John D Hazen - Experimental Aircraft Builder's Log

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Date: 2-16-2021
Number of Hours: 4.00
Manual Reference: 26iS/U and 28iS/U
Brief Description: Tank Mount and Rudder/BrakePedals

Completed steps 7-9 page 26iS/U-08 Step 7: Ensured that the bottom of the fuel tank is seated fully down and forward, then match-drilled #12 the screw hole in the F-01227 into the F-01229A and F-01229-1. Step 8: Removed the F-01229-1 and F-01229A, match-drill the nutplate rivet holes into both parts, then deburred the holes. Step 9: Machine countersunk the F-01229A for the nutplate attach rivets, dimpled the F-01229-1 and F-01229A for the other two flush rivets, then riveted the two parts and nutplate together. Removed tankat rthis point. Completed steps 1-6 page 28iS/U-02 Step 1: Cut the F-1235A Inbd Rudder Pedal Block and the two F-1235B Outbd Rudder Pedal Blocks as shown in Figure 1. Marked the split parts so that they remain together and so that they can be assembled in their original, pre-split orientation. Step 2: Temporarily clamped the WD-01206-1 Rudder Pedals using the F-1235A & B Rudder Pedal Blocks as shown in Figure 2. Checked that the rudder pedals were oriented as shown in the figure (long end and short end together), and placed the heads of the bolts on the bottom so that the clamped assembly will lay flat on the work surface. Step 3: Slid the WD-1211-L & -R Brake Pedal Torque Tubes into the WD-01206-1 Rudder Pedals as shown in Figure 3. Step 4: Checked that the F-1235A & B Rudder Pedal Blocks are all flush against the work surface , then temporarily slid one of the remaining WD-1211-L or -R Brake Pedal Torque Tubes into both of the WD-01206-1 Rudder Pedals as shown in Figure 3.This will lock both rudder pedals into the neutral position. Step 5: Temporarily attached the BRAKE MAST.CYL.RIGHT-1 & LEFT-1 Right and Left Brake Master Cylinders to the WD-01206-1 Rudder Pedals and WD-1211-L & -R Brake Pedal Torque Tubes as shown in Figure 4. Step 6: Slid the WD-1209 Brake Pedals over the WD-1211-L & -R Brake Pedal Torque Tubes and against the WD-01206-1 Rudder Pedals as shown in Figure 4. Used a square to make sure both the WD-1209 and WD-01206-1 are vertical (or perpendicular to the wo

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Category		# Logs	# Hours

All		502	1448

10.0 Tailcone		32	89

11.0 Empenage Assemb		9	28

11.0 Empennage Attac		9	28

11iS Empenange Attac		5	8

12iS Emmpenage Fairi		1	2

13.0 Wing Spar Assem		5	16

14.0 Rear Spar, Stub		9	18

14.0 Wing		9	18

15.0 Wing Ribs		17	55

16.0 Stall Warning		4	7

17.0 Wing Skins		36	110

18.0 Flaperons		12	42

20.0 Fuselage Center		6	22

20is Center Section		32	89

21.0 Mid Fuse Ribs a		36	118

21IS Mid Fuse Ribs a		21	96

22.0 Fwd Lower Fusel		6	22

22iS/U FWD Lower Fus		5	21

23.0 Fuselage Side S		19	62

23iS/U Side Skins		13	44

24.0 Rollover Struct		9	28

24iS/U Rollover Stru		9	34

25iS/U Seatbacks		3	11

26.0 Seat Backs		2	6

26iS/U Fuel Tank		1	4

27 iS Fuel Syste		6	18

27.0 Rudder Pedals a		5	16

27iS/U iS Fuel Syste		6	18

28.0 Fuel System		7	22

28iS/U Rudder Pedals		3	13

29A.0 Fwd Upper Fuse		12	33

29iS/U FWD Upper Fus		13	46

32iS/U Flight Contro		3	7

35GiS/U Preminum Bra		1	3

35iS/U Landing Geat		1	1

40.0 Lighting		13	38

6.0 Vertical Stabili		17	38

7.0 Rudder		11	22

7A Trim Tab		1	2

8.0 Anti Servo Tabs		5	9

9.0 Horizontal Stabi		24	42

Empennage		4	9

Empennage		17	38

Empennage/Tailcone K		17	38

Fixtures		2	9

Fuselage		6	9

Hangar		4

Miscellaneous		7	22

SB 18-02-03 AST		1	2

SB180202		2	5

Shop Supplies		2	8

Wings		2	2