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MM-DD-YYYY |
Hours |
Photos |
Scope of work |
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10-25-2004 |
4.0 |


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Laid out parts for
the firewall
Laid out position
lines on firewall
Drilled 2 inch hole
in upper channel
Laid out rivet line
on upper channel, positioned, drilled and clecoed upper channel to
firewall
Laid out rivet
pattern for firewall stiffeners, drilled and clecoed in place
Laid out channel
doublers, drilled and clecoed to vertical lower channel
Drilled center hole
to 5/8 inch for bungee pin
Cut lower section of
vertical lower channel down to 33mm
Positioned, drilled
and clecoed vertical lower channel to firewall
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10-26-2004 |
7.0 |


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Fit, drilled and
clecoed both gear gussets to the vertical lower channel and the upper
channel
Top channel stiffener
cut to size, drilled and clecoed to the upper channel and firewall
Drilled and clecoed
the vertical top channel to the firewall
Cut Z angle to size,
drilled and clecoed to front of firewall
Cut upper bearing to
size, drilled bolt hole pattern and used the nose gear strut to center the
upper bearing in the 2 inch hole in the upper channel, drilled the 4 bolt
holes and clecoed the upper bearing in place
Fit engine mount to
firewall to verify all parts line up correctly
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10-27-2004 |
5.0 |

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Drilled all holes up
to #20
Disassembled
firewall, deburred all holes
Cut slots for
steering rods
Applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to all mating surfaces of the firewall
Riveted and assembled
firewall
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10-28-2004 |
5.0 |


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Cut both nose gear
stops to size
Laid out and drilled
the holes for the firewall line in the rear lower bearing
Marked and cut the 2’
hole in the rear lower bearing
Clamped the nose gear
stops inside the lower channel and back drilled into the rear lower
bearing
Marked the center of
the front lower bearing and cut the 2” hole in it
Positioned the lower
bearing, the front lower bearing and nose gear stops then back drilled the
holes thru the nose gear stops
Cut the lower bearing
in half
Drilled the 1/8”
holes for the cotter pins in the ends of the bungee pin
Marked the stop plate
and drilled the two 3/16” holes
Trimmed the stop
plate to a circle and installed on top of the nose strut
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10-29-2004 |
5.0 |

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Laid out the parts
for the forward fuselage
Marked and cutout
both the floor bottom skins
Marked centerline on
floor bottom skins
Trimmed the bottom
channel to size and marked the centerline
Predrilled the 4
channel doublers and drilled and clecoed to the bottom channel
Marked, drilled and
clecoed the floor bottom skins and bottom channel in place
Started the layout of
the holes in the seat front doubler
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10-30-2004 |
6.5 |


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Laid out and cut the
holes in the seat front
Drilled the hole
pattern in the seat front doublers
Back drilled the holes thru the seat front doubler
into the seat front
Drilled rivet holes up to size
Drilled holes for
grommets up to size thru the seat front and seat front doubler
Disassembled the seat
front doubler from the seat front, deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Riveted the seat
front doublers to the seat front
Installed rudder
cable fairleads on seat front
Drilled the 4 channel
doublers to bottom channel up to size, removed doublers, deburred and
applied Cortec VCI-373 Wash
Primer/Corrosion Inhibitor to the mating surfaces
Riveted channel
doublers to the bottom channel
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11-1-2004 |
9.5 |



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Smoothed the edges of
both gear strut fittings
Fit and clecoed the
gear strut fittings to the cabin sides
Cut gauge boards for
the front and rear cabin width and set the width of the cabin
Drilled and clecoed
the cabin floor to the bottom of the cabin sides
Cut, positioned, back
drilled, and clecoed the front and rear floor stiffeners to the floor and
bottom of the cabin sides
Laid out, positioned
, back drilled the center floor stiffener to the floor
Cut both front bottom
lonerons to the proper angles, positioned, drilled and clecoed in place
Drilled all holes up
to proper size in floor bottom
Laid out, cut,
drilled the 1 1/8” hole in the front bearing and predrilled the rivet
holes
Laid out, cut,
predrilled the rivet holes in the front bearing bottom
Positioned the front
top bearing and front bearing bottom, drilled and clecoed in place
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11-2-2004 |
7.0 |


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Marked, cut, drilled
and clecoed the tunnel in place
Cut, drilled and
installed the tunnel angles and L angles at the front of the tunnel
Marked, predrilled
and positioned the central seat belt attachments
Drilled and clecoed
the central seat belt attachments
Marked, predrilled
and positioned the lateral seat belt attachments
Drilled and clecoed
the lateral seat belt attachments
Laid out, cut out for
the flap position and predrilled the flaperon stop
Positioned, drilled
and clecoed the flaperon stop to the seat front and the floor
Cut, positioned and
drilled the L angle for the flaperon stop
Drilled all holes up
to proper size in the tunnel, seat belt attachments, flaperon stop and
front bearing top and bottom
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11-4-2004 |
9.5 |




