| A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | |
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1 | Chapter | Category | Item | Qty | Units | Notes | ||||||||||||||||||||
2 | Chapter 3: Education | |||||||||||||||||||||||||
3 | Glass: | BID | 4 | yd | I purchased 4 yd of BID and had some leftover. | |||||||||||||||||||||
4 | UND | 2 | yd | I purchased 2 yd of UNI and had some leftover. | ||||||||||||||||||||||
5 | Epoxy: | 0.25 | gal | I purchased a quart kit of Aeropoxy (PR2032 & PH3660) | ||||||||||||||||||||||
6 | Foam: | urethane board (tan) 1" thick | You'll also need a 2" thick (7"x7") urethane block; or you can glue two 1" blocks together instead. | |||||||||||||||||||||||
7 | urethane board (tan) 2" thick | <-- not necessary if you glue two 1"x7"x7" blocks (see note above this line) | ||||||||||||||||||||||||
8 | Other: | Flox | 1 | lb | ||||||||||||||||||||||
9 | Micro | 1 | lb | |||||||||||||||||||||||
10 | Peel-ply (dacron) - 2" roll | 1 | roll | Not necessary but get some now so you can experiment with it. | ||||||||||||||||||||||
11 | ||||||||||||||||||||||||||
12 | Chapter 4: Bulkheads | |||||||||||||||||||||||||
13 | Hardware: | AN509-10R10 screws | 6 | ea | Used in firewall for rudder pulley bracket attachment bolts. (Alternative: MS24694-S52) | |||||||||||||||||||||
14 | Glass: | BID | 5 | yd | Look at my 'Materials ordered' tab; I ordered a lot of BID and UNI to get me through the next few chapters. | |||||||||||||||||||||
15 | UND | 3 | yd | Look at my 'Materials ordered' tab; I ordered a lot of BID and UNI to get me through the next few chapters. | ||||||||||||||||||||||
16 | Epoxy: | 0.5 | gal | Purchased a 5 gallon kit to take care of the next few chapters | ||||||||||||||||||||||
17 | Foam: | 0.8" thick type R45 | 8 | sq. ft. | PVC Foam type H45 (same as R45); one panel (0.75"x32"x48") Divinycell H-45 (this makes both the front seat and the rear seat bulkheads). | |||||||||||||||||||||
18 | 0.2" thick type R250 | 9 | sq. ft. | PVC Foam type H250 (same as R250); 2 panels of (1/4"X 24.8"X 27.75"). One for the instrument panel and F28 bulkheads, another panel for the F22 and doubler. | ||||||||||||||||||||||
19 | Wood: | 24" x 30" x 0.25" 5-ply birch plywood | 1 | pc | Leftover scraps of this will be used in Ch 8 & Ch 9; also, the instrument panel gets a small plywood insert from this board as well. | |||||||||||||||||||||
20 | Metals: | 24" x 30" x 0.016" stainless steel (321) | 1 | pc | Decided to go with type 321 due to its ability to maintain corrosion resistance when it undergoes heat cycling. | |||||||||||||||||||||
21 | Misc: | 24" x 30" x .040" fiberfrax 970-F | 1 | pc | Not necessary to order now since it is not installed untill fuselage assembly. | |||||||||||||||||||||
22 | Peel-ply (dacron) | Get two 2" rolls | ||||||||||||||||||||||||
23 | ||||||||||||||||||||||||||
24 | Chapter 5: Fuselage sides | |||||||||||||||||||||||||
25 | Prefab parts: | LMGA assembly | 2 | pcs | see page 5-3 for specs; requires two 6.75" 4130 steel tubes 5/8" OD x 0.049 wall (got them from the Cozy Girls (CG Products) - includes the LMGA-B bushings) | |||||||||||||||||||||
26 | LMGA-B bushing (any steel) | 4 | ea | see page 5-3 for specs; requires four steel bushings; got them from the Cozy Girls (CG Products) as part of the LMGA assy. | ||||||||||||||||||||||
27 | Hardware: | AN6-80A bolts | 2 | ea | Main landing gear attachment bolts. ACS does not carry these bolts. Got them from B and B aircraft supply. | |||||||||||||||||||||
28 | AN4-16A bolts | 16 | ea | These bolts attach the main landing gear brackets to the fuselage. | ||||||||||||||||||||||
