| 1 | Part#: | VMA-T210WW |
20090716 00010709 |
| 2 | Dimensions: | Please See Note |
20070426 00010710 |
| 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 |
20070426 00010711 |
| 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 |
20070426 00010712 |
| 5 | Wing General Information 1: | na |
20070426 00010713 |
| 6 | Wing Location: | Above Fuselage |
20070426 00010714 |
| 7 | Wing Span Tip to Tip: | 61.34 in. (1558 mm) |
20070426 00010715 |
| 8 | Wing Span (effective): | 61.34 in. (1558 mm) |
20070426 00010716 |
| 9 | Wing Chord at Root: | 7.00 in. (177.8 mm) |
20070426 00010717 |
| 10 | Wing Chord at outboard end of Aileron: | 7.00 in. (177.8 mm) |
20070426 00010718 |
| 11 | Wing Chord (effective): | 7.00 in. (177.8 mm) |
20070426 00010719 |
| 12 | Wing Area: | 429.37 sq in. (2770.12 sq cm) |
20070426 00010720 |
| 13 | Wing Width of Saddle: | .00 in. (.00 mm) |
20070426 00010721 |
| 14 | Wing Length of Saddle: | .00 in. (.00 mm) |
20070426 00010722 |
| 15 | Wing Area of Saddle only: | .00 sq in. (.00 sq cm) |
20070426 00010723 |
| 16 | Wing Area without Saddle: | 429.37 sq in. (2770.12 sq cm) |
20070426 00010724 |
| 17 | Wing Airfoil Shape: | Semi Symmetrical |
20070429 00010725 |
| 18 | Wing Anhedral: | na |
20070426 00010726 |
| 19 | Wing Dihedral at Center: | .00 degrees |
20070426 00010727 |
| 20 | Wing Polyhedral: | na |
20070426 00010728 |
| 21 | Wing Taper along Leading Edge: | None |
20070426 00010729 |
| 22 | Wing Taper along Trailing Edge: | None |
20070426 00010730 |
| 23 | Wing Thickness Maximum: | .00 in. (.00 mm) |
20070426 00010731 |
| 24 | Wing Material: | Balsa Wood & Light Plywood. Ribs, Formers and Sheeting are Laser Cut. Sticks, Stringers & Strips are Saw Cut. |
20070426 00010732 |
| 25 | Wing Construction Method: | Built Up |
20070426 00010733 |
| 26 | Wing Construction Adhesive: | PVA, Cyanoacrylate and Epoxy |
20070426 00010734 |
| 27 | Wing Sheeted Fully: | na |
20070426 00010735 |
| 28 | Wing Sheeted Center Section: | .00 in. (.00 mm) |
20070426 00010736 |
| 29 | Wing Sheeted Leading Edge: | .00 in. (.00 mm) |
20070426 00010737 |
| 30 | Wing Sheeted Trailing Edge: | .000 in. (.00 mm) |
20070426 00010738 |
| 31 | Wing Ribs Capped: | Yes |
20070426 00010739 |
| 32 | Wing Plugs In to Fuselage: | No |
20070426 00010740 |
| 33 | Wing Front attaches to Fuselage with: | na |
20070426 00010741 |
| 34 | Wing Back attaches to Fuselage with: | na |
20070426 00010742 |
| 35 | Wing Requires Struts: | Yes |
20070426 00010743 |
| 36 | Wing Spar Joiner Quantity: | 1 (Please See Note) |
20070428 00010744 |
| 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 |
20070426 00010745 |
| 38 | Wing Spar Joiner Length: | .00 in. (.00 mm) |
20070426 00010746 |
| 39 | Wing Spar Joiner Width: | .000 in. (.00 mm) |
20070426 00010747 |
| 40 | Wing Spar Joiner Thickness: | .000 in. (.00 mm) |
20070426 00010748 |
| 41 | Wing Spar Joiner (Secondary) Material: | na |
20070426 00010749 |
| 42 | Wing Spar Joiner (Secondary) Length: | .00 in. (.00 mm) |
20070426 00010750 |
| 43 | Wing Spar Joiner (Secondary) Width: | .000 in. (.00 mm) |
20070426 00010751 |
| 44 | Wing Spar Joiner (Secondary) Thickness: | .000 in. (.00 mm) |
20070426 00010752 |
| 45 | Wing Joining Alignment Dowels: | na |
20070426 00010753 |
| 46 | Wing Joint Adhesive: | 30 Minute Epoxy |
20070426 00010754 |
| 47 | Wing Joint Trim Tape: | Yes Clear |
20070426 00010755 |
| 48 | Wing Ailerons Factory Installed: | Yes |
20070426 00010756 |
| 49 | Wing Ailerons Quantity: | 2 |
20070426 00010757 |
| 50 | Wing Aileron Type: | Strip (2) |
20070426 00010758 |
| 51 | Wing Aileron Length per Aileron (effective): | .00 in. (.00 mm) |
