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41 aircraft flight trimming chart – HITEC Eclipse 7 Pro User Manual

Page 43

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41

Aircraft Flight Trimming Chart

To test for

Test Procedure

Observations

Adjustments

9. Aileron differential

Method 1: fly model toward you &

pull into a vertical climb before it

reaches you. Neutralize controls,

then half-roll the model.

Method 2: fly model on normal

pass

and do three or more rolls

Method 3: fly the model straight

and

level and gently rock the aileron

stick back and forth

A. No heading changes

B. Heading change opposite to

roll command

(i.e. heading veers left after right

roll)

C. Heading change in direction

of roll

command

A. Roll axis on model centerline

B. Roll axis off to same side of

model as roll

command (i.e. right roll, roll axis

off right

wing tip)

C. Roll axis off to opposite side

of model as

roll command

A. Model flies straight ahead

without yawing

B. Model yaws away from roll

command

(i.e. right roll, yaw left)

C. Model yaws towards roll

command

(i.e. right roll, yaw right)

A. Differential settings OK

B. Increase differential

C. Decrease differential

A. Differential settings OK

B. Increase differential

C. Decrease differential

A. Differential settings OK

B. Increase differential

C. Decrease differential

10. Dihedral

Method 1: Fly the model on

normal

pass and roll into knife-edge

flight;

maintain flight with top rudder (do

this test in both left & right

knifeedge

flight)

Method 2: Apply rudder in level

flight

A. Model has no tendency to roll

B. Model rolls in direction of ap-

plied rudder

C. Model rolls in opposite direc-

tion in both tests

A. Dihedral OK

B1. Reduce dihedral

B2. Use mixer to produce aileron

opposing rudder travel (start

with 10%)

C1. Increase dihedral

C2. Mix ailerons with rudder

direction 10%

A. Elevators in correct

11. Elevator alignment

(for models with

independent

elevator halves)

Fly the model as in Test 6 and

pull

up into an inside loop. Roll it

inverted and repeat the above by

pushing it up into an outside loop.

A. No rolling tendency when

elevator applied

B. Model rolls in same direction

in both tests

- halves misaligned.

C. Model rolls opposite directions

in both tests.

One elevator half has more throw

than the

other (model rolls to side with

most throw).

A. Elevators in correct alignment

B. Either raise one half, or lower

the other

C. Reduce throw on one side, or

increase throw

on the other.

12. Pitching in

knife-edge flight

Fly the model as in Test 10

A. There is no pitch up or down

B. The nose pitches up (the

model climbs

to its top side)

C. Nose pitches down (model

dives to its

bottom side)

A. No adjustment needed

B. Alternate cures:

1) move CG back;

2) increase incidence;

3) droop ailerons;

4) mix down elevator with rudder

C. Reverse ‘B’ above

*Trim tab is 3/16” x 3/4” x 4” trailing edge stock, placed just in front of aileron on bottom, pointed end forward.