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John (Jack) Clark's Web Site
RV-A8  
  All  
  12-10-2007
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Date:  12-10-2007
Number of Hours:  1.50
Manual Reference:  8-33
Brief Description:  Start fuselage final assembly

Spray can primed forward floor contact areas common with the lower longeron and center spar.

Bolted the lower ongerons to the forward floor with AN-3 5A bolts. The bolts were torqued to 25 in-lbs and marked with Torque seal.

Riveted lower longerons in place.

Clecoed the forward/center/mid sections together.
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RV-14A Home

RV-A8 Home

Category # Logs  # Hours


 All 2277 5987

 Aircraft Related 314 1351

 Avionics 206 404

 Brakes 11 18

 Canopy 41 63

 Cooling System 7 9

 Cowl Flap 13 20

 Cowling 146 354

 Electrical System 157 311

 Empennage 29 48

 Engine 88 158

 Fiberglass 148 316

 Finishing Kit 27 76

 First Flight Prep 4 1

 Flight Control Syste 75 118

 Flight Testing 18 20

 Flights 6 7

 Forward Baggage Comp 6 9

 Forward Top Skin 24 36

 Fuel System 84 155

 Fuselage 344 812

 Heating System 1 0

 Inspection 5 5

 Interior 24 20

 Landing Gear 53 100

 Lighting 17 24

 Miscellaneous 8 5

 None 14 6

 Oxygen System 5 6

 Painiting 11 28

 Painting 11 28

 Prop 22 27

 Sensors 5 7

 Testing 1 1

 Ventilation 3 4

 Windscreen 8 13

 Wing Construction 27 76

 Wings 314 1351









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