Aircraft Trimming
Test for Procedure Results Adjustments
Control Neutrals test response to each control Adjust trims for straight & level flight adjust clevises to center xmter trims
Control Throws Apply full deflection of each control Check for response; Aileron hi rate 3 rolls in 3 secs. Elevator, square loop corners Rudder, 35 to 40 Deg. Change control horns, ATV, and Duel Rates as required
Center of Gravity 1. Roll into a vertically banked turn 1. A. Nose Drops A. Add tail weight
Method 1 1. B. Tail Drops
2. Roll into inverted flight B. Add Nose weight
Method 2 2. A. lot of down required to hold level flight
(see Note A at bottom)
2. B. up elevator needed to hold level flight
Up/ Down Thrust, test 1 Fly model straight & level, then cut throttle A. Model continues level flight with a gradual drop A. No Change
Note Either change B or C requires retest of Decalage and Verticals
B.Model abruptly dives B. Increase down thrust
C. Model abruptly climbs C. Reduce down thrust
Up/Down Thrust, test 2 Fly model straight & level, then pull up A.Model continues straight up A. No Adjustment
Note Either change B or C requires retest of Decalage and Verticals
B.Model pulls to canopy B. Increase down thrust
C.Model pulls to belly C. Reduce down thrust
Decalage, Angle of Incidence Power off vertical dive from high altitude (neutralize elevator) A. Model continues straight down A. No change needed
(see Note B at bottom)
B. Model pulls to canopy B. Increase wing or stab incidence
C. Model pulls to belly C. Reduce wing or stab incidence
Knife Edge Pitch Fly model on normal pass, roll to knife edge, left and right, use rudder to hold model level A. Model does not change pitch A. No adjustment needed
B. Model pitches to canopy B. Either move CG aft; or increase wing incidence; or mix down elevator with rudder
C. Model pitches to belly C. Reverse of B;
Tip Weight - Test1 Fly straight; level, roll inverted, release aileron stick A. Model does not drop a wing A. No adjustment
B. Left wing drops B. Add weight to right tip
C. Right wing drops C. Add weight to left tip
Tip Weight - Test 2 Fly model towards you / away from you, pull tight inside loop, repeat with outside loop A. Model comes out with wings level A. No adjustment
B.Model comes out with right wing low B. Add weight to left tip
C. Model comes out with left wing low C. Add weight to right tip
Side Thrust Fly model away from you and pull up to vertical A. Model continues straight up A. No Adjustment
B. Model veers left B. Increase Right thrust
C. Model veers right C. Reduce Right thrust
Aileron Differential Fly model toward you, pull into a vertical climb before it reaches you. Neutralize controls then half roll . A. No Heading Changes A. Differential settings OK
B. Heading change opposite to roll command B. Increase differential
C. Heading change in direction of roll command C. Decrease differential
Dihedral Fly model on normal pass, roll to knife edge, left and right, use rudder to hold model level A. Model does not roll A. Dihedral OK
B. Model rolls indirection of rudder B. Reduce dihedral
C. Model rolls opposite to rudder C. Increase dihedral
Note A:These two methods for determining the C.G. of a model will give approximate results only. Start out with the C.G. where the Designer suggested, or somewhere between 25% to 35% of the Mean Aerodynamic Cord. The optimum C.G. for your model will require further testing while performing maneuvers. The results will only be an approximation at best.
Note B:This portion of the trimming chart may be unclear for the following reason;
In order to maintain level upright flight, the wing of a plane with a symmetrical airfoil wing needs to have a positive Angle of Attack (AOA, usually less than 1 degree). This positive angle provides the lift required to cause the plane to fly level. If the plane is balanced slightly to the nose heavy side (required for pitch stability), it will require a slight up elevator trim to hold level flight. A plane with a zero/ zero wing to elevator angle will also need a slight amount of up elevator trim to hold level flight. Therefore, a plane trimmed in this manner will have a tendency to pull to the canopy on a straight, thumbs off, down line because the elevator is controlling the AOA of the wing.
This positive AOA may also be achieved by a positive incidence change, which requires an offsetting down elevator for level flight. Thus, a power-off down line should fall straight down, with neutral controls. There are significant interactions between wing incidence changes and CG, therefore it is most important that the C.G. of the airplane be established first.
In the final analysis, flight trimming an airplane is a personal preference issue after you have taken care of the basic essentials.