to #30 and clecoed with copper clecos
Drilled 8 holes in
the lift strut fitting and support angle to #20 and installed black clecos
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|
07-12-2004 |
6.5 |



|
Laid out rivet
pattern for second half of both jury strut fittings at rib #2
Drilled, shaped and
trimmed the jury strut fittings
Shaped, trimmed and
filed the L angles at 4 flaperon attachment arms
Disassembled bottom
of wing, deburred all holes and started applying
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to all mating surfaces
|
|
07-13-2004 |
3.0 |



|
Finished applying
Cortec VCI-373 Wash
Primer/Corrosion Inhibitor to all mating surfaces of the bottom and nose
skins
Assembled bottom of
wing with clecos
Pulled rivets in
bottom of wing except along leading edge and forward lift strut angle
Turned wing right
side up and leveled wing
|
|
07-14-2004 |
8.0 |


|
Filed, and smoothed
the 4 flaperon attachment arms for the bottom of the right wing
Filed and smoothed
the 8 L angles for the flaperon brackets for the right wing
Filed and smoothed
the forward lift strut attachment for the right wing
Cut, filed and
smoothed the 12 fuel tank channel for both wings
Removed top skin from
left wing
Removed top skin
cutout inboard of rib #1 and filed the edges smooth
Drilled and applied
Cortec VCI-373 Wash
Primer/Corrosion Inhibitor to all mating surfaces
and installed the 6 fuel tank channels on ribs #1 and #2 and on main spar
of the left wing
Reinstalled top skin
on left wing
Worked nose skin into
position and drilled with #40 and clecoed skin to nose ribs
Cleaned nose skin for
marking of main spar rivet line
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|
07-15-2004 |
5.0 |





|
Marked and drilled
main spar rivet holes to #40
Marked and drilled
bent L angle rivet holes to #40
Drilled all holes in
nose skin up to #30
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|
08-05-2004 |
8.0 |




|
Built access panel to
mount pitot-static tube on
Built reinforcement
panel for access panel
Aligned and drilled
access panel to accept pitot-static tube
Marked and cut out
area between nose ribs #3 and #4 to install pitot-static tube
Aligned and drilled
reinforcement panel and nose skin
Installed #6 screw
nutplates on reinforcement panel
Fit all parts
together then removed the pitot tube to continue work on the wing
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|
08-07-2004 |
5.0 |



|
Deburred all
remaining holes in nose skin
Riveted the angle
support and lift strut fitting to wing bottom
Riveted forward jury
strut fitting to bottom of wing
Riveted bottom half
of nose skin to skeleton
Riveted pitot tube
reinforcement panel to nose skin
Removed top wing skin
Attached cork to fuel
tank and wing skeleton channels
Drilled fuel tank
outlet hole in rib #1
Drilled fuel tank
drain hole in lover wing skin
Installed nutplates
for strobe power supplies on left and right wing spar tips.
Clecoed L angles on
end of left and right spar tips |
|
08-10-2004 |
5.0 |
|
Fabricated domed
access covers to go on top of both wings over the capacitive type fuel
quantity probes |
|
08-11-2004 |
3.0 |



|
Attached cork to side
of right fuel tank
Cut holes in top of
both fuel tanks for fuel probe
Installed fuel probe
in each fuel tank
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|
08-13-2004 |
2.0 |
|
Fabricated
reinforcement rings for the domed fuel probe access covers
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|
08-15-2004 |
3.0 |


|
Ran wires for the nav
and strobe lights the length of the wing
Built wire harness
for fuel probe and installed in the wing
Installed 2 styroform
battans on top of fuel tank
Installed strobe
power supply in wing tips of both wings
Installed finger
strainer and nipple for fuel outlet of tank
Attached fuel tank
ground wire and wing ground wire to #1 rib
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|
08-16-2004 |
4.0 |


|
Installed pitot and
static lines in wing and secured with ties
Cut holes in top wing
skin for fuel filler neck and domed access panel
Drilled all holes for
the domed access panel
Deburred all holes on
inside of top wing skin
Applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to all mating surfaces on the inside of the top skin and wing
skeleton
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|
08-17-2004 |
6.0 |



|
Installed #8
nutplates on domed access panel
Installed access
panel on wing skin
Inspected inside of
left wing prior to closing up the wing
Installed top skin on
wing
Pulled all the rivets
on the wing top skin
Drilled the trailing
edge holes and deburred the holes
Squeezed all the
rivets on the trailing edge
Marked and cut the
wing tip curved top skin and bottom skin
Fluted the wing tip
top and bottom angles and clecoed in place
Began the alignment
of the fiberglass wing tip panel
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|
08-18-2004 |
6.0 |


|
Trimmed nose skin to
proper size
Fit and trimmed the
wing tip skin and clecoed in place
Drilled mounting
holes in both fiberglass wingtip panels for the Nav/Strobe lights
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|
08-19-2004 |
8.0 |




|
Built an access panel
and reinforcing plate for the panel to go on the wingtip skin
Painted the
fiberglass wingtip with gray primer, inside and outside
Installed the Nav/Strobe
light head on the fiberglass wingtip
Clecoed fiberglass
wingtip in position on the wing
Ran the electrical
wires to the strobe power supply and the nav light
Tested the strobe and
nav lights for operation, both work fine
Secured all wires in
the wingtip bay
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|
08-20-2004 |
4.0 |


|
Rolled the edge of
the top, bottom, nose and wingtip skin for a better fit
Riveted wingtip top
and bottom angles to the skin
Riveted wingtip to
top and bottom angles
Predrilled holes for
wing root skin
Measured and laid out
the wing root skin pattern
Began drilling and
clecoing wing root skin in place
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|
08-22-2004 |
4.0 |


|
Finished drilling and
clecoing wing root skin in place
Drilled all wing root
skin holes up to size
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|
Total Time: |
112.0 |
|
Left wing done until
fuselage is finished |