Product Information
PRODUCT INFORMATION
 
 
VMA-F690NW
VMAR F18 HORNET 60-91 ARF - WING - NAVY
 
 



1 Part#: VMA-F690NW   20070222
00004009
2 Dimensions: Please See Note   20070207
00004010
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
00004011
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   20070110
00004012
5 Wing General Information 1: na   20070110
00004013
6 Wing Location: Attached to sides of Fuselage   20070110
00004014
7 Wing Span Tip to Tip: 57.24 in. (1454 mm)   20070110
00004015
8 Wing Span (effective): 57.24 in. (1454 mm)   20070110
00004016
9 Wing Chord at Root: 17.56 in. (446 mm)   20070110
00004017
10 Wing Chord at outboard end of Aileron: 8.31 in. (211 mm)   20070110
00004018
11 Wing Chord (effective): 12.93 in. (329 mm)   20070110
00004019
12 Wing Area: 740.34 sq in. (4776.39 sq cm)   20070110
00004020
13 Wing Width of Saddle: 9.53 in. (242 mm)   20070110
00004021
14 Wing Length of Saddle: 17.56 in. (446 mm)   20070110
00004022
15 Wing Area of Saddle only: 167.29 sq in. (1079.32 sq cm)   20070110
00004023
16 Wing Area without Saddle: 573.05 sq in. (3697.07 sq cm)   20070110
00004024
17 Wing Airfoil Shape: Symmetrical   20070110
00004025
18 Wing Anhedral: na   20070110
00004026
19 Wing Dihedral at Center: 0 degrees   20070110
00004027
20 Wing Polyhedral: na   20070110
00004028
21 Wing Taper along Leading Edge: Yes   20070110
00004029
22 Wing Taper Along Trailing Edge: Yes   20070110
00004030
23 Wing Thickness Maximum: 1.81 in. (46 mm)   20070110
00004031
24 Wing Material: Balsa Wood & Light Plywood. Ribs, Formers and Sheeting are Laser Cut. Sticks, Stringers & Strips are Saw Cut.   20070110
00004032
25 Wing Construction Method: Built Up   20070110
00004033
26 Wing Construction Adhesive: PVA, Cyanoacrylate and Epoxy   20070115
00004272
27 Wing Sheeted Fully: Yes   20070110
00004034
28 Wing Sheeted Center Section: .00 in. (0 mm)   20070110
00004035
29 Wing Sheeted Leading Edge: .00 in. (0 mm)   20070110
00004036
30 Wing Sheeted Trailing Edge: .000 in. (0 mm)   20070110
00004037
31 Wing Ribs Capped: na   20070110
00004038
32 Wing Plugs In to Fuselage: Yes   20070110
00004039
33 Wing Front attaches to Fuselage with: Bolt, Washer & Nut   20070110
00004040
34 Wing Back attaches to Fuselage with: Bolt, Washer & Nut   20070110
00004041
35 Wing Requires Struts: No   20070110
00004042
36 Wing Spar Joiner Quantity: 2   20070110
00004043
37 Wing Spar Joiner Material: Aluminum Tube   20070110
00004044
38 Wing Spar Joiner Length: 26.77 in. (680 mm)   20070110
00004045
39 Wing Spar Joiner Width: .576 in. (14.63 mm)   20070110
00004046
40 Wing Spar Joiner Thickness: .000 in. (0 mm)   20070110
00004047
41 Wing Spar Joiner (Secondary) Material: Aluminum Tube   20070110
00004048
42 Wing Spar Joiner (Secondary) Length: 20.87 in. (530 mm)   20070110
00004049
43 Wing Spar Joiner (Secondary) Width: .576 in. (14.63 mm)   20070110
00004050
44 Wing Spar Joiner (Secondary) Thickness: .000 in. (0 mm)   20070110
00004051
45 Wing Joining Alignment Dowels: na   20070110
00004052
46 Wing Joint Adhesive: na   20070110
00004053
47 Wing Joint Trim Tape: na   20070110
00004054
48 Wing Ailerons Factory Installed: Yes   20070110
00004055
49 Wing Ailerons Quantity: 2   20070110
00004056
50 Wing Aileron Type: Semi-Strip (2)   20070110
00004057
51 Wing Aileron Length per Aileron (effective): 9.80 in. (249 mm)   20070110
00004058
52 Wing Aileron Chord (effective): 2.421 in. (62 mm)   20070112
00004059
Wing Aileron Chord tapers from 71 mm at the inboard end (closest to the fuselage) to 52 mm at the outboard end.
