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A recent design change to the fuel tank caps has created a possible hazard to the venting system and it is therefore requested that the caps be reworked in the following manner.
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Instructions for inspecting the battery box lid for proper clearance between the lid and the battery terminals.
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Suggestions to alleviate troubles with the stabilizer adjusting mechanism.
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Due to a number of reported failures of single strand .032" safety wire used on control system turnbuckles, it is considered necessary to replace the safety wire with single strand .040" brass or copper wire.
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Due to a number of reported failures of single strand .032" safety wire used on control system turnbuckles, it is considered necessary to replace the safety wire with single strand .040" brass or copper wire.
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Correction to the fuel grade specification in flight manuals and fuel tank placards for the Lycoming O-290-D2 engines.
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To preclude the possibility of in-flight fires, the following inspection and rework is necessary to eliminate combustible material and possible ignition sources from the area aft of the firewall underneath the forward cabin floor.
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Mandatory replacement of 1/8 - 7 x 19 flexible stainless steel control cables to prevent cracked nicopress sleeves.
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Reports of collapsed wing mounted fuel tanks due to inadequate venting of the tank.
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Reports of collapsed wing mounted fuel tanks due to inadequate venting of the tank.