conrad booze - Experimental Aircraft Builder's Log

Conrads X-10 Build Log


Date: 5-4-2009
Number of Hours: 2.00
Manual Reference: 21-6, Step 2.
Brief Description: Clecoed at every other hole the Top Skin Assembly

05/04/2009 … 21-6, Step 2. Clecoed at every other hole the Top Skin Assembly A-1001-L (top) to the top Flange of the Spar Assembly. Placed AN426AD-3.3.5 rivets, secured with tape and riveted with a mush-room type set and bucked with the tungsten bar, removed the clecoes and repeated the process. Time for both Ailerons about 2 hours.

Top Skin Assembly A-1001-Left (top) to the top Flange of the Spar Assembly.

Top Skin Assembly A-1001- Right

Both Top Skin Assembly A-1001-Left/ Right (top) to the top Flange of the Spar Assembly

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Category		# Logs	# Hours

All		510	2382

Avionics		24	176

EAA and FAA Inspecti		2	1

Empennage		3	26

Engine		3	54

FAB		2	30

FF		5	38

FF1 Engine Installat		4	31

FF2 Cowl Baffle		9	88

Final_Kit		2	14

Flight_Training_and_		3	36

FUEL TANK Section 18		9	42

Fuselage		2	11

Gas_Expense		1	6

Hanger_Rent		1	90

Interior Finishing		6	37

Lights Nav and Strob		3	19

Miscellaneous		10	32

OP-37 Wiring Harness		12	18

Oxygen System		5	30

Paint Empennage		3	40

Paint Fuselage		2	14

Paint Wings		4	14

Perry_Apt_Hanger		7	88

Propeller		3	16

Section 10 Tail Cone		22	72

Section 11 Empennage		8	22

Section 12 Empennage		7	22

Section 13 Main Spar		5	11

Section 14 Wing Ribs		6	25

Section 15 Rear Spar		3	8

Section 16 Top Wing		2	12

Section 17 Outboard		6	47

Section 18 Fuel Tank		12	58

Section 19 Stall War		1	2

Section 20 Bottom Wi		16	56

Section 21 Aileron		15	32

Section 22 Flaps		9	42

Section 23 Aileron A		7	18

Section 24 Wing Tips		4	23

Section 25 Mid Fusel		5	25

Section 26 Mid Fusel		10	45

Section 27 Fire Wall		6	29

Section 28 Forward F		16	77

Section 29 Fuselage		24	84

Section 30 Step Inst		3	5

Section 31 Upper For		10	27

Section 32 Tail Cone		7	27

Section 33 Baggage A		10	24

Section 34 Baggage D		7	8

Section 35 Access Co		7	10

Section 36 Brake Lin		3	3

Section 37 Fuel Syst		5	13

Section 38 Rudder Pe		5	10

Section 39 Control S		7	14

Section 40 Flap Syst		1	10

Section 41 Upper For		3	10

Section 42 Rear Seat		3	7

Section 43 Cabin Cov		15	51

Section 44 Wing Atta		1	5

Section 45 Cabin Doo		21	100

Section 45A Cabin Do		7	15

Section 46 Engine Mo		8	29

Section 47 Spinner &		7	42

Section 48 Gear Leg		18	68

Section 49 Seats & S		4	8

Section 50 Cabin hea		1	2

Section 6 Vertical S		3	28

Section 7 Rudder		6	35

Section 8 Horizontal		9	54

Section 9 Elevators		20	83

Stall Warning Sectio		1	2

Tools		2	5

Wing Expenses		1

Wings		6	26