53 Wing Aileron Area: 47.47 sq in. (306 sq cm)   20070112
00004060
54 Wing Aileron Area relative to Wing Area: 6.41 %   20070114
00004061
55 Wing Aileron Area relative to Wing Area without wing saddle: 8.28 %   20070114
00004062
56 Wing Aileron Hinges per Aileron: 3   20070110
00004063
57 Wing Aileron Hinge Type: Flexible Live Low Gap   20070116
00004064
58 Wing Aileron Hinge Material: Proprietary Super Strong   20070116
00004065
59 Wing Aileron Hinge Adhesive: Cyanoacrylate   20070114
00004066
60 Wing Aileron Hinges Pinned: Yes   20070110
00004067
61 Wing Aileron Servo Required: Yes 2 Standard   20070110
00004068
62 Wing Aileron Servo Location: Bottom of Wing aligned approximately with the inboard end of the aileron.   20070110
00004069
63 Wing Aileron Servo Rails: Yes in Servo Cavity   20070110
00004070
64 Wing Aileron Servo Cover Plate: na   20070110
00004071
65 Wing Aileron Servo Wiring Tube: Yes   20070110
00004072
66 Wing Ailerons Flaperon Ready with Computer Radio: Yes   20070110
00004073
67 Wing Flaps Factory Installed: Yes   20070110
00004074
68 Wing Flaps Mandatory: No. Can be locked at neutral position   20070110
00004075
69 Wing Flaps Quantity: 2   20070110
00004076
70 Wing Flaps useable as Spoilers or Speed Brakes by deflecting upwards: No   20070426
00004077
71 Wing Flap Length per Flap (effective): 12.60 in. (320 mm)   20070110
00004078
72 Wing Flap Chord (effective): 3.307 in. (84 mm)   20070112
00004079
Wing Flap Chord tapers from 73 mm at the inboard end (closest to the fuselage) to 95 mm at the outboard end.
73 Wing Flaps Area: 83.33 sq in. (538 sq cm)   20070112
00004080
74 Wing Flap Area relative to Wing Area: 11.26 %   20070114
00004081
75 Wing Flap Area relative to Wing Area without wing saddle: 14.54 %   20070114
00004082
76 Wing Flap Hinges per Flap: 3   20070110
00004083
77 Wing Flap Hinge Type: Flexible Live Low Gap   20070116
00004084
78 Wing Flap Hinge Material: Proprietary Super Strong   20070116
00004085
79 Wing Flaps Hinge Adhesive: Cyanoacrylate   20070114
00004086
80 Wing Flap Hinges Pinned: Yes   20070110
00004087
81 Wing Flap Servo Required: Yes 2 Standard   20070110
00004088
82 Wing Flap Servo Location: Bottom of Wing aligned approximately with the inboard end of the flap   20070110
00004089
83 Wing Flap Servo Rails: Yes in Servo Cavity   20070110
00004090
84 Wing Flap Servo Cover Plate: na   20070110
00004091
85 Wing Flap Servo Wiring Tube: Yes   20070110
00004092
86 Wing Hatches: na   20070110
00004093
87 Wing Color Top Schema: US Navy Gray   20070110
00004094
88 Wing Color Top Main: Gray   20070110
00004095
89 Wing Color Top Trim: Single Stars and Bars (Red, White and Blue) Left   20070110
00004096
90 Wing Color Top Lines: Black   20070110
00004097
91 Wing Color Top Rivets: Gray 3D and Black graphics   20070110
00004098
92 Wing Color Top vs Bottom: Different   20070110
00004099
93 Wing Color Bottom Schema: US Navy White   20070110
00004100
94 Wing Color Bottom Main: White   20070110
00004101
95 Wing Color Bottom Trim: Single Stars and Bars (Red, White and Blue) Right   20070110
00004102
96 Wing Color Bottom Lines: Black   20070110
00004103
97 Wing Color Bottom Rivets: Gray 3D and Black graphics   20070110
00004104
98 Wing Weight: 1.49 lbs (676 g). Please See Note   20070110
00004105
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   20070110
00004106
100 Wing More Information 2: na   20070110
00004107
101 Wing More Information 3: na   20070110
00004108

20110315 15:09:26 PST. Subject to Change Without Notice.
Copyright Richmond RC Supply Ltd. VMA-F690NW_spec.htm