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Control Centering: Fly straight and
level. Use transmitter trims for hands off straight and level flight. Adjust
clevis to center transmitter trims, or reset computer trims.
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Control throws: Fly model and apply
full deflection of each cotrol in turn. Check response of each control:
Aileron hi-rate: 3 rools in 4 seconds, low rate: 3 rolls in 6 seconds,
Elevator high rate: to give a good and smooth corner, low rate: to give a loop
of approx. 130 foot in diameter, Rudder high rate: 30-35 degrees for stall
turns, low rate: to maintain knife edge.
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Decalage: Power off vertical dive,
cross wind (if any). Release controls when model is vertical (elevator trim
mush be neutral).
A: Model continues straight down; no adjustment.
B: Model starts to pull nosw up; Reduce wing incidence.
C: Model starts to pull nose down; Increase wing incidence.
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Center of gravity:
Method 1: Roll into a near vertically banked turn.
A: Nose drops; Add tail weight.
B: Tail drops; Add nose weight.
Method 2: (Simple) Roll inverted.
A: Lots of down elevator required to mantain level flight. Add tail weight.
B: Now down elevator required or plane climbs; Add nose weight.
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Tip weight: (course adjustment) Fly
straight and level upright. Adjust aileron trim for level flight. Roll
inverted, level wings and release stick.
A: Model does not drop a wing; No adjustment.
B: Left wing drops; Add weight to right tip.
C: Right wing drops; Add weight to left tip.
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Side thrust: Fly away from you, into
any wind and pull vertical.
A: Model continues straight up; No adjustment.
B: Model veers left; Add right thrust.
C: Model veers right; Reduce right thrust.
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Up/Down thrust: Fly normal path into
wind, parallel to you, approx 100 yards from you. Elevator trim should be
neutral per test 3. Pull vertical and release elevator.
A: Model continues straight up; No adjustment.
B: Model pitches nose up; Add down thrust.
C: Model pitches nose down; Reduce down thrust.
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Tip weight: (fine adjustment)
Method 1: Fly model as per test 7, and pull into a small loop (1 only)
Method 2: Fly model as per test 7, and push into a small outside loop (1 only)
A: Model comes out with wings level; No adjustment.
B: Model comes out with right wing low; Add weight to left tip.
C: Model comes out with left wing low; Add weight to right tip.
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Aileron differential:
Method 1: Fly towards you and pull into a vertical climb. Release controls,
then do a half roll.
A: No heading changes; No adjustment.
B: Heading changes to opposite of roll command (veer left after right roll);
Increase differential.
C: Heading changes in direction of roll command; Reduce differential.
Method 2: Fly model on a normal pass and do three or more rolls.
A: Roll axis on model center line; No adjustment.
B: Roll axis off same direction as roll command (right roll, roll axis off
right wing tip); Increase differential.
C: Roll axis opposite of command; Reduce differential.
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Dihedral: Fly on normal pass and roll
knife edge (left and right).
A: Model holds knife edge; No adjustment needed.
B: Model rolls in direction of rudder; Reduce dihedral.
C: Model rolls opposite direction of rudder; Add dihedral.
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Elevator alignment with independent
halves: Fly model per test 6 and pull into a loop. Roll inverted and push into
an outside loop.
A: No roll tendency when elevator applied; No adjustment needed.
B: Model rolls same in both tests; Elevator halves misaligned. Raise one half
or lower the other according to roll.
C: Model rolls opposite in both tests; One elevator half has more throw than
the other. Model rolls direction of more throw.
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Pitching and knife edge: Fly per test
10.
A: No pitch up or down; No adjustment.
B: Nose pitches up;
1) Move C. G. aft.
2) Increase wing incedence.
3) Add down trim to ailerons.
C: Nose pitches down; Reverse above.