| 1 | Part#: | VMA-F590UW |
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| 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: | Attached to sides of Fuselage |
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| 7 | Wing Span Tip to Tip: | 55.59 in. (1412 mm) |
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| 8 | Wing Span (effective): | 55.59 in. (1412 mm) |
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| 9 | Wing Chord at Root: | 16.38 in. (416 mm) |
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| The Wing Chord at Root was measured without considering the wing fairings that extend forward from the leading edge in the vicinity of the wing root. | |||
| 10 | Wing Chord at outboard end of Aileron: | 7.68 in. (195 mm) |
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| 11 | Wing Chord (effective): | 12.03 in. (306 mm) |
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| 12 | Wing Area: | 668.62 sq in. (4313.66 sq cm) |
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| 13 | Wing Width of Saddle (Effective): | 8.67 in. (220 mm) |
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| The Wing Saddle has an "Hourglass" shape. The saddle is 231 mm wide at the forward and aft ends. The saddle narrows to 199 mm in width at the midway point. | |||
| 14 | Wing Length of Saddle: | 16.54 in. (420 mm) |
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| 15 | Wing Area of Saddle only: | 143.44 sq in. (925.40 sq cm) |
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| 16 | Wing Area without Saddle: | 525.18 sq in. (3388.26 sq cm) |
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| 17 | Wing Airfoil Shape: | Symmetrical |
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| 19 | Wing Dihedral at Center: | 0 degrees |
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| 21 | Wing Taper along Leading Edge: | Yes |
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| 22 | Wing Taper Along Trailing Edge: | Yes |
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| 23 | Wing Thickness Maximum: | 2.24 in. (57 mm) |
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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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| 27 | Wing Sheeted Fully: | Yes |
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| 32 | Wing Plugs In to Fuselage: | No. This is a "one piece" wing. |
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| 33 | Wing Front attaches to Fuselage with: | Wood dowel in leading edge of wing |
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| 34 | Wing Back attaches to Fuselage with: | 2 nylon bolts |
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| 35 | Wing Requires Struts: | No |
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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: | Semi-Strip (2) |
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| 51 | Wing Aileron Length per Aileron (effective): | 11.22 in. (285 mm) |
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| 52 | Wing Aileron Chord (effective): | 2.539 in. (65 mm) |
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| Wing Aileron Chord tapers from 76 mm at the inboard end (closest to the fuselage) to 53 mm at the outboard end. | |||
| 53 | Wing Aileron Area: | 56.99 sq in. (368 sq cm) |
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| 54 | Wing Aileron Area relative to Wing Area: | 8.52 % |
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| 55 | Wing Aileron Area relative to Wing Area without wing saddle: | 10.85 % |
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| 56 | Wing Aileron Hinges per Aileron: | 3 |
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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 Standard |
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| 62 | Wing Aileron Servo Location: | Bottom of Wing aligned approximately 30% outboard from inboard end of aileron |
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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: | Yes |
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| 68 | Wing Flaps Mandatory: | No. Can be locked at neutral position |
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| 69 | Wing Flaps Quantity: | 2 |
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| 70 | Wing Flaps useable as Spoilers or Speed Brakes by deflecting upwards: | Yes |
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| 71 | Wing Flap Length per Flap (effective): | 9.29 in. (236 mm) |
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| 72 | Wing Flap Chord (effective): | 3.130 in. (80 mm) |
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| Wing Flap Chord tapers from 90 mm at the inboard end (closest to the fuselage) to 69 mm at the outboard end. | |||
| 73 | Wing Flaps Area: | 58.16 sq in. (375 sq cm) |
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| 74 | Wing Flap Area relative to Wing Area: | 8.70 % |
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| 75 | Wing Flap Area relative to Wing Area without wing saddle: | 11.07 % |
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| 76 | Wing Flap Hinges per Flap: | 2 |
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| 77 | Wing Flap Hinge Type: | Flexible Live Low Gap |
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| 78 | Wing Flap Hinge Material: | Proprietary Super Strong |
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| 79 | Wing Flaps Hinge Adhesive: | Cyanoacrylate |
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| 80 | Wing Flap Hinges Pinned: | Yes |
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| 81 | Wing Flap Servo Required: | Yes 2 Standard |
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| 82 | Wing Flap Servo Location: | Bottom of Wing aligned approximately with the inboard end of the flap |
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| 83 | Wing Flap Servo Rails: | Yes in Servo Cavity |
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| 85 | Wing Flap Servo Wiring Tube: | Yes |
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| 87 | Wing Color Top Schema: | Camoflage |
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| 88 | Wing Color Top Main: | Khaki and Olive Drab |
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| 89 | Wing Color Top Trim: | Single Stars and Bars (Red, White and Blue) Left US AIR FORCE text Right |
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| 90 | Wing Color Top Lines: | Gray |
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| 91 | Wing Color Top Rivets: | 3D Khaki and Olive Drab |
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| 92 | Wing Color Top vs Bottom: | Different |
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| 93 | Wing Color Bottom Schema: | Single Color with Small Elements |
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| 94 | Wing Color Bottom Main: | Khaki |
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| 95 | Wing Color Bottom Trim: | Single Stars and Bars (Red, White and Blue) Left. US AIRFORCE text Right |
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| 96 | Wing Color Bottom Lines: | Gray |
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| 97 | Wing Color Bottom Rivets: | 3D Khaki |
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| 98 | Wing Weight: | 1.64 lbs (745 g). Please See Note |
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| 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. | |||