Phoenix Model Flying Club
MODEL TRIMMING CHART

This chart will help you to set-up (trim) your new model on it's first few flights, this can even be used to trim an older model if you are not entirely happy with it's flying characteristics. A well trimmed and balanced plane will be a delight to fly and can convert an "old dog" into a model that will give immense pleasure in the air.
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| Pre Trimming Configuration...... | |||||||||
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TO TEST FOR |
TEST PROCEDURE |
OBSERVATIONS |
ADJUSTMENTS |
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1. Control Neutrals |
Fly the model straight and level |
Use Transmitter trims for hands |
Adjust clevises to centre |
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off straight and level flight |
Transmitter trims |
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2. Control Throws |
Fly model and apply full |
Check response of each control |
Aileron :- Hi-rate, 3 rolls in 3 to 4 |
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deflection of each control in |
seconds. Lo-rate, 3 rolls in 6 |
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turn |
seconds |
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Elevator :- Hi-rate to give a |
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smooth square corner, Lo-rate |
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to give a loop of approximately |
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130 feet diameter |
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Rudder :- Hi-rate approximately |
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30-35 degrees, for stall turns, |
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Lo-rate to maintain knife edge |
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flight. |
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3. Centre of Gravity (Method 1) |
Roll model into a near |
A. Nose drops |
A. Add weight to tail |
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vertically banked turn |
B. Tail drops |
B. Add weight to nose |
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(Method 2) |
Roll model inverted |
A. Lots of down elevator |
A. Add weight to tail |
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required to maintain level flight |
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B. No down elevator required |
B. Add weight to nose |
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to maintain level flight, or |
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model climbs |
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4. Decalage |
Power off vertical dive, cross |
A. Model continues straight down |
A. No adjustment required |
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wind (if any). Release controls |
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when model is vertical, |
B. Model starts to pull out, |
B. Reduce incidence |
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(elevator must be neutral). |
(nose up). |
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C. Model starts to tuck in, |
C. Increase incidence |
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(nose down). |
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5. Tip Weight (course |
Fly the model straight and level, |
A. Model does not drop a wing |
A. No adjustment required |
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adjustment) |
upright. Check aileron trim |
B. The left wing drops |
B. Add weight to right tip |
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maintains wings level. Roll the |
C. The right wing drops |
C. Add weight to left tip |
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model inverted, wings level. |
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Release aileron stick |
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6. Elevator Alignment. (for |
Fly model away from you and |
A. No rolling tendency when |
A. Elevators in correct |
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models with independent elevator |
into any wind. Pull it into an inside |
elevator applied |
alignment |
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Halves) |
loop or vertical climb, roll it inverted |
B. Model rolls in same |
B. Elevator halves misaligned. |
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and repeat by pushing it into an |
direction in both tests |
Either raise one half or lower |
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outside loop or vertical climb |
the other |
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C. Model rolls in opposite |
C. One elevator half has more |
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directions in both tests |
throw that the other, (the model |
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rolls to the side with the most |
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throw). Reduce throw on side |
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with the most throw or increase |
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throw on the other |
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Trimming starts here in earnest |
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1. Tip Weight (Final adjustment) |
Fly the model high into the wind |
A. Neither wing drops on pulling |
A. No adjustment required |
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either coming towards you or |
out. |
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or going away from you, smoothly |
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push the model into a vertical |
B. The right wing drops on pulling |
B. Add weight to the left wing |
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dive, pull out sharply and watch |
out. |
tip. |
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for a wing dropping. |
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C. The left wing drops on pulling |
C. Add weight to the right wing |
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out |
tip |
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2. Dihedral |
Fly the model straight and level |
A. The model does not roll. |
A. No adjustment required |
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into any wind, apply rudder and |
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watch for any tendency for the |
B. The model rolls in the direction |
B. Reduce dihedral |
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model to roll. |
of the applied rudder. (Proverse |
