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The Hypass No. 48P6 ignition filters should be removed from the magnetos and replaced with magneto filter, Piper No. 63149.
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Cracking in the leading edge of the streamlined tube of the landing gear at the point where the tube joins the inboard end of the axle.
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Inspection of the left and right upper longerons for cracks using the dye penetrant technique.
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Steps to prevent loss of the elevator control system as a result of worn clevis bolts.
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Blade retaining flanges, P/N 3277 must be replaced with P/N 3277-1.
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Steps to prevent wing fabric loosening along the upper surface of the front and rear spars in the area of the fuel tank causing a spoiler action.
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Inspect engine mount bolts, spacer, hose, bushings, cup washers, nut, pin, and engine mount seats for damage.
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Inspection of the stabilizer leading edge attachment to the fuselage should be made for fatigue cracks.
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Examine the two flexible fuel lines to determine whether the hose inner liner has collapsed or failed thus causing a restriction to the flow of fuel.
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To forestall the possibility of engine fuel starvation during takeoff operations, install a placard on the right fuel quantity gauge.