Fairchild SA227-CC
Service difficulty reports · 84
Newest first. General aviation reporting is voluntary.
Query with SQL
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 = 'SA227CC' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'SA227CC' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA070108009Engine · damaged(CAN) UPON SHORT FINAL A "POP" WAS HEARD SIMILAR TO THE SOUND OF A DOOR SEAL. THE AIRCRAFT YAWED A BIT YET NOT ENOEGH TO ALERT THE FLIGHT CREW THAT IT WAS ANYTHING MORE THAN TURBULENCE. OIL PRESSURE WAS NOTED TO BE DROPPING. AN ENGINE FAILURE OCCURED ON THE SDR 2006F00054Fire Warning · activatedRT ENGINE FIRE WARNING ILLUMINATED, RETURNED TO FIELD.SDR CA061018008Spinner · dented(CAN) GOOSE HIT THE OB SIDE OF THE LT PROP SPINNER. DAMAGE WAS MINIMAL TO THE SPINNER WHERE THE BLADE CUT OUT IS. THERE WAS ALSO MINIMAL DAMAGE TO THE CHIN COWL PN 27-63026-053. DAMAGE ON BOTH UNITS WERE COVERED BY THE SRM LIMITS OF .3750 DEGREES 4. (TC NR SDR CA061018009Line · cracked(CAN) HYD FLUID WAS DISCOVERED FROM GEAR UP LINE WHEN SYSTEM PRESSURE WAS APPLIED. LINE WOULD ONLY LEAK AFTER 1200 PSI WAS APPLIED, SYSTEM PRESSURE WAS 2000 PSI. PIN HOLE WAS IN RADIUS OF LINE. (TC NR 20061018009)SDR CA061018010Pump · cracked(CAN) UPON ROUTINE SPLINE REPLACEMENT IT WAS NOTICED THAT A CASTING DEFECT HAD BEEN FOUND AT THE BASE OF THE PUMP BELOW A FITTING. THE NATURE OF THE CASTING DEFECT IS WHAT IS TERMED AS A COLD SHUNT. A FLOURSECENT PENETRANT INSPECTION WAS CARRIED OUT AND THE SDR CA060511007Striker · loose(CAN) AFTER GEAR SWING TO CHECK FOR HYD LEAK IT WAS NOTED THAT THE LT GEAR DID NOT EXTEND. THE LT OB STRIKER ON THE LT CAM ASSY WAS LOOSE AND NOT CONTACTING ACTUATOR AREA FOR UPLOCK RELEASE. THE BOLT WAS REMOVED FROM STRIKER AND FOUND TO BE STRIPPED AND THE SDR CA060112009Indicator · inoperativeON TAKEOFF, THE TORQUE INDICATOR WENT TO ZERO. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE REPLACED INDICATOR AND RELEASED AIRCRAFT AFTER SATISFACTORY GROUND RUN.SDR CA051213007Starter Gen · intermittentGENERATOR DROPPED OFF LINE, GENERATOR RESET AND WAS FINE FOR REMAINDER OF LEG. UPON LANDING GENERATOR DROPPED OFF LINE AND AGAIN WAS RESET WITH NO FURTHER PROBLEMS. UPON FURTHER INVESTIGATION MAINTENANCE FOUND WHAT HAD THE APPEARANCE OF REMNANTS OF A BEARINGSDR LNX2005F00001Engine · unknownAIRCRAFT WAS ON TAKEOFF ROLL FOR DEPARTURE. THE CREW WAS UNABLE TO ACHIEVE TARGET TORQUE ON THE RT ENGINE AND ABORTED THE ROLL. CAUSE OF LOW TORQUE COULD NOT BE ISOLATED TO AN EXTERNAL CAUSE AND THE ENGINE WAS REMOVED AND SENT TO THE VENDOR FOR EVALUATION. SDR MR0510Line · crackedJUST BEFORE LANDING, HYDRAULIC