positive flap with maximum aileron deflection must be at least 10
mm. Check that the wheels are attached positively to the wing.
7. Check that the control surface gap seals are installed and
properly adhered to the wing recesses.
8. Check that the NACA ducts on the lower surface of the flaperons
are clear.
9. If the bug wiper system is installed, perform the checks given in
Section 7.12.3.
10. If flying with water ballast:
• Check before filling if all the rubber seals on the dump valves
are in position and that all valves are operating correctly.
• Check the dump rate of the main tanks with the filler caps
installed. Ensure that the dump rates of the left and right
wings are equal and that the dump rate is faster than that of
the tail tank.
Fuselage ⑤
1. General condition: Check for evidence of damage to the surface
finish or structural damage, pressure marks and cracks.
2. Check that the static pressure ports on the fuselage boom are
unobstructed.
3. Check that the tail wheel is sufficiently inflated.
4. Check that the water drain orifice in front of the tail wheel is not
obstructed.
Tail section ⑥
1. General condition: Check for evidence of damage to the surface
finish or structural damage, pressure marks and cracks.
2. Check that the total energy and pitot-static probe receptacles are
clear. Drain all possible water from the receptacle (if the probe
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