| 1 | Part#: | VMA-T210WW |
20090716 00010709 |
| 2 | Dimensions: | Please See Note |
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| 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 |
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| 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. | |||
| 6 | Wing Location: | Above Fuselage |
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| 7 | Wing Span Tip to Tip: | 61.34 in. (1558 mm) |
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| 8 | Wing Span (effective): | 61.34 in. (1558 mm) |
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| 9 | Wing Chord at Root: | 7.00 in. (177.8 mm) |
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| 10 | Wing Chord at outboard end of Aileron: | 7.00 in. (177.8 mm) |
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| 11 | Wing Chord (effective): | 7.00 in. (177.8 mm) |
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| 12 | Wing Area: | 429.37 sq in. (2770.12 sq cm) |
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| 16 | Wing Area without Saddle: | 429.37 sq in. (2770.12 sq cm) |
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| 17 | Wing Airfoil Shape: | Semi Symmetrical |
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| 21 | Wing Taper along Leading Edge: | None |
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| 22 | Wing Taper along Trailing Edge: | None |
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| 24 | Wing Material: | Balsa Wood & Light Plywood. Ribs, Formers and Sheeting are Laser Cut. Sticks, Stringers & Strips are Saw Cut. |
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| 25 | Wing Construction Method: | Built Up |
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| 26 | Wing Construction Adhesive: | PVA, Cyanoacrylate and Epoxy |
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| 31 | Wing Ribs Capped: | Yes |
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| 32 | Wing Plugs In to Fuselage: | No |
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| 35 | Wing Requires Struts: | Yes |
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| 36 | Wing Spar Joiner Quantity: | 1 (Please See Note) |
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| In some markets the wing halves have been joined by the factory and the wing then shipped in one piece. Where a one piece wing has been supplied, the individual wing halves, wing spar joiner(s), alignment pins, center joint trim tape and other components used to join wing halves together have already been incorporated by the factory into the one piece wing. | |||
| 37 | Wing Spar Joiner Material: | Wood |
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| 46 | Wing Joint Adhesive: | 30 Minute Epoxy |
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| 47 | Wing Joint Trim Tape: | Yes Clear |
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| 48 | Wing Ailerons Factory Installed: | Yes |
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| 49 | Wing Ailerons Quantity: | 2 |
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| 50 | Wing Aileron Type: | Strip (2) |
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| 57 | Wing Aileron Hinge Type: | Flexible Live Low Gap |
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| 58 | Wing Aileron Hinge Material: | Proprietary Super Strong |
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| 59 | Wing Aileron Hinge Adhesive: | Cyanoacrylate |
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| 60 | Wing Aileron Hinges Pinned: | Yes |
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| 61 | Wing Aileron Servo Required: | Yes 2 Sub-micro |
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| 62 | Wing Aileron Servo Location: | Near motor nacelles outboard in Wing |
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| 63 | Wing Aileron Servo Rails: | Yes in Servo Cavity |
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| 65 | Wing Aileron Servo Wiring Tube: | Yes |
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| 66 | Wing Ailerons Flaperon Ready with Computer Radio: | Yes |
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| 67 | Wing Flaps Factory Installed: | No |
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