Cessna T207A

Service difficulty reports · 42

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'T207A'
  ORDER BY difficulty_date DESC"

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SDR 2025F00156Blades · ground damageAIRCRAFT TAXIING THROUGH SHELTAIR RAMP AT KPMP PARKING RAMP AND THE PROPELLER CAME INTO CONTACT WITH A STACK OF 3 TO 4 RUBBER CONSTRUCTION CONES, WITCH RESULTED IN TWO OF THE THREE BLADES OF THIS PROPELLER TO BREAK FREE OF THE RETAINING RING CLIPS THAT HOLD TJun 22, 2025 · N6449H · Cessna T207A · Propeller Blade SectionSDR 2024FA0000770Switch · meltedSMOKE IN CABIN FROM ELECTRICAL SWITCH PANEL. CHAFED WIRE FOUND IN LEFT HAND WING LEADING EDGE NEAR RIB/SKIN JUNCTION. REPLACED WIRE, SWITCH AND CIRCUIT BREAKER. HOURS ON SWITCH UNKNOWN, WAS INSTALLED FEB. 10, 2013.Oct 9, 2024 · N100PC · Cessna T207A · Exterior LightingSDR WIWA2020F00000Oil System · leakingTHE PILOTS REPORTED THAT HE SET TAKEOFF POWER, ENGINE PARAMETERS READ NORMAL AND UPON REACHING 40 KNOTS HE SAW A ROLL BACK. HE EXECUTED AN ABORTED TAKEOFF AND HEARD SOME ENGINE SPUTTERING FOLLOWED BY THE ENGING SHUTTING OFF. MAINTENANCE FOUND NO ABNORMAL PROSep 16, 2020 · N9317M · Cessna T207A · Reciprocating Engine Oil SystemSDR P9KA2015120802Fuel Tank · leakingDUE TO LEAKAGE OF THE RT WING TANK, THE LT WING WAS REMOVED TO ACCESS & INSPECT IT'S FIBERGLASS TANK. ON TANK REMOVAL, IT WAS FOUND TO HAVE ONE LOCATION OF APPARENT CRACKING & LEAKAGE. DUE TO THE DIFFICULTIES INVOLVED IN ACCESSING THESE TANKS FOR INSPECTION Dec 4, 2015 · N1301L · Cessna T207A · Fuel StorageSDR P9KA2015120801Fuel Tank · leakingTHE ACFT WAS WRITTEN UP & INVESTIGATED MULTIPLE TIMES DUE TO FUEL SMELL IN THE CABIN. AFTER SEVERAL ATTEMPTS TO FIX THE PROBLEM, PROCESS OF ELIMINATION LED TO THE RT WING TANK LEAKING. BECAUSE THE ACFT HAD A FIBERGLASS TANK INSTALLED, THE WING & BUTT RIB HADDec 4, 2015 · N1301L · Cessna T207A · Fuel StorageSDR P9KA2015120803Governor · intermittentDURING A PREFLIGHT RUN UP, THE GOVERNOR WOULD NOT CYCLE THE PROPELLER EVEN WHEN LT IN THE LOW RPM POSITION FOR 10+ SECONDS. THE PROPELLER GOVERNOR WAS REPLACED WITH SERVICEABLE & OPERATIONS WERE NORMAL. THE GOVERNOR ONLY HAD 29.5 HOURS SINCE OVERHAUL & THE ROct 7, 2015 · N1301L · Cessna T207A · Propeller GovernorSDR P9KA15022602Attach Bracket · crackedTHE HORIZONTAL STABILIZER WAS REMOVED AS PART OF A ROUTINE ANNUAL INSPECTION. DURING INSPECTION THE RT HORIZONTAL STABILIZER ATTACH BRACKET PN 1212128-2 WAS FOUND CRACKED JUST ABOVE THE BOLT HOLE. THE PART WAS REPLACED WITH NEW. ACCORDING TO THE ACFT LOGS TFeb 23, 2015 · N1301L · Cessna