Boeing 737-275C
Service difficulty reports · 36
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 = '737275C' 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 = '737275C' 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 JRAA2018041200001Pump · brokenNR 1 ENGINE FAILED DURING TAKEOFF, GOT 3 BACK FIRING BEFORE ENGINE SHUTDOWN, QRH COMPLETED. REMOVED FUEL PUMP AND DISCOVERED IT HAD A BROKEN SHAFT. INSTALLED NEW FUEL PER MM 72-00-61 AND OPS CHECKED IT PER AMM 71-09-100.SDR JRAA20160229001Check Valve · leakingRIGHT FUEL TANK DUMPING FUEL INTO CTR TANK IN FLIGHT. TURNED ON CTR TANK RT BOOST PUMP & TURNED OFF RT TANK FUEL PUMPS. LANDED WITH 5400 LBS LT TANK, 4000 LBS RT TANK & 2000 LBS IN CTR TANK. FLIGHT BEGAN WITH 16000 LBS FUEL ON BOARD & CTR TANK ALMOST EMPTY.SDR CA130719007Clamp · broken(CAN) SHORTLY AFTER TAKEOFF, THE CREW RECEIVED A START VALVE OPEN CAUTION LIGHT FOR ENGINE NR 1. THE CREW FOLLOWED THEIR SOPS AND SHUTDOWN THE NR 1 ENGINE. THE CREW THEN HELD A CIRCUIT FOR APPROXIMATELY 1 HR TO BURN OFF FUEL SO THEY COULD PERFORM A NON-OVERWSDR CA130905014Tube · cracked(CAN) THE CREW REPORTED LOW ENGINE PRESSURE RATIO ON ENGINE NR 2 AND SUBSEQUENTLY REJECTED TAKEOFF, RTO, DUE TO AN EPR FAILURE. MAINTENANCE TROUBLESHOT THE SYS VIA LEAK TESTS ON THE EPR SYSTEM AND, THROUGH THE PROCESS OF ELIMINATION, DETERMINED THE CAUSE WAS SDR CA120127010Blades · damaged(CAN) SERVERE VIBRATION ON NR 2 ENGINE WHEN ENGINE SELECTED TO IN-FLIGHT IDLE AT TOP OF DECENT. ENGINE VIBRATION GUAGE AT FULL MAXIMUM IN "TURBINE POSITION". FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL EXAMISDR CA111012011Spindle · sheared(CAN) ACFT WAS ON FINAL APPROACH, WHEN THE FLIGHT CREW SELECTED INCREASING FLAP ANGLES, THEY NOTICED THE ACFT TENDED TO ROLL TO THE LT AND RUDDER TRIM WAS REQUIRED TO STABILIZE THE ROLL. WITH FLAPS SELECTED TO 40, 3 UNITS OF RUDDER TRIM WERE REQUIRED TO COMPESDR CA101122001Hinge · sheared(CAN) ON ARRIVAL OF THE MAINTENANCE PERSONNEL THEY FOUND THE INBOARD HINGE BROKEN AND THE CRACK ON THE KRUGER FLAP INBD SKIN WHICH COULD HAVE BEEN CAUSED WHEN THE KRUGER FLAP WAS EXTENDED CATCHING THE WING (WHICH WAS NOT DAMAGED) BENDING THE UPPER INBD SKIN OFSDR CA100517002Shear Tie · corroded582 HMV, LEVEL 2 CORROSION IDENTIFIED (IN THE FWD E&E BAY AT STA 360 BETWEEN STR 28 AND 27 ON BOTH THE RT AND LT SIDES OF THE ACFT.) - INVESTIGATION DATA STILL BEING COLLECTED - INITIAL REPORT THAT SHEAR TIES AND RADIUS FILLERS WERE REQUIRED TO BE FABRICATEDSDR CA091022001Screw · wrong part(CAN) FUEL