Boeing 737-217
Service difficulty reports · 308
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 = '737217' 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 = '737217' 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 CA001122017Tire · failed(CAN) DURING THE TAKEOFF ROLL NR 4 MAIN WHEEL TIRE TREAD SEPARATED. THERE WAS NOTHING UNUSUAL NOTED BY THE FLIGHT CREW AND THE AIRCRAFT PROCEEDED TO SASKATOON. THE SEPARATED TIRE TREAD WAS DISCOVERED ON THE RUNWAY BY AIRPORT MAINTENANCE CREWS AND REPORTED TO CSDR CA000901006Engine · fod(CAN) NOT AN SDR - A/C 708, AUGUST 08/2000, YYZ, LOG SEQUENCE 0204503. ADVANCING THROTTLES FOR TAKEOFF, (APPROXIMATELY 5 TO 10 KNOTS) LARGE BANG WAS HEARD FROM NR 1 ENGINE. TAKEOFF WAS ABANDONED. ENGINE WAS SHUTDOWN, PARAMETERS APPEARED NORMAL. A PASSENGER REPSDR CA000804009Accessory Unit · failed(CAN) AFTER TAKEOFF FROM YUL LANDING GEAR LEVER WILL NOT MOVE UP. GEAR RETRACTED WITH LOCK TRIGGER OVERRIDE. REVERSER ISOLATION VALVE LIGHT ILLUMINATED IN FLIGHT. ON APPROACH TO YYZ LANDING GEAR POSITION LIGHTS NOT ON WHEN GEAR HANDLE SELECTED DOWN. VISUAL CHESDR CA000731009Pressure Switch · failed(CAN) SHORTLY AFTER TAKEOFF, THRUST REVERSER ISOLATION VALVE WARNING LIGHT ILLUMINATED. RETUNED. LIGHT WENT OUT WHEN LANDING GEAR SELECTED DOWN. REPLACED NR 1 AND NR 2 ENGINE LOW OIL PRESSURE WARNING SWITCHES AS PER MM 79-33-11.SDR CA000731002Engine · failed(CAN) A/C 717, JULY 19/2000, FLT 966, YEG, LOG SEQUENCE 0287301. REJECTED TAKEOFF DUE TO LARGE BANG AND AIRCRAFT SWERVED. FIRE BOTTLES DISCHARGED INTO NR 2 ENGINE. INSPECTION FOUND NR 2 ENGINE HAD SEVERE INTERNAL DAMAGE. NR 2 ENGINE. NR 2 ENGINE MOUNT INSPECTISDR CA000731006Line · leaking(CAN) AFTER TAKEOFF, "B" LOW QUANTITY LIGHT ILLUMINATED, FOLLOWED BY A LOW PRESSURE WARNING LIGHT ON "B" PUMPS. RETURNED. FOUND SUPPLY LINE TO RIGHT ELEVATOR ACTUATOR LEAKING. LINE REPLACED, SERVICED HYDRAULIC SYSTEM, LEAK CHECKED OK.SDR CA000731005Line · leaking(CAN) ON FINAL INTO YYZ, A COMPLETE LOSS OF A SYSTEM HYDRAULIC PRESSURE OCCURRED. WHEN TRAILING EDGE FLAPS SELECTED, WARNING LIGHTS AND A LEADING EDGE SLAT ASYMMETRIC WARNING INDICATION. AN EMERGENCY WAS DECLARED. FLAPS AND GEAR WERE LOWERED MANUALLY, FLIGHT LSDR CA000718007Transmitter · failed(CAN) ON TAKEOFF ROLL AT TAMPA, ABANDONED TAKEOFF AT 70 KNOTS, DUE NR 1 EPR DID NOT INDICTAE ABOVE 1.6 EPR. NR 1 EPR TRANSMITTER REPLACED AS PER WORK CARD 4241.SDR CA000718005Control Panel · failed(CAN) FLIGHT EXPERIENCED ELECTRICAL PROBLEMS AFTER ARRIVAL. GROUND POWER WOULD NOT STAY CONNECTED. APU WAS RUN TO SUPPLY ELECTRICS AND AIR. AFTER ENGINES STARTED, APU GENERATOR TRIPPED OFF. ENGINE GENERATORS SELECTED ON. THE APU WAS SELECTED OFF. DURING TAKEOFSDR CA000706001Gcu · failed(CAN) NR 2 ENGINE GENERATOR SYSTEM FAILED, UNABLE TO ESTABLISH APU