|
To Test For |
Test Procedure |
Observations |
Adjustment |
|
1. Control neutrals |
Fly model straight and level |
Adjust the transmitter trims
for hands off straight and level flight |
Adjust clevises to center
transmitter trims |
|
2. Control throws |
Fly model and apply full
deflection of each control in turn |
Check the response of each
control |
*Aileron Hi-rate: 3 rolls in
4 seconds.
*Lo-rate: 3
rolls in 6 seconds.
*Elevator
Hi-rate: to give smooth square corner.
*Lo-rate:
to give a loop of approx. 130' dia..
*Rudder
Hi-rate: approx. 30-35 degrees for stall
turns.
*Lo-rate to maintain knife
edge flight. |
|
3. Decalage |
Power off vertical dive.
Release controls when model is vertical
(elevator must be neutral). |
A. Does the model continue
straight down?
B. Does the
model start to pull out (nose up) ?
C. Does the model start to
tuck in (nose down)? |
A. No adjustment
B. Reduce
incidince
C. Increase incidince |
|
4. Center of gravity |
Method 1: Roll model into
near vertically banked turn.
Method 2: Roll model
inverted. |
A. Nose drops
B. Tail
drops
C. Lots of
down elevator required to maintain level
flight
D. No down elevator required
to maintain level flight, or model climbs |
A. Add weight to tail
B. Add
weight to nose
C. Add
weight to tail
D. Add weight to nose |
|
5. Tip Weight (course
adjustment) |
Fly model straight and level
upright. Check that aileron trim maintains
wings level. Roll model inverted, wings
level. Release aileron stick |
A. Model does not drop a
wing
B. Left
wing drops
C. Right wing drops |
A. No adjustment required
B. Add
weight to right tip
C. Add weight to left tip |
|
6. Side Thrust |
Fly model away from you into
any wind. Pull it into a vertical climb
(watch for deviations as it slows down). |
A. Model continues straight
up
B. Model
veers left
C. Model veers right |
A. No adjustment needed
B. Add
right thrust
C. Reduce right thrust (move
thrust line left) |
|
7. Up/Down Thrust |
Fly model on a normal path
into any wind. Parallel to strip, at a
distance of around 100m from you (elevator
trim should be neutral as per test No.3).
Pull into a vertical climb & neutralize
elevator. |
A. Model continues straight
up
B. Model
pitches up (goes towards top of model)
C. Model pitches down (goes
towards bottom of model) |
A. No adjustment needed
B. Add down
thrust
C. Reduce down thrust |
|
8. Tip Weight (fine
adjustment) |
Method 1: Fly model as per
test No.6 and pull it into a reasonably
small dia. inside loop (1 loop only).
Method 2: Fly the model as
per test No.6 and push it down into an
outside loop (1 loop only & fairly tight). |
A. Model comes out with wings
level
B. Model
comes out right wing low
C. Model comes out left wing
low |
A. No adjustment needed
B. Add
weight to left tip
C. Add weight to right tip |
|
9.(a) Aileron Differential
Method 1: |
Fly the model towards you,
before it reaches you, pull it up into a
vertical climb. Neutralize controls, then
half roll the model |
A. No heading changes
B. Heading
change opposite to direction of roll
commands (ie. heading veers to models & your
left after right roll).
C. Heading changes in
direction of roll command |
A. Differential OK
B. Increase
differential
C. Reduce differential |
|
9.(b) Aileron Differential
Method 2: |
Fly the model on a normal
pass and do 3 or more rolls |
A. Roll axis on model center
line
B. Roll
axis off to same side as roll command (ie.
right roll, roll axis off right wing tip)
C. Roll axis off to opposite
side of model as roll command |
A. Differential OK
B. Increase
differential
C. Reduce differential |
|
10. Dihedral |
Fly model on normal pass and
roll into knife-edge flight, maintain
altitude with top rudder (do this test in
both left & right knife-edge flight) |
A. Model has no tendency to
roll out of knife-edge flight
B. Model
rolls in direction of applied rudder
C. Model rolls in opposite
direction in both tests |
A. Dihedral OK
B. Reduce
dihedral
C. Increase dihedral |
|
11. Elevator alignment (for
models with independent elevator halves) |
Fly model as in test #6 and
pull it up into an inside loop. Roll
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
C. Model rolls in opposite
direction in both tests |
A. Elevators are in correct
alignment
B. Elevator
halves misaligned. Either raise one half or
lower the other half
C. One elevator half has more
throw than the other (model rolls to the
side with the most throw). Reduce throw on
one side or increase throw on the other |
|
12. Pitching in knife-edge
flight |
Fly model as per test no. 10 |
A. There is no pitching up or
down
B. The nose
pitches up (the model climbs laterally)
C. Nose pitches down (model
dives laterally) |
A. No adjustment needed
B.
Alternate cures:
1. Move the
CG aft
2. Increase
wing incidence
3. Add down
trim to ailerons
C. Reverse the above |