PANELS HAD BEEN OPEN FOR MAINTENANCE, WHEN IT CAME TIME FOR RE-TORQUE OF THE SCREWS, THE SCREWS BOTTOMED OUT, AS THEY WERE THE WRONG LENGTH. MAINTENANCE CONTRACTOR HAS BEEN ADVISED. PROPER SCREWS HAVE BEEN INSTALLED (TC 20091022001)SDR CA090716006Seal · leaking(CAN) AFTER A CHANGE OF GEARBOX FOR ONE REMOVED SERVICEABLE FROM ANOTHER ENG, THE ENG STARTED LEAKING OIL IN FLIGHT, WHICH GAVE INDICATIONS OF OIL FLUXUATION. ENG WAS SHUTDOWN AS A PRECAUTION. SEAL WHEN REMOVED WAS FOUND FULL OF CARBON. SEAL WAS REPLACED, ASDR CA090219009Deflector · damaged(CAN) NOSE LANDING GEAR, GRAVEL DEFLECTOR, PLATE, RETAINER AND FIBERGLASS SKIN WITH WEARS, GOUGES, CORROSION AND NICKS. GRAVEL DEFLECTOR COMPONENTS WITH LUGS AND BORES CORRODED. ASSY DEFLECTOR ASSY PN: 65-76611-26 SN: 9994 MODIFICATION INCORPORATED 39-1067.SDR CA090203005Skin · corrodedDURING ROUTINE SCHEDULED HEAVY MAINTANANCE VISIT (C3 CHECK), CORROSION WAS FOUND ON A LAP JOINT AT STA 460 TO 480, ON STR 26L. THIS CORROSION IS BELIEVED TO BE CAUSED BY THE BONDING PROCESS AT FACTORY. THE PROCESS (COLD BONDING) WAS ACCOMPLISHED ON THE FIRST SDR CA081002004Battery · overheated(CAN) PASSENGERS WERE ON THE ACFT, ACFT WAS ON EXTERNAL GROUND POWER AT THE TIME. WHEN THE PILOTS WENT TO START THE APU, THEY NOTICED THE START WAS NOT NORMAL, AND THE APU ALSO DID NOT START. APU OVERSPEED CAUTION LIGHT ILLUMINATED. CAPTAIN WENT TO THE E&E SDR CA060206012Bearing Race · worn(CAN) LOW FREQUENCY OSCILLATION FELT THROUGH AIRFRAME DURING CLIMB BETWEEN 240-270 KTS. NO CHANGE WITH AUTOPILOT ON OR OFF. ( NOTE: THIS WAS NOT VIBRATION ) HORIZ STAB PIVOT BEARINGS ON BOTH THE LT AND RT SIDE WERE REPLACED, BEARING HOUSING WAS REPLACED ON LTSDR CA051128009Flex Line · kinked(CAN) THE SUBJECT AIRCRAFT HAD INTERMITTENT HISTORY ASSOCIATED WITH NOSE GEAR EXTENSION/RETRACTION ANOAMLIES. DURING A RECENT HEAVY CHECK THIS ISSUE WAS FURTHER INVESTIGATED.THE TEFLON LINED HYDRAULIC FLEX LINE WAS FOUND TO HAVE KINKED.IT IS BELIEVED THAT THISSDR CA051101009Hinge Fitting · corroded(CAN) NO CPCP CORROSION TASK COVERS THIS AREA, BUT DUE TO THE FINDINGS THE MAINTENANCEPROGRAM IS BEING AMENDED TO REDUCES THE CORROSION FINDINGS IN THIS AREA. THE CO RROSION WAS FOUND ON THE AFT AIRSTAIRS UPPER HINGE FITTING ON THE LOWER FOLDING SECTION. THE FSDR CA051101008Fitting · corroded(CAN) THE CORROSION TASK C53-107-01-01.7 IS INSPECTING THE CABIN SEAT TRACKS. THE CORROSION WAS FOUND ON THE UPPER DECK CARGO G NET FITTING P/N 65-62157-505. THE FOLLOWING INSPECTIONS OF THIS FITTING HAVE BEEN INCORPORATED