ON AIRCRAFT BUSS. AIRCRAFT DIVERTED TO YHZ. NR 2 GENERATOR CONTROL PANEL REPLACED AS PER WORK CARD, SYSTEM CHECKED SERVICEABLE. APU GENERATOR OPERATIONS CHECKED NORMAL WHEN FUNCTIONED GROUND ANSDR CA000621004Switch · failed(CAN) ON TAKE, THRUST REVERSER ISOLATION VALVE WARNING LIGHT ILLUMINATED. RETURNED TO YYZ. THRUST REVERSERS OPERATED AS PER WORK CARD 1187, COULD NOT DUPLICATE DISCREPANCY. REPLACED NR 1 AND 2 THRUST REVERSER PRESSURE SWITCHES PER MM 78-31-16. OVERWEIGHT LANDISDR CA000410002Switch · failed(CAN) SHORTLY AFTER TAKEOFF THE THRUST REVERSER ISOLATION VALVE CAME ON THE OVERHEAD PANEL. CHECKLIST CAFFIED OUT, A/C RETURNED. LIGHT WENT OUT WHEN THE LANDING GEAR LOWERED. NR 1 THRUST REVERSER HYDRAULIC SYS PRESSURE SWITCH REPLACED.SDR CA000314001Fitting · corroded(CAN) HORIZONTAL STAB REMOVED FOR REPLACEMENT ANDIT WAS DISCOVERED THAT TWO BUSHINGS IN STABSCREWJACK ATTACH FITTING, LT ATTACH LUG, WERE LOOSE IN THE BORE. WHEN BUSHINGS WERE REMOVED CORROSION PITS WERE FOUND IN LUG BORE. FITTING REPLACED.SDR CA000215007Engine · failed(CAN) TURBINE SUSTAINED DAMAGE. TEARDOWN REPORT REQUIRED.SDR CA000224017Turbine · damaged(CAN) CONFIRMED TURBINE DAMAGE WHILE IN-FLIGHT. REPORT TO FOLLOW.SDR CA000110018Regulator · failedHYDRAULIC PRESSURE REGULATOR FAILED ON DESCENT. (ADP)SDR CA991229013Fan · jammed(CAN) ELECTRICAL SMOKE FOUND IN COCKPIT DURING B CHECK. SMOKE COMING OUT OF PEDESTAL. FOUND PDC CONTROL UNIT PANEL FAN JAMMED AND SMOKING. CONTROL DISPLAY UNIT AND AREA VENTILATED, FLIGHT DECK CLEANED AND SEAT COVERS REPLACED.SDR CA991208056Csd · failed(CAN) ON TAKEOFF, NR 1 GENERATOR DROPPED OFF-LINE WHEN POWER APPLIED FOR TAKEOFF. TAKEOFF REJECTED DUE NR 2 GEN US AND ON MEL, APU TOOK OVER POWER ELECTRONICS. NR 1 GENERATOR ON BUS WHEN RESET. NR 1 ENGINE RUN-UP CARRIED OUT AND TAKEOFF POWER WAS COMPLETED,SDR CA991208054Dust Shield · overtorqued(CAN) REPORT OF ELEVATOR FEEL NOT NORMAL. THIS SNAG GENERATED AFTER FIRST FLIGHT AFTER HEAVY MAINTENANCE VISIT. ELEVATOR FEEL BREAKOUT TORQUE WITHIN LIMITS. WAS PREVIOUS SAME SNAG. ELEVATOR COMPUTER REPLACED AND ELEVATOR CABLES CHECKED FOR PROPER TENSION. SDR CA991027008Valve · failed(CAN) ON DESCENT, NR 1 HYDRAULIC SYSTEM PUMP FAILED, HALFWAY THROUGH CHECK LIST, NR 2 A-PUMP LOW PRESSURE LIGHT CAME ON, WITH CORRESPONDING DROP OF A-SYSTEM PRESSURE. LOSS OF A-SYSTEM PRESSURE CHECK LIST CARRIED OUT , NR 1 AND NR 2 ENGINE CASE DRAIN FILTERS CSDR CA991027006Indicator · failed(CAN) CAPTAIN'S MACH AIRSPEED INDICATOR CYCLING ZERO TO 450 FTS, CIRCUIT BREAKER RESET, INDICATION NORMAL. ON TAKEOFF ROLL, AIRSPEED WENT U/S AGAIN, TAKEOFF ABANDONED, RETURNED TO RAMP. MACH AIRSPEED INDICATOR REPLACED.SDR CA991007015Regulator · leaking(CAN) AFTER 4 HOURS OF FLIGHT, STARTED DESCENT, NR 1 HYDRAULIC PRESSURE LOW LIGHT ON. EMERGENCY CHECK