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Disassembled the
cockpit floor area and deburred all holes
Applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Assembled cockpit
floor and pulled all necessary A4 and A5 rivets
Smoothed edges on the
engine mount
Shaped lower
attachment of engine mount to fit the angle of the lower front longeron
Laid out and drilled
the seat back panel to the rear fuselage
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11-6-2004 |
8.0 |



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Squared firewall to
floor center line and clecoed firewall to floor
Fit engine mount to
firewall and clecoed
Fit and trimmed rear
uprights to the cabin sides
Squared the cockpit
center line with the rear fuselage using plumb lines and a laser
Fit, drilled and
clecoed the bottom channel to the bottom skin
Set the overlap of
the cabin sides with the side skins
Leveled the rear
fuselage and set floor at proper angle
Made two wing pick-up
templates
Positioned the wing
pick-up templates and clamped the cabin frame in proper position
Leveled the cabin
frame and the upper tubes
Laid out the rivet
pattern for the upper tubes
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11-7-2004 |
8.0 |


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Checked that the
cabin frame is on the center line with the cabin floor with a plumb line
Rechecked the upper
tubes for level and position of the wing pick-up templates
Drilled and clecoed
the upper tubes to the top longeron gusset
Drilled and clecoed
the cabin frames to the cabin sides
Drilled holes up to
size in the bottom of the firewall and rear lower bearing
Disassembled the
forward fuselage and applied Cortec
VCI-373 Wash Primer/Corrosion Inhibitor to the mating surfaces
Cut out the gussets
7F13-1 and drilled the rivet pattern
Predrilled the rivet
line in the rear uprights
Assembled the lower
forward fuselage to the rear fuselage
Back drilled the
rivet line in the rear uprights thru the side skins and clecoed
Fit the gussets to
the side channels, drilled and clecoed in position
Positioned, drilled
and clecoed the seat back channel
Began drilling holes
in the uprights to proper size
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11-8-2004 |
7.0 |


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Finished drilling all
holes in the sides of the fuselage and front cockpit up to size for final
joining
Applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Predrilled all bolt
holes in both gear strut fittings
Fit gear strut
fittings to side skins and bottom channel and drilled up to proper size
holes
Drilled pilot holes
for the lift struts and rounded the fitting corners
Cleaned the inside of
all the open steel tubes for the cabin frame, engine mount and flaperon
control
Cleaned gear strut
fittings and primed with self etching primer
Riveted the front
edge of the rear fuselage on both sides, top and bottom
Riveted gussets
7F13-1 and seat back channel
Riveted rear uprights
to side skins
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11-9-2004 |
4.0 |


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Cut down Yamaha
rubber boots and made new retainer plates for use around rudder pedal
links to the nose gear
Coated the inside of
all open steel tubes of the engine mount, cabin frame and flaperon control
with epoxy primer
Sprayed self etching
primer on engine mount and cabin frame
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11-10-2004 |
4.0 |


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Laid out rivet line
on seat back for the seat back channel and drilled up to size
Cut and clecoed L
angles on seat back panel
Riveted firewall to
cockpit floor
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11-11-2004 |
6.0 |

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Fit upper diagonal
tube to cabin frame and drilled holes to size
Used Poly Fiber
E-2310 Aluma-Dyne Phosphoric Acid Etch to clean the upper tubes and
diagonal tube then treated the tubes with E-2300 Aluma-Dyne Conversion
Coating
Sprayed one coat of
self etching primer on the upper tubes and diagonal tube
Sprayed another coat
of self etching primer on engine mount
Disassebled the seat
back, deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Assembled the cabin
frame and upper tubes and diagonal tube to the rear fuselage, cabin sides
and firewall
Assembled the seat
back and pulled the rivets in the seat back |
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11-12-2004 |
5.5 |
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Bent both doubler
strips to fit, drilled and clecoed
Laid out rivet
pattern on striker plates, drilled and clecoed in place
Drilled all holes in
doublers and striker plates up to size
Disassebled the
doublers, deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Assembled the
doublers and striker plates to the cabin sides and pulled the rivets
Laid out gussets for
the upper tubes and diagonal tube, drilled all holes up to size
Removed the gussets,
deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion Inhibitor to the mating surfaces
Riveted the gussets
to the upper channel
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11-14-2004 |
1.0 |

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Pulled remaining
rivets in floor of baggage compartment
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11-15-2004 |
2.0 |


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Primed the fuselage
area for the gear strut fitting with self etching primer
Drilled the lift
strut holes up to size and sprayed with self etching primer
Installed the gear
strut fittings to the fuselage with proper hardware and four A5 rivet in
each fitting
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11-16-2004 |
11.0 |