29 | AN960-616 washers | 4 | ea | These washers are used on the AN6-80A bolts (main landing gear attachment bolts). | ||||||||||||||||||||||
30 | AN960-416 washers | 32 | ea | These washers are used to attach the main landing gear bracket to the fuselage. Should be AN960-416 (not -416L like stated in the plans BOM); also, see mod about using AN970-4 instead for the washers on the outside of the fuselage (16 of them). | ||||||||||||||||||||||
31 | AN970-4 | 16 | ea | These washers are extra large washers that are used on the outside fuselage only to attach the landing gear brackets onto the fuselage. Some will have to be grinded down in order to fit. See blog pictures for details. | ||||||||||||||||||||||
32 | MS21042-4 nuts | 16 | ea | These nuts are for the main landing gear brackets to the fuselage. | ||||||||||||||||||||||
33 | AN363-624 nuts | 2 | ea | These nuts are for the AN6-80A main landing gear bolts. | ||||||||||||||||||||||
34 | Glass: | BID | 3 | yd | Already had BID from bulk order - don't know exactly how much was used. | |||||||||||||||||||||
35 | UND | 9 | yd | Already had UNI from bulk order - don't know exactly how much was used. | ||||||||||||||||||||||
36 | Epoxy: | 0.8 | gal | Already had epoxy from bulk order. | ||||||||||||||||||||||
37 | Foam: | 0.8" thick type R45 | 32 | sq. ft. | 4 panels of (32"x48") Divinycell H-45; this is for the fuselage sides. | |||||||||||||||||||||
38 | 1" thick urethane | 3 | sq. ft. | This is to fill the area of the LWX / LWY. You can use leftover R45 instead. | ||||||||||||||||||||||
39 | Wood: | 0.7" x 1" x 104" spruce longerons | 3 | pcs | 2 for the longerons and 1 is to make the LWX and LWY parts. Some of this leftover is used to make F28 dooublers. | |||||||||||||||||||||
40 | 0.4" x 0.7" x 60" spruce stiffener | 2 | pcs | the plans say '5 pcs'; this is wrong. It should be '2 pcs'; this is to make the left and right top longeron stiffeners | ||||||||||||||||||||||
41 | 0.7" x 0.7" triangle spruce 105" long | 2 | pcs | These are for the lower longerons | ||||||||||||||||||||||
42 | 0.7" x 0.7" triangle spruce 48" long | 1 | pcs | This is to make the lower longeron aft stiffeners; ok to have 2 pc 24" each since you will be cutting them in half anyway. | ||||||||||||||||||||||
43 | Metals: | 2" x 2" x 0.25" 6061-T6 extruded 90 angle | 24 | inches | This is to make the main landing gear brackets (see pg 9-3) | |||||||||||||||||||||
44 | Misc: | Alodine solution and alumi prep | 1 | qt | Get a qt kit of alodine solution to bath the landing gear brackets. You should alodine ALL aluminum parts for corrosion resistance. | |||||||||||||||||||||
45 | ||||||||||||||||||||||||||
46 | Chapter 6: Fuselage assembly | |||||||||||||||||||||||||
47 | Prefab parts: | NB nose wheel box cover | Purchased this from Feather Lite ($33) | |||||||||||||||||||||||
48 | Glass: | BID | 6 | yd | This is to cut BID tape strips AND to glass the fuselage floor. I should note that I had to purchase additional BID since ran out halfway through cutting enough fabric to glass the floor. | |||||||||||||||||||||
49 | Epoxy: | 0.4 | gal | Still had epoxy from bulk order - don't know exactly how much was used. | ||||||||||||||||||||||
50 | Foam: | 1.6" thick type R45 | 16 | sq. ft. | This is for the fuselage bottom floor. | |||||||||||||||||||||
51 | Misc: | Custom made clamps | 3 | each | You'll need to purchase some threaded rod, washers and nuts to make 3 large clamps; see blog for details. This is to sandwhich the fuselage sides onto the bulkheads. | |||||||||||||||||||||