20070426 00010759 |
| 52 | Wing Aileron Chord (effective): | .000 in. (0 mm) |
20070426 00010760 |
| 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. (.00 sq cm) |
20070426 00010761 |
| 54 | Wing Aileron Area relative to Wing Area: | .00 % |
20070426 00010762 |
| 55 | Wing Aileron Area relative to Wing Area without wing saddle: | .00 % |
20070426 00010763 |
| 56 | Wing Aileron Hinges per Aileron: | na |
20070426 00010764 |
| 57 | Wing Aileron Hinge Type: | Flexible Live Low Gap |
20070426 00010765 |
| 58 | Wing Aileron Hinge Material: | Proprietary Super Strong |
20070426 00010766 |
| 59 | Wing Aileron Hinge Adhesive: | Cyanoacrylate |
20070426 00010767 |
| 60 | Wing Aileron Hinges Pinned: | Yes |
20070426 00010768 |
| 61 | Wing Aileron Servo Required: | Yes 2 Sub-micro |
20070426 00010769 |
| 62 | Wing Aileron Servo Location: | Near motor nacelles outboard in Wing |
20070426 00010770 |
| 63 | Wing Aileron Servo Rails: | Yes in Servo Cavity |
20070426 00010771 |
| 64 | Wing Aileron Servo Cover Plate: | na |
20070426 00010772 |
| 65 | Wing Aileron Servo Wiring Tube: | Yes |
20070426 00010773 |
| 66 | Wing Ailerons Flaperon Ready with Computer Radio: | Yes |
20070426 00010774 |
| 67 | Wing Flaps Factory Installed: | No |
20070428 00010775 |
| 68 | Wing Flaps Mandatory: | na |
20070428 00010776 |
| 69 | Wing Flaps Quantity: | .00 |
20070428 00010777 |
| 70 | Wing Flaps useable as Spoilers or Speed Brakes by deflecting upwards: | na |
20070428 00010778 |
| 71 | Wing Flap Length per Flap (effective): | .00 in. ( mm) |
20070428 00010779 |
| 72 | Wing Flap Chord (effective): | .000 in. (0 mm) |
20070428 00010780 |
| 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. (.00 sq cm) |
20070428 00010781 |
| 74 | Wing Flap Area relative to Wing Area: | .00 % |
20070428 00010782 |
| 75 | Wing Flap Area relative to Wing Area without wing saddle: | .00 % |
20070428 00010783 |
| 76 | Wing Flap Hinges per Flap: | na |
20070428 00010784 |
| 77 | Wing Flap Hinge Type: | Flexible Live Low Gap |
20070428 00010785 |
| 78 | Wing Flap Hinge Material: | Proprietary Super Strong |
20070428 00010786 |
| 79 | Wing Flaps Hinge Adhesive: | Cyanoacrylate |
20070428 00010787 |
| 80 | Wing Flap Hinges Pinned: | Yes |
20070428 00010788 |
| 81 | Wing Flap Servo Required: | Yes 1 Standard |
20070428 00010789 |
| 82 | Wing Flap Servo Location: | Outboard in bottom of each wing panel in proximity of Flap |
20070428 00010790 |
| 83 | Wing Flap Servo Rails: | Yes in Servo Cavity |
20070428 00010791 |
| 84 | Wing Flap Servo Cover Plate: | na |
20070428 00010792 |
| 85 | Wing Flap Servo Wiring Tube: | Yes |
20070428 00010793 |
| 86 | Wing Hatches: | na |
20070428 00010794 |
| 87 | Wing Color Top Schema: | na |
20070428 00010795 |
| 88 | Wing Color Top Main: | na |
20070426 00010796 |
| 89 | Wing Color Top Trim: | na |
20070426 00010797 |
| 90 | Wing Color Top Lines: | na |
20070426 00010798 |
| 91 | Wing Color Top Rivets: | na |
20070426 00010799 |
| 92 | Wing Color Top vs Bottom: | na |
20070426 00010800 |
| 93 | Wing Color Bottom Schema: | na |
20070426 00010801 |
| 94 | Wing Color Bottom Main: | na |
20070426 00010802 |
| 95 | Wing Color Bottom Trim: | na |
20070426 00010803 |
| 96 | Wing Color Bottom Lines: | na |
20070426 00010804 |
| 97 | Wing Color Bottom Rivets: | na |
20070426 00010805 |
| 98 | Wing Weight: | .00 lbs (.00 g). Please See Note |
20070426 00010806 |
| 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 |
20070426 00010807 |
| 100 | Wing More Information 2: | na |
20070426 00010808 |
| 101 | Wing More Information 3: | na |
20070426 00010809 |