LIST CARRIED OUT, THEN THE NR 2 HYDRAULIC LOW PRESSURE LIGHT ON. A HYDRAULIC PRESSURE WENT TO 35 PSI. NO NOTICEABLE HYD FLUID LOSS. EMERGENCY DECLARED. SDR CA990817017Bolts · loose(CAN) DURING ROUTINE C-CHECK, FOUND SEVERAL PERIMETER BOLTS LOOSE AT THE AFT PRESSURE BULKHEAD TO FUSELAGE BUTT SPLICE STN 1016. TORQUE CHECK OF ALL 225 BOLTS REVEALED 183 WERE LOOSE AND 11 BOLTS SHANKED. ALL BOLTS WERE REMOVED AND HOLES CHECKED FOR DAMAGE. SDR CA990728023Line · loose(CAN) ON DESCENT AS POWER WAS REDUCED, A-SYSTEM PRESSURE FLICKERED THEN WENT TO ZERO, LOW PRESSURE LIGHTS ON. EMERGENCY DECLARED. LEFT ENGINE A-HYDRAULIC PUMP PRESSURIZED SYSTEM. LANDED OK. AFTER SHUT DOWN, AIRCRAFT TOWED TO GATE. FOUND HYDRAULIC TANK PSDR CA990707026Engine · slow(CAN) ON TAKEOFF, NR 1 ENGINE SLOW TO SPOOL UP. AT TAKEOFF, THRUST, EPR FLUCTUATED.SDR CA990707024Fire Detector · failed(CAN) ON CLIMB-OUT, NR 1 ENGINE OVERHEAT WARNING ILLUMINATED. ENGINE SHUT DOWN, BOTH FIRE BOTTLES DISCHARGED. LIGHT STILL ON. AIRCRAFT DIVERTED. REPLACED NR 1 ENGINE LOWER FIRE DETECTOR.SDR CA990614016Fire Loop · faulty(CAN) ON APPROACH , NR 1 FIRE WARNING ON, BOTH FIRE BOTTLES DISCHARGED, NR 1 ENGINE CHECKED, NO INDICATION OF FIRE, NR 1 ENGINE LOWER FIRE DETECTOR AT FAULT, DETECTOR SHORTED. REPLACED.SDR CA990603005Battery · overheated(CAN) DURING BOARDING, CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AND INITIATED FAULT ISOLATION PROCEDURES. THE BATTERY CHARGER CIRCUIT BREAKER TRIPPED AND THE MAIN AIRCRAFT BATTERY OVERHEATED. BATTERY AND CHARGER REPLACED. BATTERY HAD NOT BEEN MODIFIED SDR CA990330013Bulkhead · cracked(CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT, THE WEB WAS IDENTIFIED AS CRACKED DURING DISASSEMBLY .11 CM LONG Y SHAPED CRACK. WEB REPLACED.SDR CA990330012Bulkhead · cracked(CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT STA 178, VERTICAL WEB STA 178 RBL 5.7 IDENTIFIED AS CRACKED 2 CM LONG FROM EDGE OF WEB THROUGH ADJACENT FASTENER HOLE AND THREE CRACKS THROUGH 3 ADJACENT FASTENER HOLES. REPAIRED.SDR CA990310050Actuator · failed(CAN) ON INSTALLATION, FOUND ACTUATOR RAN IN OPPOSITE DIRECTION AS REQUESTED. REPLACED AND VENDOR ADVISED.SDR CA990310049Windshield · cracked(CAN) FIRST OFFICER'S WINDSHIELD CRACKED, REPLACED.SDR CA990310042Module · failed(CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE ON PUSH BACK, RETURN TO BLOCKS. REPLACED A-SYSTEM MODULE.SDR CA990310043Window · shattered(CAN) ON TOP OF CLIMB AT FL 270 FIRST OFFICER'S WINDOW STARTED TO SPARK AND BEFORE HEAT TURNED OFF, THE OUTER PANE SHATTERED. WINDOW REPLACED.SDR CA990310039Window · cracked(CAN) AIRCRAFT ARRIVED WITH NR 4 EYEBROW WINDOW CRACKED ON OUTER PANE. REPLACED.SDR CA981125021Receiver · failed(CAN) MISSED APPROACH DUE CAPTAIN'S GLIDE SLOPE READING TOO HIGH. SECOND APPROACH