09/23/2021Patrick Standish
Correcting a condition that could cause loss of security of one or more screws which attach the aileron and flap hinge brackets.
09/23/2021Patrick Standish
Tightening engine mounting bolts to obtain a torque of (40) inch pounds.
09/23/2021Patrick Standish
Servicing instructions for the carburetor air filter with paper cartridge.
09/23/2021Patrick Standish
Misalignment of the oil radiator lines on the Lycoming 0-290-D2 135 horsepower engines at the point where they pass through the rear engine baffle.
09/23/2021Patrick Standish
Correction to the fuel grade specification in flight manuals and fuel tank placards for the Lycoming O-290-D2 engines.
09/23/2021Patrick Standish
Possibility of the fuel valve detent pins in a few valves were improperly centered, thus preventing positive indication of valve position.
09/23/2021Patrick Standish
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.
09/23/2021Patrick Standish
Mandatory replacement of 1/8 - 7 x 19 flexible stainless steel control cables to prevent cracked nicopress sleeves.
09/23/2021Patrick Standish
Inspecting for weld separation where the rudder pedal cable attachment fitting is welded to the rudder pedal.
09/23/2021Patrick Standish
Reports of the vacuum pump splined coupling on Airborne Mechanisms Vacuum Pumps Models 113A5 and 113A8 may fail prematurely as a result of over-curing.
09/23/2021Patrick Standish
Instructions for compliance with Marvel-Schebler Division Bulletin No. A1-69.
09/23/2021Patrick Standish
Instructions for an inspection of the vacuum pump adapter drive assembly.
09/23/2021Patrick Standish
Checking fuel selector valve for ease of rotation and instructions for lubricating.
09/23/2021Patrick Standish
Instructions to inspect the fuel tank filler caps for presence of a vent hole in the cap dome.
09/23/2021Patrick Standish
Instructions and material to reroute the rudder control cables to prevent cable contact with the adjacent fuselage frame tubes.
04/12/2022Patrick Standish
Reports of collapsed wing mounted fuel tanks due to inadequate venting of the tank.
04/12/2022Patrick Standish
A recent fuel tank collapse was attributed to inadequate venting, caused by obstruction of the cap vent holes installed per Piper Service Bulletin No. 522.
09/23/2021Patrick Standish
Instructions for the installation of an additional support plate to strengthen the attachment mechanism.
09/23/2021Patrick Standish
Exhaust muffler inspection and modification, Piper Part Number 12433-00, 12433-14, 12232-00.
04/12/2022Patrick Standish
Installing an improved forward fuel header tank with thicker walls and welded seals, which provides greater resistance to impact rupture in the event of an accident.