JIGGING OF THE FUSELAGE
.....
In this step, you will want to trim for final fitting the
following bulkheads: FS175, FS120, FS94, Seatback Bulkhead, and
Firewall. All bulkheads, including the firewall, fit inside the shells,
so that they rest against the inside skin of the shells. Begin by
drawing BLOO down the bottom fuselage shells, forward and rear. Check
the squareness of the lower forward fuselage shell where the firewall is
located. It may be necessary to trim the forward edge of the lower
forward fuselage shell to make the firewall set square. (i.e.
perpendicular to BLOO and WL15). For now, you may assume that a level
placed across the longitudinal split line at the firewall attachment
point is correct for leveling the fuselage laterally. Don't forget that
the firewall fits inside the shell. The FS120 bulkhead location is
nominally at FS120 for the forward face, but is uncritical and can be
moved plus or minus 1 inch for best fit. The FS94 bu1khead should not be
trimmed until after the Seatback Bulkhead. The FS175 bulkhead aft face
is located at FS175.
.....
The location and angle of the seatback bulkhead is the prime
consideration for comfortably accommodating different pilot sizes. If
the primary pilot is over 616" tall or less than 5'5" tall, then Quickie
Aircraft Corporation should be contacted for assistance in creating a
comfortable fit. Basically, moving the break point in the Seatback
Bulkhead lower allows the
Summary of Contents for Q2 Lite
Page 10: ...Q2 Plans Appendix Page v Q2 Plans Chapter 1 Page 1 1...
Page 17: ...Q2 Plans Chapter 1 Page 1 3...
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Page 25: ...CONTINUED ON NEXT PAGE PAGE 3 1 Q2 Plans Chapter 3 Page 3 02...
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Page 70: ...CONTINUED ON NEXT PAGE PAGE 3 15 Q2 Plans Chapter 3 Page 3 16...
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Page 74: ...CONTINUED ON NEXT PAGE PAGE 3 16 Q2 Plans Chapter 3 Page 3 17...
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Page 123: ...END OF CHAPTER PAGE 7 2 Q2 Plans Chapter 8 Page 8 01...
Page 127: ...CONTINUED ON NEXT PAGE PAGE 8 2 Q2 Plans Chapter 8 Page 8 03...
Page 134: ...END OF CHAPTER PAGE 8 5...
Page 136: ...NOTE See Bottom and Top Main Wing Lamination Drawing for exact sizing of sparcaps A thru M...
Page 137: ...CONTINUED ON NEXT PAGE PAGE 9 1 Q2 Plans Chapter 9 Page 9 02...
Page 138: ...CONTINUED ON NEXT PAGE PAGE 9 2 Q2 Plans Chapter 9 Page 9 03...
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Page 246: ...PAGE 15 1 Q2 Plans Chapter 15 Page 15 02...
Page 249: ...END OF CHAPTER PAGE 15 2 Q2 Plans Chapter 16 Page 16 01 ENGINE INSTALLATION...
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Page 276: ...END OF CHAPTER PAGE 17 3...
Page 279: ...END OF CHAPTER PAGE 18 1...
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Page 295: ...Congratulations on completing your very own Q2 PAGE 20 4...
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