52 | ||||||||||||||||||||||||||
53 | Chapter 7: Fuselage exterior | |||||||||||||||||||||||||
54 | Glass: | UND | 14 | yd | I purchased additional UNI to make sure I didn't run out halfway through glassing the exterior of the fuselage. | |||||||||||||||||||||
55 | Epoxy: | 0.85 | gal | I had to purchase EZ poxy for the outside fuselage; since a portion of the outside fuselage is part of the fuel tank. Aeropoxy is NOT fuel resistant so EZ poxy must be used instead. | ||||||||||||||||||||||
56 | Foam: | 1" thick urethane | 1 | sq. ft. | Small amount to fill the foam voids on the outside fuselage where the landing gear attach brackets are. | |||||||||||||||||||||
57 | Misc: | 1/2" flex hose | 4 | ft | This is to implament the conduit mod to be able to route a set of cables from the avionics bay to the leading edge of the strakes. | |||||||||||||||||||||
58 | ||||||||||||||||||||||||||
59 | Chapter 8: Rollover structure and seat belts | |||||||||||||||||||||||||
60 | Prefab parts: | seat belt / shoulder harness assembly | 2 | ea | ||||||||||||||||||||||
61 | Hardware: | AN525-416R16 screws | 8 | ea | These screws are used to bolt the seat belt brackets to the fuselage; plans say 6 but since I am not installing the external foot step, I need a total of 8. | |||||||||||||||||||||
62 | AN960-416 washers | 8 | ea | I used these under the nuts when installing the seat belt hard points / brackets. | ||||||||||||||||||||||
63 | MS21042-4 nuts | 8 | ea | 8 of these are used to install the seat belt brackets to the fuselage. | ||||||||||||||||||||||
64 | Stainless steel t-nut (10/32) | 8 | ea | These get embedded on the outside face of the top longerons so that the rollover structure can be bolted on. | ||||||||||||||||||||||
65 | AN3-?A | 8 | ea | Bolts to mount the rollover structure onto the top longerons | ||||||||||||||||||||||
66 | AN960-10L washers | 8 | ea | Washers for the bolts used to mount the rollover structure. | ||||||||||||||||||||||
67 | Glass: | BID | 2 | yd | You'll need some BID at 45 degree to glass the plywood pucks that go on the lower fuselage longerons where the seat belt hard point brackets get installed. | |||||||||||||||||||||
68 | UNI | To do patch work on the outside top longerons to go over the t-nuts. | ||||||||||||||||||||||||
69 | Epoxy: | 0.1 | gal | To glass the pucks as mentioned above. | ||||||||||||||||||||||
70 | Foam: | 1" thick urethane | 1 | sq. ft. | Small amount to fill the foam holes made to install the t-nuts on the outisde of the top longerons (during rollover bar installation) | |||||||||||||||||||||
71 | Metals: | 1" x 1" x 0.125" 2024-T3 aluminum 90 angle | 8 | inches | This is to make the brackets that attach to the fuselage to attach the seat belts. | |||||||||||||||||||||
72 | 4130 steel tube 1x0.049 3ft | 3 | ft | To make rollover structure - this is for the two aft cross braces | ||||||||||||||||||||||
73 | 4130 steel tube 1-1/8x0.049 3ft | 3 | ft | To make rollover structure - this is for the two tubes that make up the main triangular structure | ||||||||||||||||||||||
74 | 4130 steel tube 1-1/4x0.049 2ft | 2 | ft | To make rollover structure - this is for the two tubes that connect the two angle on the top longerons | ||||||||||||||||||||||
75 | 4130 rect tube 1x1-3/4x0.065 2ft | 2 | ft | To make rollover structure - this is cut into two pieces to get two 'L' angles | ||||||||||||||||||||||
76 | Wood: | scraps of 0.25" thick plywood left over from firewall | N/A | This is to make the pucks that go under the 7 plies of BID where the seat belt brackets attach to. | ||||||||||||||||||||||