T207A · Horizontal Stabilizer, Attach FittingsSDR P9KA15022601Attach Bracket · crackedTHE HORIZONTAL STABILIZER WAS REMOVED AS PART OF A ROUTINE ANNUAL INSPECTION. DURING INSPECTION THE LT HORIZONTAL STABILIZER ATTACH BRACKET PN 1212128-1 WAS FOUND CRACKED JUST ABOVE THE BOLT HOLE. THE PART WAS REPLACED WITH NEW. ACCORDING TO THE ACFT LOGS TFeb 23, 2015 · N1301L · Cessna T207A · Horizontal Stabilizer, Attach FittingsSDR P9KA2015010801Fork · crackedDURING A ROUTINE 100 HOUR INSPECTION, CRACKS WERE NOTED IN THE NLG FORK. THE CRACKS EXTENDED FROM THE FWD 2 BOLT HOLES FWD TO THE EDGE OF THE PART & AFT APPROXIMATELY 1/2 INCH ON EACH SIDE. DISASSEMBLY REVEALED SEVERAL MORE CRACKS THAT DID NOT EXTEND PAST THJan 6, 2015 · N1301L · Cessna T207A · Nose/Tail Landing Gear Strut/AxleSDR OW62010F00000Cylinder · crackedFUEL STAIN ON OUTER ALUMINUM CASTING, CRACK FOUND BETWEEN COOLING FINS NEAR UPPER SPARKPLUG HOLE AND FUEL INJECTOR PORT. CRACK CONFIRMED BY PRESSURIZING INDUCTION SYSTEM AND SOAP BUBBLES. CRACK ORIGINATED IN THE INTAKE PORT AREA. THIS IS THE 3RD CYLINDER REFeb 11, 2010 · N7608U · Cessna T207A · Reciprocating Engine Cylinder SectionSDR OW62009F00000Cylinder · brokenPART 135 OPERATOR WITH 6 PERSONS ON BOARD, SCENIC TOUR FLIGHT. NR 5 CYLINDER/BARREL SEPARATED IN FLIGHT. ACFT MADE EMERGENCY OFF-AIRPORT LANDING.Sep 12, 2009 · N7608U · Cessna T207A · Reciprocating Engine Cylinder SectionSDR CA090706004Engine · failed(CAN) ENGINE FAILED IN FLIGHT, WEATHER WAS GOOD, RESTART FAILED, ACFT MADE FORCED LANDING MINOR INJURIES. ACFT TO BE RECOVERED AND INVESTIGATED BY SAFETY BOARD.Jun 18, 2009 · Cessna T207A · Engine (Reciprocating)SDR 2009FA0000321Blade · crackedTHE ACFT WAS TAKEN OUT OF SERVICE DUE TO A BLADE THAT ROTATED FREELY IN THE HUB AND WAS NOT CONNECTED TO THE PITCH CHANGE MECHANISM. THE PROPELLER WAS DISASSEMBLED AND THE RETENTION AREA OF ONE BLADE WAS FOUND TO BE CRACKED APPROX 3 INCHES ACROSS THE RETENTIOApr 15, 2009 · N803AN · Cessna T207A · Propeller Blade SectionSDR 2007FA0000879Selector Valve · mismanufacturedWHEN THE FUEL SELECTOR VALVE IS SELECTED TO THE RT TANK, FUEL IS BEING DELIVERED FROM THE LT TANK, VISE VERSA. THIS WAS DISCOVERED DURING A SHORT FLIGHT IN WHICH THE PILOT NOTICED THE RT TANK FUEL GAUGE WAS DROPPING WHEN THE LT TANK WAS SELECTED. THIS WAS LASep 9, 2007 · N803AN · Cessna T207A · Fuel Selector/Shut-Off ValveSDR 2007FA0000359Fitting · crackedFWD RT STABILIZER FITTING CRACKED. FOUND CRACKED FITTING UPON ANNUAL INSPECTION OF EMPENNAGE. (K)Apr 3, 2007 · N803AN · Cessna T207A · Horizontal Stabilizer StructureSDR CA060511001Door Frame · cracked.5 INCH CRACK FOUND IN LOWER LT DOOR POST JAMB DURING ROUTINE INSPECTION.May 11, 2006 · Cessna T207A · Fuselage Main, StructureSDR CA060316004Fitting · gougedDURING WING REMOVAL FOR PAINT, LT LOWER WING STRUT FITTING WAS FOUND TO HAVE A GOUGE OF APPROXIMATELY 1/8" FROM STRUT FAIRING SCREW.Mar 6, 2006 · Cessna T207A · Wing Miscellaneous StructureSDR 2005FA0001134Fitting · brokenPILOT FOUND VERTICAL STABILIZER LOOSE ON PREFLIGHT. MAINTENANCE INSPECTED AND FOUND RT FWD ATTACHMENT FITTING BROKEN. REPLACED BOTH FWD FITTINGS WITH NEW PARTS. (K)Jul 28, 2005 · N9482M · Cessna T207A · Fuselage, Stabilizer Attach FittingsSDR ENHA0507Alternator · failedREMOVED DUE TO CB POPPING FREQUENTLY.Jan 27, 2005 · N8NZ · Cessna T207A · AC Generation SystemSDR UAT2005F00005Alternator · failedALTERNATOR FAILED AT 225.2 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K)Nov 29, 2004 · N73789 · Cessna T207A · AC Generator-AlternatorSDR UAT2005F00004Alternator · failedALTERNATOR FAILED AT 57.4 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K)Nov 29, 2004 · N73789 · Cessna T207A · DC Generator-AlternatorSDR ENHA2003005Pushrod · bentNR 6 CYLINDER EXHAUST PUSHROD BENT.Aug 20, 2003 · N8NZ · Cessna T207A · Reciprocating Engine Cylinder SectionSDR ENHA2003004Pushrod Tube · crackedNR 6 CYLINDER EXHAUST PUSHROD TUBE HOUSING CRACKED, PUSHROD BENT. SUSPECT STUCK VALVE.Aug 20, 2003 · N48CF · Cessna T207A · Reciprocating Engine Cylinder SectionSDR CA020702002Piston · damaged(CAN) AFTER A SOUTH BOUND DEPARTURE FROM CYPY RUNWAY 03 AN ABNORMAL DROP IN MANIFOLD PRESSURE WAS NOTICED. THE P/C SWITCHED FUEL TANKS TO ENSURE THE CAUSE WAS NOT FUEL CONTAMINATION. THERE WAS NO IMPROVEMENT. ENGINE INDICATIONS WERE LOW OIL PRESSURE, HIGH OIL Jun 20, 2002 · Cessna T207A · Reciprocating Engine Cylinder SectionSDR KNF2002F00000Tire · failedRIGHT MAIN TIRE BLEW OUT ON LANDING. TIRE HAD SURFACE TREAD AND WAS NOT WORN. A FLAT SPOT WAS NOTED WHERE THE BLOWOUT OCCURED. BRAKES WERE APPLIED BEFORE AIRCRAFT TOUCHED DOWN. PILOT NEEDS TO KEEP FEET OFF THE BRAKES UNTIL THE AIRCRAFT HAS LANDED.Mar 27, 2002 · N3156X · Cessna T207A · Wheel/Ski/FloatSDR CA000720017Cylinder · cracked(CAN) WHEN PERFORMING A CYLINDER DIFFERENTIAL COMPRESSION CHECK, FOUND CYLINDER NR 5 HAD A 60/80 COMPRESSION, AND AIR WAS LEAKING OUTSIDE CYLINDER. AFTER FURTHER INSPECTION, FOUND CRACK COULD BE SEEN JUST INBOARD OF THE EXHAUST PIPE FLANGE. CYLINDER WAS REMOVJul 7, 2000 · Cessna T207A · Reciprocating Engine Cylinder SectionSDR AU000577Support Bracket · cracked(AUS) RUDDER BAR SUPPORT ASSEMBLIES PN 1213887-1 (LEFT) AND