OK. REPLACED VHF NAVIGATOR RECEIVER.SDR CA981125015Regulator · failed(CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE NOTED. SUSPECT PRESSURE REGULATING VALVE FOR RESERVOIR HEAD PRESSURE. REPLACED VALVE.SDR CALA9801858Line · leakingTHE NR 1 ENGINE THROTTLE WAS TWO KNOBS AHEAD OF NR 2 WITH CLIMB POWER SET OUT OF MSP. THE SPLIT INCREASED TO ABOUT 3 KNOBS DIFFERENCE AS CLIMB PROGRESSED. FUEL FLOW WAS ABOUT 2000 LBS HIGHER ON NR 1 FOR SAME ENGINE PARAMETERS AT ABOUT 31,000 FT. THE NR 1 ENSDR CA980916027Fire Loop · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, APU FIRE WARNING LIGHT CAME ON AND BELL SOUNDED. APU SHUT DOWN. FIRE DRILL COMPLETED. FIRE LIGHT REMAINED ON AND FIRE BELL SOUNDED INTERMITTENTLY. AIRCRAFT RETURNED. REPLACED TAIL PIPE AND EXHAUST DUCT FIRE DETECTION LOOPS ASSDR CA980916021Indicator · reads low(CAN) ABORTED TAKEOFF DUE TO EGT 650 DEGREES, ALSO, EPR NOT ACTIVATED, AIRCRAFT RETURNED TO RAMP. CLEANED WATER TRAP AND PS4 LINE. ENGINE RUN AT TAKEOFF POWER. AIRCRAFT SERVICEABLE. REPLACED NR 1 EGT INDICATOR.SDR CA980818008Coffee Maker · malfunctioned(CAN) COFFEE MAKER FLASHED AND SMOKED, SMELL OF BURNING ENSUED. REPLACED COFFEE MAKER. PHASE LOSS DETECTOR CARD RESISTOR OVERLOADED AND BURNT.SDR CALA9801229Angle · crackedINSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 648-767, RBL 45. THE CRACKED AREA WAS CUT OUT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND MM 51-20-11.SDR CA980707025Computer · failed(CAN) TAKEOFF ABORTED AT 90 KNOTS DUE CAPT'S AIRSPEED INDICATOR INDICATING ZERO DURING TAKEOFF ROLL. AIR DATA COMPUTER REPLACED. A/C SERVICEABLE.SDR CA980707022Door · chafed(CAN) NOSE LANDING GEAR WORN ON INNER SURFACE. NO MENTION OF CLEARANCE CHECK IN AMM. DOOR REPLACED.SDR CA980602025Sensor · failed(CAN) AIRCRAFT TURNED BACK DUE TO L/H WING OVERHEAT LIGHT ON AND MASTER CAUTION LIGHT FLICKERING ON. FOUND SENSOR TOUCHING BLEED DUCT AND A LOOSE GROUND WIRE TO SENSOR. REPOSITIONED SENSOR AND CHECKED CONNECTIONS. ENGINE RUN OK.SDR CALA9800854Wire · brokenESCAPE PATH LIGHT INOP AT ROW 24. BROKEN WIRE AND MISSING LENS. REPAIRED LIGHT SOCKET WIRE AND REPLACED LENS SET PER MM 33-51-5.SDR CALA9800684Slide · low pressureINSPECTION FOUND R-2 DOOR SLIDE PRESSURE AT ZERO. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-311.SDR CA980602017Switch · failed(CAN) AIRCRAFT DIVERTED AFTER ENGINE SHUTDOWN DUE TO OIL BYPASS LIGHT ILLUMINATION. REPLACED OIL PRESSURE SWITCH AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA980602015Pump · failed(CAN) AIRCRAFT RETURNED TO GATE DUE TO FLUCTUATING ENGINE PARAMETERS. THE FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA980415009Switch · failed(CAN) AIRCRAFT RETURNED TO RAMP DUE TO STARTER VALVE LIGHT ON. VALVE REPLACED.
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