These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
PILOT REPORTED: NORMAL: WEIGHT AND BALANCE CHECK, PREFLIGHT, FUELING (35 FRNT 35 CTR 05 REAR) PAX LOADING/BRIEFING, TAXI FOR SE DEPART, AND RUN UP. PREFLIGHT CHECKLIST: FUEL SELECTOR CTR TANK, FLAPS AND TRIM SET TO TAKEOFF, WATER RUDDERS RETRACTED, CARB HEAT 1/2 SELECTED CLEARED BY TOWER FOR SE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · tie rod · corrodedJul 22, 2019
ALL 4 LOWER FLOAT TIE-ROD (FLYING WIRES) WIRE PULLS SHOW SIGNS OF CORROSION AND ATTACHMENT HOLE ELONGATION.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Reciprocating engine · stud · failedJul 21, 2014
THREE MINUTES AFTER TAKEOFF, THE PILOT EXPERIENCED A LOSS OF POWER AND SLIGHT OIL ON THE WINDSHIELD IN HIS FLOAT EQUIPED ACFT. RETURNED TO THE WATER TAKEOFF AREA UNDER ITS OWN POWER. VISUALLY DETERMINED THAT 6 OF THE 10 CYLINDER BASE STUD ATTACHMENTS FOR CYLINDER NR 1 HAD FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
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Stabilizers · bracket · crackedJan 11, 1996
LEFT HORIZONTAL STABILIZER ATTACH FITTING ON STABILIZER SPAR FOUND CRACKED. INTERGRANULAR CORROSION EVIDENT ON THE COMPLETE LENGTH OF CRACK. PART IS HIGHLY LOADED AND SUBJECT TO STRESS CORROSION. SUBMITTER STATED THIS FITTING SHOULD BE EXAMINED CAREFULLY DURING THE REPETITIVE INSPECTIONS REQUIRED…
From FAA Service Difficulty Reports; matched by N-number and serial number.