PNO1213887-2 (RIGHT) CRACKED THROUGH BOLT HOLES.Jan 19, 2000 · Cessna T207A · Rudder StructureSDR 99ZZZX3403Controller · failedON ROLL-OUT, AIRCRAFT WOULD NOT DEVELOP POWER. ONLY REACHED 24 MAP. APC WAS FOUND WITH CARBON AND METAL CONTAMINATION. AIRCRAFT HAD TURBOCHARGER CATASTROPHIC FAILURE 2 WEEKS PRIOR. POSSIBLE CAUSE WAS METAL PARTICLES FROM TURBO FAILURE CONTAMINATED SEAT VALAug 13, 1999 · N9482M · Cessna T207A · Exhaust TurbochargerSDR 99ZZZX3111Turbocharger · failedPILOT REPORTED GOOD M.A.P. AT TAKEOFF. TWO MINUTES INTO FLIGHT, M.A.P. DROPPED TO 23 INCHES. THIRTY SECONDS LATER, M.A.P. DROPPED TO 20 INCHES. SUSPECT THIS IS WHEN TURBO FROZE UP AND RESTRICTED EXHAUST FLOW LIMITING ENGINE POWER. SUBMITTER STATED NO PASSEJul 27, 1999 · N9482M · Cessna T207A · Exhaust TurbochargerSDR 99ZZZX3178Controller · malfunctionedDURING TAKEOFF ROLL, A LOSS OF MANIFOLD PRESSURE OCCURRED OF APPROXIMTAELY 10 IN HG. TAKEOFF ABORTED WITHOUT INCIDENT. DURING GROUND RUN AND TROUBLESHOOTING, THE PROBLEM WAS DUPLICATED AND DETERMINED TO BE A STICKING WASTEGATE CONTROLLER VALVE. THE CONTROLLJun 22, 1999 · N6491H · Cessna T207A · Engine Exhaust SystemSDR 97ZZZX4446Blade · crackedPILOT REPORTED SLIGHT ENGINE VIBRATION AND PROPELLER SLOW TO RESPOND IN RETURN TO LOW PITCH. DISASSEMBLY REVEALED ONE BLADE WAS CRACKED 180 DEGREES NEAR BEARING SURFACE AT ROOT END. CAUSE UNKNOWN. CATASTROPHIC FAILURE IMMINENT. BLADE UNDER ANALYSIS AT MCCAOct 7, 1997 · N75870 · Cessna T207A · Propeller Blade SectionSDR 97ZZZX3748Hub · crackedPENETRANT INSPECTION DURING NORMAL OVERHAUL INDICATED A FINE LINEAR CRACK OR SCRATCH. SUBSEQUENT EDDY CURRENT TESTING USING PHASE PLANE ANALYSIS INSTRUMENTATION REVEALED A CRACK APPROXIMATELY 1.5 INCHES LONG, ESTIMATED OVER .040 INCH DEEP ON THE EXTERIOR SURFJul 29, 1997 · N9317M · Cessna T207A · Propeller Hub SectionSDR 97ZZZX3386Cylinder · failedAIRCRAFT WAS AT 6,500 FEET MSL, CRUISE POWER SETTINGS. WHEN PILOT RETARDED THROTTLE FOR DESCENT, HE FELT A VIBRATION. HE TURNED TO AN ALTERNATE AIRPORT. THE ENGINE WAS RUNNING ROUGH AND ON SHORT FINAL, NR 6 CYLINDER SEPARATED FROM ENGINE CAUSING THE ENGINE TJul 3, 1997 · N6427H · Cessna T207A · Reciprocating Engine Cylinder SectionSDR 97ZZZX1592Hinge Pin · failedPILOT REPORTED LOSS OF MANIFOLD PRESSURE AFTER TAKEOFF. MADE OFF-AIRPORT LANDING. NO INJURY, NO DAMAGE TO AIRCRAFT. MAINTENANCE INSPECTION FOUND ALTERNATE AIR DOOR HINGE PIN MISSING WHICH ALLOWED THE DOOR TO FALL INTO THE CONNECTING ELBOW TO THE TURBOCHARGEMar 13, 1997 · N1783U · Cessna T207A · Engine Air Intake SystemSDR 96ZZZX3774Cylinder · separatedPILOT