77 | ||||||||||||||||||||||||||
78 | Chapter 9: Part 1 (Speed brake) | |||||||||||||||||||||||||
79 | Prefab parts: | Electric actuator - 4" stroke, 115 lb min. thrust | 1 | ea | ServoCity.com | |||||||||||||||||||||
80 | Hardware: | AN25-10R8 screws | 2 | ea | 2 of these go on the outside of the piano hinge that attaches the hinge to the speed brake - the portion outside of LB19. | |||||||||||||||||||||
81 | AN525-10R10 screws | 6 | ea | 2 of these go on the inside of the piano hinge that ataches the hinge to the speed brake - the portion that goes through LB19. 4 of these are used to bolt the actuator attach bracket onto the speed brake flap - goes through LB19. | ||||||||||||||||||||||
82 | AN960-416 washers | 8 | ea | 4 of these go with the screws that bolt the piano hinge to the speed brake flap. 4 of these go with the AN4-5A bolts used to mount the piano hinge onto the fuselage. | ||||||||||||||||||||||
83 | MS21042-3 nuts | 8 | ea | 4 where the piano hinge mates with the speed brake flap, 4 for the actuator bracket mounts with the speed brake flap. | ||||||||||||||||||||||
84 | Stainless steel t-nut (10/32) | 4 | ea | These go on the backside of the 4"x4" puck that goes behind the pilot's seat to attach the actuator bracket. | ||||||||||||||||||||||
85 | AN3-4A bolts | 4 | ea | 4 bolts that mount the actuator bracket to the back of the pilot's seat | ||||||||||||||||||||||
86 | AN960-10L washers | 4 | ea | 4 washers used on the AN3-4A bolts used to mount the actuator bracket onto the pilot's seatback. | ||||||||||||||||||||||
87 | AN4-5A bolts | 4 | ea | 4 bolts to mount the piano hinge onto the fuselage. | ||||||||||||||||||||||
88 | AN3-17 | 2 | ea | Bolts that act as pins for the actuator | ||||||||||||||||||||||
89 | AN310-3 CASTLE NUT | 2 | ea | Nuts for the bolt pins for the actuator | ||||||||||||||||||||||
90 | AN960-416, AN960-416L, AN960-10, AN960-10L | 4 | ea | Washers that act as spacers to center the actuator rods (get a few of each of these; 8+ of each just in case) | ||||||||||||||||||||||
91 | SAE 863 Bronze Sleeve Bearing, for 1/4" Shaft Diameter, 5/16" OD, 3/4" Length | 2 | ea | Sleeve that helps reduce wear and tear on the above AN3-17 bolt (from McMaster Carr) P/N: 2868T44 | ||||||||||||||||||||||
92 | Stainless steel female threaded round standoff 1/4" OD, 1" length, 10-32 | 2 | ea | Spacer that goes through the AN3-17 bolt (from McMaster Carr) P/N: 91125A220 #18-8 | ||||||||||||||||||||||
93 | Glass: | BID | ? | yd | For the speed brake panel and the recess | |||||||||||||||||||||
94 | UND | ? | yd | |||||||||||||||||||||||
95 | Epoxy: | 0.8 | gal | |||||||||||||||||||||||
96 | Foam: | 1" thick urethane (18"x18") | To make the speed brake panel - I had 0.8" thick type R45 leftover so I used that instead of urethane | |||||||||||||||||||||||
97 | Metal: | 2024-T3 aluminum 0.25" thick | 1 | ft | To make 3 (I made 4) LB22 pucks (1"x1" sqaures) that bond behind LB23 - they are tapped and act as nuts where the speed brake hinge gets bolted on to. | |||||||||||||||||||||
98 | 1" x 1" x 0.125" 2024-T3 aluminum 90 angle | 1 | ft | To make the brackets used to attach the linear actuator to the back of the pilot's seat and the speed brake flap | ||||||||||||||||||||||
99 | Wood: | scraps of 0.25" plywood (left over from firewall) | To make the LB23 (8"x2.4"), LB19 (3"x5.6") and the small piece (4"x4") that goes behind the pilot's seat where the electric actuator attaches to. | |||||||||||||||||||||||
100 | Misc: | MS20001-P6 hinge | 8 | inches | To mount the speed brake flap with the fuselage |