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a. Test in both directions. |
roll) |
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b. Make changes in increments |
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of no more than 1/8" at a time |
C. The model rolls in the opposite |
C. Increase Dihedral |
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c. Don't worry about the nose |
direction to the applied rudder |
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pitching down or up. |
(Adverse roll) |
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3. Side Thrust |
Fly the model away from you, |
A. Model continues straight up |
A. No adjustment required |
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(During tests re-trim with rudder |
into any wind. Pull it smoothly |
B. Model veers left |
B. Add right thrust |
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until a straight vertical is achieved, |
into a vertical climb going at |
C. Model veers right |
C. Reduce right thrust |
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then add side thrust to the value of |
least to normal manoeuvre height |
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half the rudder trim that was |
(watch for deviations to the left |
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needed. Zero the rudder trim) |
or right as it slows down) |
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(Go back and re-test after |
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adjusting) |
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4. Up/Down Thrust |
Fly the model cross wind, at a |
A. Model continues straight up |
A. No adjustment required |
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distance of around 100m from |
B. Model pitches up, (goes |
B. Add down thrust |
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you, (elevator trim should be |
towards the top of the model) |
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neutral as per test No 3), pull |
C. Model pitches down, (goes |
C. Reduce down thrust |
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it into a vertical climb and |
toward the bottom of the model) |
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neutralize the elevator, (watch |
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for any deviations up or down |
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as it slows down) |
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5. Aileron Differential |
Fly the model level and into |
A. The model does not veer |
A. No adjustment required |
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(Set the model up with 12 Degrees |
any wind, going away from |
sideways. |
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up and 11 to 12 Degrees down |
yourself. Pull it up into a |
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as a starting point.) |
45 Degree climb and roll to |
B. The model's path veers to the |
B. Increase differential, increase |
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the right. |
right. |
the up throw on both ailerons |
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(After adjusting, try again |
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in both directions) |
C. The model's path veers to the |
C. Decrease differential, increase |
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left. |
the down throw on both ailerons. |
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6. Pitching in knife-edge flight |
Fly the model on a normal pass |
A. There is no pitch up or down |
A. No adjustment required |
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(Method 1) |
and roll into knife-edge flight, |
B. The nose pitches up, (the |
B. Alternative cures :- |
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maintain height with top rudder, |
model climbs laterally) |
1. Move the C of G aft |
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(do this test in both left and |
2. Increase wing incidence |
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right knife-edge flight) |
3. Add down trim to ailerons |
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C. The nose pitches down, (the |
C. Reverse the above |
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model dives laterally) |
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6a. Knife-edge tracking |
Fly the model on a normal pass |
A. The model does not pitch |
A. No adjustment required |
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(Method 2) |
and roll into edge-edge flight, |
up or down |
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maintain height with top rudder, |
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(do this test in both left and |
B. The model pitches to the canopy |
B. Lower both Ailerons slightly |
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right knife-edge flight) |
in both knife-edges. |
Approximately 2 turns |
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C. The model pitches to it's bottom |
C. Raise both Ailerons slightly |
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in both knife-edges |
approximately 2 turns |
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D. The model pitches in opposite |
D. Use mixing from rudder to |
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directions in each knife-edge |
elevator to fix the problem. |
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7. Power off Tracking (Test #1) |
Fly the model level into any |
A. No roll to either side |
A. No adjustment required |
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wind, pull the power off and |
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watch for any roll off to either |
B. The model rolls left |
B. Mix 2% to 3% right aileron |
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side |
to low throttle, the amount |
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enough to neutralize the roll. |
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C. The model rolls right |
C. Mix 2% to 3% left aileron |
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to low throttle, the amount |
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enough to neutralize the roll. |
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Test #2 |
Fly the model high at a distance |
A. The model shown no |
A. No adjustment required |
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of approximately 100m into or |
tendency to roll |
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across wind but sideways to |
B. The model rolls to it's left |