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Laid out, the left
front side skin and cut lower corner section and filed the edges
Marked and filed the
3mm notch and made the 10mm bend
Rolled the lower
section to follow the curve of the firewall
Positioned, drilled
and clecoed the front side skin to the cabin side
Laid out the bottom
edge rivet pattern, drilled and clecoed
Positioned, drilled
and clecloed the lower Z angle to the side skin
Back drilled the
holes thru the firewall to the front side skin up to the L angle location
Positioned, drilled
and clecoed the L angle to the front side skin
Back drilled the
holes thru the firewall to the front side skin up to the Z angle location
Positioned, drilled
and clecoed the top Z angle to the front side skin
Back drilled the
holes thru the firewall to the front side skin up to the side skin upright
location
Predrilled the side
skin upright
Drilled and clecoed
the side skin upright to the front side skin
Positioned, drilled
and clecoed the top aluminum plate and the lower Dzus plate
Positioned the steel
angle on the left side and drilled holes for engine mount bolt, front
rivet and side rivet
Laid out, the right
front side skin and cut lower corner section and filed the edges
Marked and filed the
3mm notch and made the 10mm bend
Rolled the lower
section to follow the curve of the firewall
Positioned, drilled
and clecoed the front side skin to the cabin side
Laid out the bottom
edge rivet pattern, drilled and clecoed
Positioned, drilled
and clecloed the lower Z angle to the side skin
Back drilled the
holes thru the firewall to the front side skin up to the L angle location
Positioned, drilled
and clecoed the L angle to the front side skin
Back drilled the
holes thru the firewall to the front side skin up to the Z angle location
Positioned, drilled
and clecoed the top Z angle to the front side skin
Back drilled the
holes thru the firewall to the front side skin up to the side skin upright
location
Predrilled the side
skin upright
Drilled and clecoed
the side skin upright to the front side skin
Positioned, drilled
and clecoed the top aluminum plate and the lower Dzus plate
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11-17-2004 |
4.0 |

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Positioned the steel
angle on the right side and drilled holes for engine mount bolt, front
rivet and side rivet
Drilled all six
engine mount holes to firewall up to 3/16” and clecoed
Laid out, cut and
bent the two panel side gussets
Positioned the panel
side gussets on each side of the panel, drilled and clecoed
Marked the overhang
of the gusset and trimmed the excess off both gussets
Riveted both panel
side gussets to the panel
Positioned the panel
in proper location, drilled and clecoed the panel side gusset to the cabin
frame
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11-18-2004 |
7.5 |

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Cut, laid out and
drilled two L angles for each side of the front side skins
Clecoed the two L
angles to the top edge of the side skins and 44mm down from the edge for
the front top skin to rivet to
Drilled all holes in
the front side skins up to size minus the holes for the front top skin
overlap
Marked and drilled
rivet pattern in the remainder of the firewall and the top of the
instrument panel
Marked the front side
skins for trimming
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11-19-2004 |
5.0 |


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Disassembled front
fuselage, deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Masked the firewall
off and primed front side of firewall with self etching primer and sprayed
with gray gloss paint
Sprayed engine mount
with epoxy gloss white paint
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11-20-2004 |
6.0 |

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Primed steel angles
for the firewall with self etching primer and sprayed with gray gloss
paint
Assembled front side
skins to fuselage front and clecoed engine mount in place
Riveted both side
skins to forward fuselage
Cut, drilled and
clecoed top L angle between the firewall and instrument panel top
Fit, back drilled and
clecoed front top skin to firewall and instrument panel
Fit, drilled and
clecoed the instrument panel top cover plate to the front top skin and
firewall
Drilled all holes in
front top skin up to proper size
Marked the front top
skin for trimming to size
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11-21-2004 |
5.0 |


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Removed the front top
skin, deburred all holes and trimmed edges to size
Fit, drilled and
clecoed the panel bottom channel to the instrument panel
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11-22-2004 |
8.0 |



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Drilled and clecoed L
angle to both sides of the tunnel
Cut out both seat
pans and fit to fuselage
Drilled and clecoed
the front of the right seat to the top flange of the seat front
Drilled and clecoed
the aft flange of the right seat to the seat back
Drilled and clecoed
the inboard edge of the right seat to the L angle on the tunnel
Drilled and clecoed a
short L angle to the right cabin side
Drilled and clecoed
the outboard side of the right seat to the short L angle
Drilled and clecoed
the front of the left seat to the top flange of the seat front
Drilled and clecoed
the aft flange of the left seat to the seat back
Drilled and clecoed
the inboard edge of the left seat to the L angle on the tunnel
Drilled and clecoed a
short L angle to the left cabin side
Drilled and clecoed
the outboard side of the left seat to the short L angle
Fabricated the left
and right gussets to close the opening between the cabin side, the seat
front and the seat
Drilled and clecoed
the right gusset in place
Drilled and clecoed
the left gusset in place
Cut and clamped the L
angle on the backside of the seat back
Back drilled the L
angle and assembled the seats
Cut and shaped the
tunnel gusset
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11-23-2004 |
4.5 |
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Drilled all holes up
to size in the seats
Disassembled the
seats, deburred all holes and applied
Cortec VCI-373 Wash Primer/Corrosion
Inhibitor to the mating surfaces
Riveted L angles on
the tunnel
Riveted the corner
gussets to the seat front
Riveted the upper
tubes to the cabin frame and the top longeron gusset
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12-18-2004 |
1.0 |
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Riveted lateral and
central seat bet attachments to fuselage side and tunnel
Riveted both seat
panels to the fuselage
Riveted the tunnel
gusset to the tunnel and seat back
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Total Time |
156.0 |
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Forward fuselage
complete until the controls and systems are installed
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