Product Information
PRODUCT INFORMATION
 
 
SPC-TM_WG25J
SPEC TEMPLATE MASTER - WING - WG25J
 
 



1 Part#: SPC-TM WG25J   20070101
00003870
2 Dimensions: Please See Note   20070207
00003769
The dimensions of the Wing include the mounting Saddle plus any Ailerons, Flaperons, Flaps or other control surfaces unless otherwise noted. The Aileron Quantity is the number of aileron segments. This is usually 2 with one aileron on the right wing panel plus one aileron on the left wing panel. The Aileron Length is expressed as the length per aileron segment. The Aileron Area is expressed as the total of the area of all aileron segments. Flaperons by design have the same specifications as ailerons. Flap dimensions are denoted in the same manner as ailerons. Flap Quantity is usually 2 (one on the left wing panel plus one on the right wing panel). Flap Length is the length of each flap segment and Flap Area is expressed as the total of the area of all flap segments.
3 Terminology: Please See Note   20070110
00003770
The term "effective" is used to desribe the size of an object which is tapered or irregularly shaped. The term "chord" describes the linear distance from the leading edge to the trailing edge through a wing or control surface. The terms "saddle" and "saddle area" describe that portion of a flying surface such as the center section of a wing or horizontal stabilizer where it intersects the fuselage.
4 Wing General Information 1: na   20061231
00003771
5 Wing General Information 1: na   20061231
00003772
6 Wing Location: Above Fuselage   20061231
00003773
7 Wing Span Tip to Tip: 62.36 in. (1584 mm)   20061231
00003774
8 Wing Span (effective): 61.42 in. (1560 mm)   20070103
00003775
9 Wing Chord at Root: 11.10 in. (282 mm)   20061231
00003776
10 Wing Chord at outboard end of Aileron: 11.42 in. (290 mm)   20061231
00003777
11 Wing Chord (effective): 11.26 in. (286 mm)   20070110
00003778
12 Wing Area: 691.55 sq in. (4461.60 sq cm)   20070110
00003779
13 Wing Width of Saddle: 3.90 in. (99 mm)   20061231
00003780
14 Wing Length of Saddle: 11.18 in. (284 mm)   20061231
00003781
15 Wing Area of Saddle only: 43.58 sq in. (281.16 sq cm)   20061231
00003782
16 Wing Area without Saddle: 647.97 sq in. (4180.44 sq cm)   20070110
00003783
17 Wing Airfoil Shape: Flat Bottom   20061231
00003784
18 Wing Anhedral: na   20070110
00003785
19 Wing Dihedral at Center: 2.3 degrees   20061231
00003786
20 Wing Polyhedral: na   20070110
00003787
21 Wing Taper along Leading Edge: None   20061231
00003788
22 Wing Taper along Trailing Edge: None   20061231
00003789
23 Wing Thickness Maximum: 1.65 in. (42 mm)   20061231
00003790
24 Wing Material: Balsa Wood & Light Plywood. Ribs, Formers and Sheeting are Laser Cut. Sticks, Stringers & Strips are Saw Cut.   20061231
00003791
25 Wing Construction Method: Built Up   20061231
00003792
26 Wing Construction Adhesive: PVA, Cyanoacrylate and Epoxy   20070115
00004268
27 Wing Sheeted Fully: No   20061231
00003793
28 Wing Sheeted Center Section: 8.82 in. (224 mm)   20061231
00003794
29 Wing Sheeted Leading Edge: 4.25 in. (108 mm)   20061231
00003795
30 Wing Sheeted Trailing Edge: .906 in. (23 mm)   20070106
00003796
31 Wing Ribs Capped: Yes   20061231
00003797
32 Wing Plugs In to Fuselage: No   20061231
00003798
33 Wing Front attaches to Fuselage with: Rubber Bands   20061231
00003799
34 Wing Back attaches to Fuselage with: Rubber Bands   20061231
00003800
35 Wing Requires Struts: No   20061231
00003801
36 Wing Spar Joiner Quantity: 1   20070110
00003996
37 Wing Spar Joiner Material: Wood   20070110
00003802
38 Wing Spar Joiner Length: 9.84 in. (250 mm)   20070110
00003803
39 Wing Spar Joiner Width: 1.102 in. (28 mm)   20070110
00003804
40 Wing Spar Joiner Thickness: .354 in. (9 mm)   20070110
00003805
41 Wing Spar Joiner (Secondary) Material: Wood   20070110
00004001
42 Wing Spar Joiner (Secondary) Length: 9.84 in. (250 mm)   20070110
00004002
43 Wing Spar Joiner (Secondary) Width: 1.102 in. (28 mm)   20070110
00004003
44 Wing Spar Joiner (Secondary) Thickness: .354 in. (9 mm)   20070110
00004004
45 Wing Joining Alignment Dowels: Yes 2   20070110
00003806
