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www.richmondrc.com > Consumers > Canada - $CDN > VMAR SPARE PARTS > CUB 09-15 ELEC_C210Y YELLOW

VMAR PARTS FIT RIGHT! FLY RIGHT! STOCK UP NOW!    > VMAR J3 CUB 09-15 ARF ECS - TAIL VERT - YELLOW
VMAR J3 CUB 09-15 ARF ECS - TAIL VERT - YELLOW

VMAR J3 CUB 09-15 ARF ECS - TAIL VERT - YELLOW

$10.99
Part # VMA-C210YTV (rn_cr)
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    PRODUCT INFORMATION
     
     
    VMA-C210YTV
    VMAR J3 CUB 09-15 ARF ECS - TAIL VERT - YELLOW
     
     



    1 Part#: VMA-C210YTV   20080115
    00012176
    6 Source Data - Horiz Stabilizer Elevator Area: 41.60 sq in. (268 sq cm)   20070506
    00012181
    7 Dimensions: Please See Note   20070505
    00012182
    The dimensions of the Vertical Stabilizer include the Rudder unless otherwise noted. The Rudder Quantity is the number of rudder segments. This is usually 1 and occasionally 2. i.e. 1 for 1 rudder, 2 for 2 rudders in the case of two vertical stabilizers on one model. The Rudder Length is expressed as the length per rudder segment. The Rudder area is expressed as the total of the area of all rudder segments.
    8 Terminology: Please See Note   20070505
    00012183
    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.
    11 Vertical Stabilizer Location: Vertical Slot in Top of aft end of Fuselage   20070505
    00012186
    12 Vertical Stabilizer Quantity: 1   20070505
    00012187
    13 Vertical Stabilizer Height Fuse to End Of Tip: 5.55 in. (141 mm)   20070503
    00012188
    14 Vertical Stabilizer Height (effective): 3.15 in. (80 mm)   20070503
    00012189
    15 Vertical Stabilizer Chord Maximum: 6.50 in. (165 mm)   20070503
    00012190
    16 Vertical Stabilizer Chord at tip end of Rudder: 2.68 in. (68 mm)   20070503
    00012191
    17 Vertical Stabilizer Chord (effective): 4.92 in. (125 mm)   20070503
    00012192
    18 Vertical Stabilizer Area: 15.50 sq in. (100.00 sq cm)   20070503
    00012193
    19 Vertical Stabilizer Area relative to Wing Area: 3.93 %   20070506
    00012194
    20 Vertical Stabilizer Area relative to Wing Area without wing saddle: 4.19 %   20070506
    00012195
    21 Vertical Stabilizer Airfoil Shape: Slab   20070503
    00012196
    22 Vertical Stabilizer Thickness Maximum: .169 in. (4.3 mm)   20070503
    00012197
    23 Vertical Stabilizer Taper along Leading Edge: Yes   20070503
    00012198
    24 Vertical Stabilizer Taper along Trailing Edge: Yes. Rounded   20070503
    00012199
    25 Vertical Stabilizer Material: Balsa Wood & Light Plywood. Ribs, Formers and Sheeting are Laser Cut. Sticks, Stringers & Strips are Saw Cut.   20070503
    00012200
    26 Vertical Stabilizer Construction Method: Built Up   20070503
    00012201
    27 Vertical Stabilizer Construction Adhesive: PVA, Cyanoacrylate and Epoxy   20070503
    00012202
    28 Vertical Stabilizer Sheeted Fully: No   20070503
    00012203
    32 Vertical Stabilizer Attaches to Fuselage via: Slot in Fuselage and Adhesive   20070505
    00012207
    33 Vertical Stabilizer Adhesive Required: 30 Minute Epoxy   20070505
    00012208
    34 Vertical Stabilizer Requires Struts: No   20070505
    00012209
    35 Vertical Stabilizer Rudder Factory Installed: Yes   20070505
    00012210
    36 Vertical Stabilizer Rudder Quantity: 1 (i.e. not split, not dual rudders)   20070505
    00012211
    37 Vertical Stabilizer Rudder Length (effective): 5.91 in. (150 mm)   20070503
    00012212
    Vertical Stabilizer Rudder Length is 196 mm at the hinge line. The Rudder Length is rounded at the trailing edge.
    38 Vertical Stabilizer Rudder Chord (effective): 1.97 in. (50 mm)   20070503
    00012213
    The Vertical Stablizer Rudder Chord varies continuously due to rounded edges throughout.
    39 Vertical Stabilizer Rudder Area: 11.63 sq in. (75.00 sq cm)   20070503
    00012214
    40 Vertical Stabilizer Rudder Area relative to Wing Area: 2.94 %   20070506
    00012215
    41 Vertical Stabilizer Rudder Area relative to Wing Area without wing saddle: 3.14 %   20070506
    00012216
    42 Vertical Stabilizer Rudder Area relative to Vertical Stabilizer Area: 75.00 %   20070503
    00012217
    43 Vertical Stabilizer Rudder Area relative to Horiz Stabilizer Area: 15.79 %   20070507
    00012218
    44 Vertical Stabilizer Rudder Area relative to Horizontal Stabilizer Area without saddle: 16.42 %   20070507
    00012219
    45 Vertical Stabilizer Rudder Area relative to Horiz Stabilizer Elevator Area: 27.94 %   20070506
    00012220
    46 Vertical Stabilizer Rudder Hinges per Rudder: 2   20070503
    00012221
    47 Vertical Stabilizer Rudder Hinge Type: Flexible Live Low Gap   20070503
    00012222
    48 Vertical Stabilizer Rudder Hinge Material: Proprietary Super Strong   20070503
    00012223
    49 Vertical Stabilizer Rudder Hinge Adhesive: Cyanoacrylate   20070503
    00012224
    51 Vertical Stabilizer Rudder Servo Required: Yes 1 Standard   20070503
    00012226
    52 Vertical Stabilizer Rudder Servo Location: Tray in centre of fuselage   20070503
    00012227
    20070503/19:31/
    53 Vertical Stabilizer Rudder Servo Mounting Method: Tray   20070505
    00012228
    58 Vertical Stabilizer Color Left Schema: Monochrome with small Cub graphic   20070503
    00012233
    59 Vertical Stabilizer Color Left Main: Yellow   20070503
    00012234
    60 Vertical Stabilizer Color Left Trim: Red & Brown Cub graphic   20070503
    00012235
    63 Vertical Stabilizer Color Left vs Right: Similar   20070503
    00012238
    64 Vertical Stabilizer Color Right Schema: Monochrome with small Cub graphic   20070503
    00012239
    65 Vertical Stabilizer Color Right Main: Yellow   20070503
    00012240
    66 Vertical Stabilizer Color Right Trim: Red & Brown Cub graphic   20070503
    00012241
    69 Vertical Stabilizer Weight: .022 lbs (10 g)   20070503
    00012244

    20120828 04:08:08 PST. Subject to Change Without Notice.
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