REPORTED ROUGH ENGINE AND LARGE RPM DROP ON MAG CHECK. INSPECTION FOUND NR 3 CYLINDER CRACKED. WHEN CYLINDER REMOVED, IT WAS DISCOVERED THE HEAD WAS COMPLETELY SEPARATED. BOTTOM SPARK PLUG WAS FOULED.Jul 11, 1996 · N6308H · Cessna T207A · Reciprocating Engine Cylinder SectionSDR 95ZZZX6803Cylinder Assy · crackedENGINE OPERATION NORMAL ON TAKEOFF, CLIMB, AND CRUISE SETTING. ROUGHLY 15 MINUTES INTO FLIGHT, THE ENGINE LOST MANIFOLD PRESSURE. FULL THROTTLE MANIFOLD PRESSURE WAS 25 INCHES. PILOT LANDED WITHOUT INCIDENT. INSPECTION FOUND THE NR 4 CYLINDER HAD CRACKED OOct 13, 1995 · N3156X · Cessna T207A · Reciprocating Engine Cylinder SectionSDR 95ZZZX3521Baffling · misinstalledBAFFLING WAS IMPROPERLY INSTALLED, JAMMING PROPELLER CONTROL INTERMITTENTLY. MAINTENANCE SHOULD DOUBLE CHECK THEIR WORK ESPECIALLY SINCE THIS AIRPLANE JUST CAME OUT OF AN INSPECTION.Jul 8, 1995 · N6372H · Cessna T207A · Engine Air Baffle SectionSDR 95ZZZX3520Strut · overservicedNOSE STRUT OVERSERVICED CAUSING LOSS OF STEERING. TO PREVENT THIS, MAINTENANCE SHOULD SERVICE TO WHAT THE MANUFACTURER STATES AND PERFORM A TAXI TEST.Jul 8, 1995 · N101EN · Cessna T207A · Nose/Tail Landing Gear Strut/AxleSDR 95ZZZX3998Filter · gasket displacedOIL FILTER INTERNAL GASKET WAS OUT OF PLACE AND COVERING INLET PASSAGE OF FILLER BODY. APPEARS TO BE MANUFACTURE DEFECT. SUBMITTER ADVISES A CLOSER INSPECTION OF OIL FILTER PRIOR TO INSTALLATION TO INSURE GASKET IS NOT BLOCKING INLET HOLE.Jul 1, 1995 · N803AN · Cessna T207A · Reciprocating Engine Oil SystemSDR 95ZZZX3474Adapter · thread damageDURING COMPLIANCE WITH SEB 92-1R1 (CESSNA). ADAPTER WAS REMOVED FROM PUMP HOUSING AND THREAD DAMAGE WAS EVIDENT. 3OX MAGNIFICATION OF DAMAGE APPEARED TO BE A MANUFACTURING DEFECT. NO DAMAGE DUE TO MISUSE IS SUSPECTED. SEB 93-1R1 IS TO CHECK THREAD DAMAGE DJun 20, 1995 · N9629M · Cessna T207A · Reciprocating Engine Oil SystemSDR HERA9506Fuel Flow Ind · malfunctionedFLT NR 1521 - AIR RETURN TO OTZ, DUE FUEL FLOW INDICATED 11 GALLONS PER HOUR (GPH) IN CRUISE FLIGHT. A LANDING WAS MADE AT OTZ WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW INDICATOR AND PERFORMED A FUEL FLOW TEST IAW THE CESSNA SERVICE MANUAL. GROUNFeb 10, 1995 · N1765U · Cessna T207A · Fuel Flow IndicatingSDR 95ZZZX919Line · hole chafedLOSS OF BRAKE PRESSURE ON RT SIDE. FOUND HOLE WORN THROUGH BRAKE LINE UNDER LANDING GEAR FAIRING. SUSPECTED LINE WAS PUSHED DOWN BY PERSONNEL CAUSING CONTACT WITH SCREW THAT SECURES FAIRING.Feb 6, 1995 · N101EN · Cessna T207A · Landing Gear Brake System
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