IN THE MAINTENANCE PROGRAM 1) ADDITISDR CA050706008Line · leakingLOSS OF A SYSTEM HYDRAULICS. RECTIFICATION INVESTIGATION FOUND THE NUMBER 2 ENGINE THRUST REVERSER HYDRAULIC RETURN LINE HAD FAILED CAUSING THE LOSS OF A SYSTEM FLUID, PART NUMBER B432E0562C. UPON DELIBERATION WITH FLIGHT OPERATIONS, IT WAS DECIDED TO DISPATSDR CA050420004Engine · failed(CAN) CLIMBING THROUGH APPROX 17,000' AT 320 KIAS, WITHOUT WARNING, A BANG WHICH CAUSED ACFT TO SHUDDER FOLLOWED BY VIBRATION & A HOWLING NOISE NR 2 ENG VIBRATION INDICATOR READING IN EXCESS OF 2 UNITS, EGT & OIL TEMP STARTED TO RISE, & ALSO A DROP IN EPR. ACSDR CA050405013Cable · malfunctioned(CAN) PILOT REPORTED THAT THE STEERING TILLER AND THE RUDDER PEDALS DO NOT CENTER WHEN RELEASED, AND THE TILLER STICKS ON HARD TURNS. MAINTENANCE FOUND THE STEERING CABLE TURN BARREL ID TAG HAD SLIPPED FROM THE TURN BARREL, THEREBY RESTRICTING FREE MOVEMENT OSDR CA050301009Housing · loose(CAN) CREW REPORTED, NR 1 ENG OIL PRESSURE WAS BELOW RED AND INDICATION WAS READING ZERO. ENG WAS SHUTDOWN, AC LANDED W/O INCIDENT. MAINT FOUND NR 1 ENG OIL FILTER CAP WAS DISLODGED DUE TO LWR STUDS OF GB HSG HELICOILS FAILING. ENGINEERING ISSUED A PROD PERSDR CA031109001Spring · failed(CAN) UPON DEPARTURE FROM THE NOSE LANDING GEAR FAILED TO LOCK UP. AFTER SELECTING GEAR HANDLE TO NEUTRAL POSITION THE NOSE GEAR FELL OUT OF THE NOSE WHEEL WELL. SEVERAL SUBSEQUENT GEAR UP SELECTIONS WERE UNSUCCESSFUL. THE AIRCRAFT RETURNED AND MADE AN UNEVESDR CA030418001Connector · damaged(CAN) FLT CREW REPORTED NLG GREEN DOWNLOCK INDICATION WOULD NOT EXTINGUISH WHEN MLG SELECTED UP. MLG DID RETRACT. GREEN LIGHT WOULD NOT EXTINGUISH. MLG CYCLED 3 TIMES, NO JOY . RETURNED TO BASE. ABLE TO DUPLICATE FAULT ON GROUND. NLG DOWNLOCK SENSOR REPLACSDR CA010503009Turbine · damaged(CAN) A/C 752, APRIL 19/2001, FLT 3697, YQR, LOG SEQUENCE 0496405, 20 MINUTES FROM YQR, NR 1 ENGINE DEVELOPED HIGH VIBRATIONS, ENGINE OIL TEMP WAS 10 DEGREES ABOVE NORMAL. CREW SHUTDOWN ENGINE AND DECLARED AN EMERGENCY, PROCEEDED TO YQR. LANDED WITHOUT FURTHERSDR CA010301020Engine · damaged(CAN) AT END OF TAKEOFF ROLL AND DURING INITIAL CLIMB, A CABIN ATTENDANT CALL ANNUNCIATOR COULD BE HEARD RINGING REPEATEDLY. WHEN AIRCRAFT LEVELLED OUT AT 5000 FEET, FLIGHT ATTENDANT SPOKE TO PASSENGER WHO REPORTED THAT SPARKS WERE COMING FROM RIGHT ENGINE. CASDR CA000614004Sensor · out of tolerance(CAN) ON TAKEOFF, LANDING GEARS WOULD NOT RETRACT WITHOUT USING GEAR OVERRIDE. AIRCRAFT RETURNED. LANDING GEAR ACCESSORY