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 |