VAPOR/SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT, ENGINES SHUTDOWN AND PAX DEPLANED. MAINTENANCE FOUND FAILED HYDRAULIC LINE IN WING ROOT THAT SPRAYED FLUID INTO AIR CYCLE MACHINE INTAKE WHICH TRANSFERRESDR O05R200416973Blade · damagedBLADE REJECTED IAW MFG CONCESSION 102566/C/P.SDR 2003FA0000885Clamp · brokenON AIRCRAFT ENGINE TRUSS ADEL CLAMPS FROM 3 O'CLOCK POSITION TO 9 O'CLOCK ARE SEVERLY BRITTLE AND ARE BREAKING, AND CORRODING THE ASSEMBLY DUE TO THE HIGH HEAT BEING GENERATED FROM THE ENGINE.SDR 510082703Blade · brokenDURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT APPROXIMATELY .7500 OF ONE THIRD STAGE TURBINE BLADE HAD BROKEN OFF AND EXITED OUT THE TAIL PIPE CAUSING DAMAGE TO THE TAIL PIPE AND SCAVENGE PUMP COVER. THE THIRD STAGE T-WHEEL ASSEMBLY HAS A SERVICE LIFE OF SDR CA021105004Warning Light · false activation(CAN) AFTER TAKE-OFF AND AS THE AIRCRAFT BEGAN TO PRESSURIZE THE CARGO DOOR WARNING LIGHT ILLUMINATED. THECREW REQUESTED A RETURN TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTION OF THE AIRCRAFT DET ERMINED THAT A FALSE WARNING INDICATION OF THE CARGO DSDR I7W2002F00001Fire Warning · false indicationFALSE NR 2 ENGINE FIRE WARNING. FIRE DETECTOR, REMOVED AND REPLACED UNIT. DID NOT SOLVE PROBLEM. STILL TROUBLESHOOTING.SDR CA020820011Tube · cracked(CAN) SHORTLY AFTER DEPARTURE THE CREW NOTED ILLUMINATION OF THE RT HYDRAULIC LIGHT. A FEW SECONDS LATER THE LEFT HYDRAULIC LIGHT ILLUMINATED FOLLOWED BY A LOSS OF PRESSURE ON THE HYDRAULIC PRESSURE GAUGE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLYSDR HKG2002F00000Actuator · failedSECOND IN COMMAND IN RT SCAT REPORTED TO CAPTAIN THAT THE PITCH TRIM WOULD NOT TRIM NOSE DOWN. PILOT IN CHARGE ATTEMPTED TRYING AUX TRIM SWITCH WITH SAME RESULTS. PITCH TRIM WAS TRANSFERRED TO THE NR 1 POSITION, PILOT IN CHARGE REPORTED THAT THERE WAS STILL SDR EAT2002F00001Windshield · crackedTHE RT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX. 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PSI. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CRACKING.SDR EAT2002F00000Windshield · crackedTHE RIGHT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PSI. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CRACKING.SDR CA000511008Line · cracked(CAN) FUEL LINE ITEM NR 105 ON IPC 73-10-01 FOUND CRACKED DUE TO VIBRATION AND LACK OF CLAMP AS REQUIRED WITHIN IPC ITEM NR 110 73-10-01 FIG. 2PAGE 2B.SDR CA991209070Switch · shorted(CAN) DURING TAXI, THE CREW DETECTED A BURNING PLASTIC SMELL. THE CREW NOTICED THE ANNUNCIATOR PANEL GO ON AND OFF AS WELL AS LOSING SOME INDICATORS. THE AIRCRAFT RETURNED TO BASE FOR MAINTENANCE. THE MAINTENANCE CREW