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Tail construction – Carl Goldberg GBGA1089 User Manual

Page 7

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7

TAIL CONSTRUCTION

* Collect the following items
(2) Right & left Stab
(1) 10mm x 182mm front stabilizer tube
(1) 10mm x 312mm Rear Stabilizer tube
(2) 4-40 x 3/8 Socket head screw

1.

Slide the short stabilizer tube into the front

hole and long stabilizer tube in the rear hole of

one side of the stab. Then slide the assembly

into the holes in the fuselage till the stab is

flush against the fuse. (The side of the stab

with the hole is the top of the stabilizer). Slide

the second stab onto the tubes sticking out

the other side of the fuselage. Squeeze both

stab pieces together firmly on to the fuselage.

Check that the stabilizer is level with the wing.

Shim the tube in the fuselage up or down if

necessary. Do not go any farther till the stab is

level to the wing.

2.

Using 4-40 x 3/8” bolt, drill and tap the stabi-

lizer tube at both hole locations. This method

will allow you to remove the stab as needed.

Remember to keep the stabilizers tight

against the fuselage.

STAB INSTALLATION

CAUTION:

You must watch the bolt holes for fatigue and drill

another hole by rotating the tube when this hap-

pens.

HINGING THE ELEVATORS

Collect the following items:

(2) Elevators
(6) Hinges

1.

Take three hinges and, as with the aileron

hinge installation, insert the hinge into the ele-

vator, using straight pins to ensure the hinge

stays centered between the stabilizer and the

elevator.

Slide the exposed side of the hinge into the

slots in the stab until the pins touch both the

stab and the elevator.

2.

Remove the pins in each hinge and, keeping

the elevator/stab assembly in position, apply 3

or 4 drops of thin CA to each hinge, on both

the top and bottom sides of the stab.

Allow ten minutes for the CA to cure before

flexing the elevator. Then install the second

elevator.

INSTALLING THE ELEVATOR SERVOS

1. * C

OLLECT THE FOLLOWING ITEMS

:

(2) S

ERVOS AND MOUNTING HARDWARE

(6) 24” S

ERVO EXTENSIONS

(2) 2-56

X

7-7/8” T

HREADED

R

OD

(2) -2-56 M

ETAL

C

LEVIS

(2) N

YLON

S

WING

K

EEPER

(2) 6-32

X

2” F

LAT

H

EAD

S

CREWS

(2) 6-32 H

EX

N

UT

(2) #6 F

LAT

W

ASHER

(2) B

LACK

A

DJUSTABLE

H

ORN

B

RACKET

(2) 2-56 H

EX

N

UT

2.

Remove the stabilizer from the fuselage.