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Due to failures of the Magnesium Die Cast Nose Wheel (which bears the number 34206 in raised letters), this wheel should be replaced by a Permanent Mold Aluminum Alloy Nose Wheel.
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Installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.
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Inspecting the existing aluminum vertical stabilizer forward attach fitting for cracks, and replacing any cracked parts.
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Inspect the vertical stabilizer rear spar fuselage attachment fitting for evidence of cracks in the fitting flange.
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Remove small baffle LAC P/N 181112 to allow for more accurate airspeed readings. With baffle installed readings can be incorrect by as much as +15 mph.
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Attach an operating limitation placard near the airspeed indicator in full view of the pilot, remove red radial marking on airspeed indicator, and/or replace wing front lift struts.
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Inspect front and rear control stick socket castings for cracks at the ears to which the push-pull tube attaches.
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Inspect the wing leading edge for buckled nose ribs or loose PK screws.
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Steps to prevent exhaust system cracking.
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Steps to detect permanent deformation and/or cracks in the lower frame side tubes on the adjustable front seat.