46 Wing Joint Adhesive: 30 Minute Epoxy   20070110
00003807
47 Wing Joint Trim Tape: Yes Clear   20070110
00003808
48 Wing Ailerons Factory Installed: Yes   20061231
00003809
49 Wing Ailerons Quantity: 2   20061231
00003810
50 Wing Aileron Type: Strip (2)   20061231
00003811
51 Wing Aileron Length per Aileron (effective): 25.91 in. (658 mm)   20070110
00003812
52 Wing Aileron Chord (effective): .000 in. (0 mm)   20070112
00003814
Wing Aileron Chord tapers from ___ mm at the inboard end (closest to the fuselage) to ___ mm at the outboard end.
53 Wing Aileron Area: .00 sq in. (0 sq cm)   20070112
00003815
54 Wing Aileron Area relative to Wing Area: .00 %   20070114
00003816
55 Wing Aileron Area relative to Wing Area without wing saddle: .00 %   20070114
00003817
56 Wing Aileron Hinges per Aileron: 4   20070110
00003818
57 Wing Aileron Hinge Type: Flexible Live Low Gap   20070116
00003819
58 Wing Aileron Hinge Material: Proprietary Super Strong   20070116
00003820
59 Wing Aileron Hinge Adhesive: Cyanoacrylate   20070114
00003821
60 Wing Aileron Hinges Pinned: Yes   20061231
00003822
61 Wing Aileron Servo Required: Yes 1 Standard   20061231
00003823
62 Wing Aileron Servo Location: Center in Wing   20061231
00003824
63 Wing Aileron Servo Rails: Yes in Servo Cavity   20061231
00003825
64 Wing Aileron Servo Cover Plate: na   20070110
00003826
65 Wing Aileron Servo Wiring Tube: Yes   20070110
00004006
66 Wing Ailerons Flaperon Ready with Computer Radio: No   20070103
00003827
67 Wing Flaps Factory Installed: No   20061231
00003828
68 Wing Flaps Mandatory: No   20061231
00003829
69 Wing Flaps Quantity: 0   20061231
00003830
70 Wing Flaps useable as Spoilers or Speed Brakes by deflecting upwards: No, Downwards deflection only   20070426
00003831
71 Wing Flap Length per Flap (effective): .00 in. ( mm)   20070110
00003832
72 Wing Flap Chord (effective): .000 in. (0 mm)   20070112
00003834
Wing Flap Chord tapers from ___ mm at the inboard end (closest to the fuselage) to ___ mm at the outboard end.
73 Wing Flaps Area: .00 sq in. (0 sq cm)   20070112
00003835
74 Wing Flap Area relative to Wing Area: .00 %   20070114
00003836
75 Wing Flap Area relative to Wing Area without wing saddle: .00 %   20070114
00003837
76 Wing Flap Hinges per Flap: 3   20070110
00003838
77 Wing Flap Hinge Type: Flexible Live Low Gap   20070116
00003839
78 Wing Flap Hinge Material: Proprietary Super Strong   20070116
00003840
79 Wing Flaps Hinge Adhesive: Cyanoacrylate   20070114
00003841
80 Wing Flap Hinges Pinned: Yes   20061231
00003842
81 Wing Flap Servo Required: Yes 1 Standard   20061231
00003843
82 Wing Flap Servo Location: Outboard in bottom of each wing panel in proximity of Flap   20061231
00003844
83 Wing Flap Servo Rails: Yes in Servo Cavity   20061231
00003845
84 Wing Flap Servo Cover Plate: na   20070110
00003846
85 Wing Flap Servo Wiring Tube: Yes   20070110
00004007
86 Wing Hatches: na   20070110
00004005
87 Wing Color Top Schema: Stylized Name and POLYCOTE logo   20061231
00003847
88 Wing Color Top Main: Red Center and Orange Diagonal Band or Dark Blue Center Light Blue Diagonal Band   20061231
00003848
89 Wing Color Top Trim: Black and White   20061231
00003849
90 Wing Color Top Lines: Gray   20061231
00003850
91 Wing Color Top Rivets: Gray   20061231
00003851
92 Wing Color Top vs Bottom: Very Different   20061231
00003852
93 Wing Color Bottom Schema: Plain   20061231
00003853
94 Wing Color Bottom Main: Yellow   20061231
00003854
95 Wing Color Bottom Trim: All Yellow   20061231
00003855
96 Wing Color Bottom Lines: Gray   20061231
00003856
97 Wing Color Bottom Rivets: Gray   20061231
00003857
98 Wing Weight: 2200.00 lbs (999999 g). Please See Note   20070106
00003858
The weight of the Wing is as it was when it is removed from the shipping box. This weight does NOT include the weight associated with any adhesives, spar joiners or other weight associated with end user assembly.
99 Wing More Information 1: na   20061231
00003859
100 Wing More Information 2: na   20061231
00003860
101 Wing More Information 3: na   20061231
00003861

20110315 14:53:39 PST. Subject to Change Without Notice.
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