DETERMINED THAT THE GPS/NAV SWITCH HAD SHOSDR CA991103009Brush · cracked(CAN) 5 MINUTES AFTER TAKEOFF, THE RIGHT GENERATOR WENT OFF-LINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE DETERMINED THAT THE STARTER/GENERATOR BRUSHES HAD CRACKED AND THE LEADS HAD SEPARATED FROM THE REMAINING BRUSH MATERIAL.SDR CA981125067Trim Actuator · seized(CAN) RUDDER TRIM SEIZED IN-FLIGHT. AIRCRAFT RETURNED OK. ACTUATOR REPLACED.SDR CA980325039Bearing · failed(CAN) PILOT COMPLAINED OF A LOUD NOISE COMING FROM THE RIGHT ENGINE ON START. STARTER REMOVED AND DRIVE END SHAFT FOUND VERY SLOPPY. DRIVE END BEARING HAD BLOWN APART.SDR CA980325038Trunnion Bolt · loose(CAN) PILOT COMPLAINED OF VIBRATIONS IN THE TAIL WHEN PITCH TRIMMING AT HIGHER SPEEDS. INSPECTION FOUND THAT THE STABILIZER HAD MORE THAN ACCEPTABLE PLAY. THE MAIN PIVOT INNER AND OUTER BOLTS WERE FOUND FAR BELOW THE SPECIFIED TORQUE AS OUTLINED IN THE FAIRCSDR CA980318006Beta Switch · leaking(CAN) CREW REPORTED NO BETA INDICATION WHEN ON LANDING ROLL AND TAXI. BETA SWITCH AND PLUMBING CHECKED. OIL LEAK WAS EVIDENT ON ENGINE COWL FLAP. SOURCE OF OIL LEAK DETERMINED TO BE FROM BETA SWITCH VENT HOLES. 0.5 LITERS OF OIL WAS LOST IN THIS MISHAP.SDR CA980318018Switch · intermittent(CAN) NO GREEN INDICATION FOR THE NOSE ALTHOUGH THE IN-TRANSIT LIGHT WAS OK.GEAR DOWN SWITCH WAS INTERMITTENT.SDR AU980053Torque Link · cracked(AUS) LH AND RH MAIN LANDING GEAR UPPER TORQUE LINKS CRACKED IN AREA OF THE CENTRE PIVOT LUGS.SDR AU971535Indicator · faulty(AUS) RH MAIN LANDING GEAR POSITION LIGHT FAULTY.SDR AU971381Pipe · cracked(AUS) HYDRAULIC PIPE SPLIT IN RADIUS LOCATED ON THE FIRST BEND FORWARD OF THE RH ENGINE FIREWALL.SDR AU970225Pin · incorrect fit(AUS) LANDING GEAR EMERGENCY GEAR EXTENSION SHUTOFF VALVE HANDLE LOCK PIN INCORRECTLY FITTED - EMERGENCY GEAR EXTENSION HANDLE WAS PUSHED FORWARD TOWARDS THE EMERGENCY POSITION PREVENTING CORRECT OPERATION OF THE LANDING GEAR RETRACTION SYSTEM - PERSONNEL ERROSDR CA951114001Line · chafed(CAN)HYDRAULIC LINE CHAFED BY ENGINE RPM SPEED LEVER CABLE NEAR HYDRAULIC SHUT OFF.SDR LOSA9512Stall Computer · malfunctionedPILOT REPORTED STICKSHAKER BRIEFLY ENGAGED IN FLIGHT ABOVE 200 KNOTS AND ALSO ENGAGED BRIEFLY DURING FLIGHT ABOVE STALL SPEED. MAINTENANCE REPLACED LEFT STALL VANE ASSY FOR EXCESSIVE UNADJUSTABLE VOLTAGE, REPLACED SAS CONTROL BOX AND LT SAS COMPUTER. OPERATISDR LOSA9510Connector · looseFAT - CREW REPORTED COPILOT AND AUXILIARY STABILIZER TRIMS INOPERATIVE. MAINTENANCE FOUND LOOSE WIRE AT CIRCUIT BREAKER. SECURED WIRE AND OPERATIONAL CHECKS NORMAL. AIRCRAFT RELEASED FOR FLIGHT. (X)
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