Section 33 Baggage Area
Page 33-4
Step 1: One of the two F-1022 Baggage Floor Stiffeners is shown (unbent) in Figure 1. Separate them into their component parts (F-1022B,C,D,E,F, and G) by removing the shaded areas depicted in the figure.
Step 2: Remove from the fuselage all of the parts clecoed in this section.
Step 3: As Shown in Figure 2, Cleco the F-1022 Baggage Floor Stiffeners to the bottom of the F-1022A-L and-R Baggage Floors only the right baggage floor is shown in the figure), then final-drill #40 the holes common to the parts.
Step 4: Final-Drill #40 the 3/32" holes in the aft flange of the F-1022A Baggage Floors..
Step 5: Final-Drill #30 the three rows of holes in both F-1022A Baggage Floors indicated in Figure 3.
Step 6: Deburr the holes of all parts drilled in this section.
NOTE: Now begins the task of dimpling. In the following steps, to facilitate hole identification, many of the parts being dimpled are shown in their installed position.
Step 7: Dimple the #40 nutplate attachment rivet holes near the outboard edge of both F-1024 Seat Floors see Figure 4). Do not dimple the #19 holes.
Step 8: Dimple the holes along the forward edge of both F-1024 Seat Floors (See Figure 4) and the common holes in the underlying flange of the F-1005A Rear Spar Bulkhead. The #19 holes are dimpled for AN509 flush head screws.
Step 9: Dimple the #30 and #40 holes along the inboard edge of both F-1024 Seat Floors (see Figure 4) and the common holes in the underlying flange of the F-1017A Rear Seat Ribs. Do not dimple the #19 holes.
Step 10: There are nutplate holes patterns punched in the tip flange of the F-1005A and F-1034A Bulkheads between the F-1024 Seat Floors. Of these holes, dimple the #40 holes in the F-1034A Bulkhead and the #40 and #19 holes in the F-1005A bulkhead.
Page 33-5
Step 1: Dimple the #30 and #40 holes in both baggage floors (including the holes in the aft flange) except for the following:
Do not dimple the hoes in the F-1022A Baggage Floor which are common to the bottom flange of the F-1027 Close-Out Panel (see Figure 2 Below)
Or the single hole indicated on the bottom of Page 33-6, Figure 2.
Do not dimple the holes in both baggage floors indicated in Figure 1.
Step 2: Dimple the #19 holes along the inboard edge of both F-1022A baggage Floors (common to the F-1019 Inbd Baggage Ribs) for AN509 Flush head screws.
Step 3: Dimple all of the holes in the top flange of the F-1019 Inbd Baggage Ribs for the dimples in the F-1022A Baggage Floors.
Step 4: Dimple the #30 holes in the F-1023B Baggage Floor Angles which are common to the F-1022A Baggage Floor.
Step 5: Dimple (flush on the forward side) the three holes in the vertical flange of the F-1027 Close-Out Panel, the four holes in the inboard vertical flange of the F-1031 Upper Baggage Door Seal Channel,
and the holes in the
F-1006A Bulkhead which are common to these holes.
Step 6: Final-Drill #40 and machine countersink (flush on the forward side for AN426AD3 rivets) the four 3/32ths" nutplate attachment rivet holes in the F-1031 Upper Baggage Door Seal Channel.
Step 7: Dimple the two holes in the lower end-tab of the F-1026 Lower Baggage Door Seal Channel.
Step 8: Dimple the holes in the F-1022 Baggage Floor Stiffeners.
Step 9: Prime all of the parts that have been drilled and dimples up to this point if/as desired.
NOTE: The seat and baggage floors will now be riveted. Although possible later, now is a good time to run any cables or wires that will pass under the seat and baggage floors.
I ran some extra corrugated black wire conduit through this section on the advice of other builders
Step 10: Rivet the F-1022 Baggage Floor Stiffeners to the F-1022A-L and-R Baggage Floors using the rivets called-out in Figure 3.
Step 11: Rivet the nutplates shown in Figure 4 to the bottom of both F-1024 Seat Floors using the rivets called out.
Page 33-6
Step 1: Rivet the two nutplates to the upper Baggage Door Seal Channel using the rivets called out in Figure 4.
Step 2: Rivet in place the F-1024 Seat Floors, F-1022A Baggage Floors, and the F-10103A Lower Seat Hinge Halves using only the rivets called-out in Figure 1. The remainder of the seat floors are riveted in a later section.
