MM-DD-YYYY

Hours

Photos

Scope of work

09-30-2004

4.0

Confirmed dimensions of predrilled bottom skin

Laid out centerline on bottom skin

Trimmed and smoothed edges of rear bottom skin

Rough cut the access hole in bottom skin

10-01-2004

4.0

Finish trimmed the access hole in bottom skin

Cut and drilled the two lateral L angles and Z angle to bottom skin

Began layout for a rear fuselage access panel

10-02-2004

7.0

Finished layout of rear access panel

Cutout, drilled and installed hinged access panel in bottom skin

Laid out, cut, drilled and installed supplemental L angles between the lateral L angles on bottom skin

11-03-2004

8.0

Installed forward and aft rear fuselage longerons on left and right sides of  bottom skin

Installed Rear Torque Tube Bearing to Bottom Channel

Installed Bottom Channel to bottom skin

Installed Z angle to left and right side of fuselage access hole

Installed Short L angles on both sides of fuselage access hole

Drilled all holes up to #30

11-04-2004

2.5

Laid out hole pattern for nutplates on access cover and fuselage bottom skin

Laid out hole pattern for nutplates on rear access panel

Drilled alignment holes for both panels to #30

10-05-2004

8.5

Drilled and installed sixteen 8-32 nutplates around access hole

Drilled and installed five 8-32 nutplates around rear access panel

Trimmed left and right side skins to size

Clecoed side skins together and filed all edges to the same size

Aligned, drilled, cut and clecoed L angles to left side skin

Aligned, drilled, cut and clecoed additional L angles to left side skin to make X’s and one diagonal brace

10-06-2004

10.5

Aligned, drilled and clecoed upper longerons on left side skin

Aligned, drilled and clecoed lower longerons on left skin

Drilled all holes in left skin up to #30

Aligned, drilled, cut and clecoed L angles to ight side skin

Aligned, drilled, cut and clecoed additional L angles to right side skin to make X’s and one diagonal brace

Aligned, drilled and clecoed upper longerons on ight side skin

Aligned, drilled and clecoed lower longerons on right skin

Drilled all holes in right skin up to #30

Disassembled and debureed the bottom skin, L angles and Z angles

Drilled necessary holes in Rear Torque Tube Bearing and Bottom Channel up to #20

Disassembled Rear Torque Tube Bearing and Bottom Channel and deburred all holes

Applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the bottom skin and angles

Assembled bottom skin to L and Z angles and Rear Torque Tube Bearing and Bottom Channel

Riveted L and Z angles and Rear Torque Tube Bearing and Bottom Channel to bottom skin

10-07-2004

7.0

Disassembled right skin and deburred all holes

Applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the right skin and angles

Assembled right skin to L angles

Riveted L angles to right skin

Disassembled left skin and deburred all holes

Applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the left skin and angles

Assembled left skin to L angles

Riveted L angles to left skin

Deburred left and right lower longerons

Applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the left and right lower longerons

10-08-2004

5.0

Trimmed top skin to size

Filed all edges of the top skin

Aligned, drilled, cut and clecoed L angles to the top skin

Aligned, drilled, cut and clecoed additional L angles to the top side skin to make X’s

Laid out 112mm hole in rear of top skin and cutout

Trimmed rear top skin stiffener

Laid out rivet pattern around rear top stiffener and drilled to #40

10-09-2004

6.0

Drilled all holes in top skin and L angles to #30

Disassembled top skin and deburred all holes

Applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the top skin and angles

Assembled top skin to L angles

Riveted L angles to top skin

Riveted additional L angles to the top side skin to make X’s

Cut rudder cables pass thru holes in left and right skins

Trimmed rear bulkheads to fit side skins

Fit left skin to bottom skin

Fit right skin to bottom skin

10-10-2004

6.0

Drilled HT bulkheads to side skins

Cut, drilled and installed L angles on top edged of HT bulkheads

Cut and fit rear diagonal L angles

Fit top skin to the side skins

Drilled HT bulkheads to top skin

Cut and trimmed rear longerons

Drilled all holes to proper size

Disassembled rear fuselage, deburred remaining holes, applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the top skin, bottom skin and side skins

Assembled and riveted the bottom skin to the lower longerons

Assembled and riveted the top skin to the upper longerons

Riveted rear top stiffener to top skin

Riveted L angles on top edge of HT bulkheads

10-11-2004

4.5

Assembled rear fuselage with clecos

Riveted lower right and left longerons to side skin

Riveted both HT bulkheads to bottom skin

Riveted upper right and left longerons to side skin

Riveted sides of HT bulkheads to the side skins

Trimmed, drilled and clecoed both rudder cable outlets and rudder cable fairlead to sides of rear fuselage

10-20-2004

7.5

Aligned, drilled and clecoed 10 gussets at corners of L angle verticals and L angle horizontals

Cutout area from 2 gussets for rudder cable clearance

Removed gussets, deburred L angles and gussets and applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the gussets

Installed 10 gussets and riveted in place

Aligned, drilled and clecoed uprights to predrilled holes

Predrilled baggage compartment back panel and clecoed to horizontal and vertical L angles

Installed L angles for sides of extended baggage panel

Installed zee channel between uprights

Cut extended baggage panel to size, predrilled holes on 3 sides and clecoed in place

Marked bottom of extended baggage panel for 2 L angles supports

Cut and marked two L angles supports for the extended baggage panel lower side

Trimmed the bottom longerons to match the side and bottom skins

10-21-2004

6.0

Cut, aligned and drilled both side channels and clecoed in place

Positioned, drilled and clecoed both top longeron gussets to top skin

Cut shoulder harness attachment to size, drilled and clecoed both attachments to side skins

Filed slot in tapered channel, positioned, drilled and clecoed channel to the side skins

Cut the rear wing attachment brackets to size and predrilled the holes

Checked the distance between the two wing attachment bolt holes and drilled the brackets and attached to the side channels with cleos

Cut the top channel to proper angle and size

Clamped the top channel behind the rear wing attachments, drilled and clecoed

Drilled and clecoed the rivet line on the top skin through the top channel

Cut, positioned, drilled and clecoed the uprights to the fuselage side skins

10-22-2004

6.5

Trimmed upright doublers

Positioned, drilled and clecoed upright doublers to the side channels and uprights

Laid out and cut the baggage floor

Cut and installed L angle inside of front flange on the baggage floor

Predrilled holes on sides of baggage floor

Positioned baggage floor, drilled and clecoed

Cut the seat back to size

Positioned, drilled and clecoed the seat back in place

10-23-2004

9.5

Cut, aligned, drilled and clecoed both aileron control rod covers in baggage compartment

Cut, drilled and clecoed all L angles for the aileron control rod covers

Cut, drilled and clecoed L angle supports under extended baggage floor

Drilled all holes in baggage compartment up to #30

Fabricated antennae reinforcement plate, installed #6 nutplates for attachment, drilled all holes to size including BNC connector access hole

Disassembled baggage compartment

10-24-2004

8.0

Installed wires for the elevator trim and tail light in rear fuselage and secured to L angle verticals on the right side of the fuselage

Drilled necessary holes up to #20 in baggage compartment

Deburred all holes in baggage compartment and applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the baggage compartment

Assembled the baggage compartment and riveted the extended baggae compartment area

11-28-2004

1.0

Installed both L angles at the ends of the bottom channel

1-8-2005

1.5

Drilled the rest of the holes thru the top angles of the aileron control tube covers and thru the fuselage top skin

Deburred all holes applied Cortec VCI-373 Wash Primer/Corrosion Inhibitor to all mating surfaces of the aileron control tube covers

Total Time:

113.0