MODULE REPLACED AS PER WORK CARD 4281. OFF CANADIAN PART 7-326-9-0010 SERIAL 0054, ON SERIAL #0438. FURTHER TROUBLESHOOTING FOUND AIR SENSSDR CA000313003Sensor · out of adj(CAN) NLG RED POSITION WARNING LIGHT REMAINED ON WITH GEAR UP. RECYCLED AND NO FIX A/C LANDED. UPLOCK SENSOR OUT OF ADJUSTMENT, ADJUSTED A/C SERVICEABLE.SDR CA000224016Proximity Sensor · out of adj(CAN) AFTER TAKEOFF NLG RED POSITION WARNING LIGHT REMAINED ON WITH GEAR UP AND OFF. RECYCLED AND RED LIGHT STILL ON. SENSOR TARGET OUT OF ADJUSTMENT, ADJUSTED A/C SERVICEABLE.SDR CA991229015Housing · cracked(CAN) FOUND AFT STAIR NOT FULLY EXTENDED. AFT STAIR FORWARD TRANSMISSION HOUSING CRACKED AND TOP STEP AFT HINGE SEGMENT CRACKED. PARTS REPLACED OR REPAIRED.SDR CA991208055Indicator · failed(CAN) CREW REPORTED NR 1 ENGINE OIL TEMPERATURE INDICATOR HAD FAILED AFTER TAKEOFF. AIRCRAFT RETURNED FOR REPAIRS. REPLACED NR 1 OIL TEMPERATURE BULB AND RUN-UP CARRIED OUT SERVICEABLE.SDR CA971003002Pcu · broken(CAN) ON TAXI OUT, 'A' SYSTEM HYDRAULIC PRESSURE AND QUANTITY DROPPED TO "0". RUDDER POWER CONTROL UNIT (PCU) REPLACED. THE METAL COVER ASSEMBLY BROKEN AND PLUGS P/N 69-54775-1 EXPOSED PERMITTING FLUID LOSS. REPLACED.SDR CA970130009Bearing · failed(CAN) CREW REPORTED #4 TIRE FLAT AT GATE. CONDITION INDICATED THAT THE AIRCRAFT HAD TAXIED PART WAY TO GATE ON FLAT TIRE. WHEN WHEEL REMOVED INNER WHEEL HALF WAS SEVERELY DAMAGED DUE TO BEARING FAILURE. REPLACED.SDR CA961029003Manifold Duct · separated(CAN) THROUGH FL240 #1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE SHUTDOWN WAS CARRIED OUT. POST FLIGHT INSPECTION FOUND THE 13TH STAGE BLEED AIR DUCT HAD SEPARATED AT THE FORWARD MOUNTING POSITION. FURTHER INSPECTION FOUND THE HOT BLEED AIR RELEASED CSDR CA961023002Seal · loose(CAN) ON TAKEOFF AND WHEN STARTED TO PRESSURIZE LOUD NOISE COMING FROM L1 FORWARD L/H MAIN ENTRY DOOR AIRCRAFT RETURNED. LOWER HINGE CAME ADRIFT, SEAL REINSTALLED.SDR CA960729004Clamp · failed(CAN) LOST HYDRAULIC QUANTITY AND PRESSURE ON "A" SYSTEM ON TAXI AFTER LANDING. BOTH ENGINES SHUT DOWN. HYDRAULIC LEAK FROM RETURN FILTER. NEW FILTER HOUSING CLAMP AND SEAL INSTALLED, LEAK CHECK CARRIED OUT SERVICEABLE.SDR CA951123105Jack Screw · corroded(CAN)ON DESCENT WITH AUTOPILOT ON, THE STAB OUT OF TRIM LIGHT CAME ON. DISCONNECTED AUTOPILOT AND ATTEMPTED TO RETRIM. POSSIBLE TO TRIM NOSE UP BUT NOT POSSIBLE TO TRIM NOSE DOWN ELECTRICALLY OR MANUALLY. CORROSION IN AUXILIARY BRAKE HOUSING AND BRAKE ARMS BI
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