Boeing 737-275
Service difficulty reports · 290
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 = '737275' 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 = '737275' 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 CA101028005Line · cracked(CAN) ENGINE FOUND TO BE LEAKING FUEL BY MAINTENANCE, ENGINE REMOVED FUEL MANIFOLD LINE FOUND TO BE CRACKED UNDER THE SHROUDS, REPLACED THE LINE. ENGINE RE-INSTALLED SERVICEABLE.SDR CA100104005Spindle · cracked(CAN) SPINDLE BROKE IN AREA OF AD 2003-24-08 PRIOR TO THE INSP THRESHOLD OF 3000C. UNIT HAD BEEN O/H, FAILED PART IS CURRENTLY WITH QA AND WILL BE SHIPPED TO MFG UNLESS OTHERWISE INSTRUCTED. FLAP SPINDLE CRACK OCCURRED AT CRITICAL "A" AREA SPECIFIED IN ASB 73SDR CA091002004Accumulator · out of tolerance(CAN) PART WAS INSTALLED WHEN NOT IN COMPLIANCE WITH AD 2003-11-03 THIS AD EFFECTIVE O3-JULY-03 STATES THAT PN 2660 472M2 MAY NOT BE INSTALLED ON ANY ACFT.SDR CA090106006Hydraulic System · malfunctioned(CAN) WHILE ON THE TAXI FROM MX HANGAR TO THE TERMINAL, THE TAXI CREW APPLIED THE BRAKES WITH NO EFFECT. THE ACFT WAS SHUT DOWN. THE AMM WAS CONSULTED, AND REMOVED A HYDRAULIC CASE DRAIN FILTER, AND FOUND THE FILTER TO BE COMPLETED BLOCKED WITH ICE. IT IS PSDR CA080208006Nose Bullet · separated(CAN) FOLLOWING DEPARTURE, THE CREW REPORTED COMPRESSOR STALLING OF THE NR 1 ENG AT CLIMB PWR. THE ENGINE PWR WAS REDUCED AND COMPRESSOR STALLS STOPPED. THE AC RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT. INSP OF THE ENGINE IDENTIFIED THAT THE NR 1 ENGINE NSDR CA050504006Controller · inoperative(CAN) ON DEPARTURE, A/C WAS CLIMBING THROUGH FL210 WHEN THE CREW NOTICED THE CABIN DIFFERENTIAL WAS AT MAXIMUM AND THE CABIN RATE OF CLIMB WAS EXCEEDING 3000 FPM (UP). THEY IMMEDIATELY INITIATED A RAPID DESCENT AND STABILIZED THE CABIN ALTITUDE AT AN A/C ALTISDR CA041013010Actuator · cracked(CAN) A SYSTEM HYDRAULIC LIGHTS ILLUMINATED, A SYSTEM QTY READ ZERO. NR 8 SPOILER ACTUATOR FOUND CRACKED. ACTUATOR REPLACED MM 27-62-91. CARRIED OUT RII INSPECTION.SDR CA040819003Fitting · cracked(CAN) CRACKED FITTING FOUND DURING CPCP INSPECTION. RT MAIN LANDING GEAR ACTUATORS WING LINK FORWARD ATTACH FITTING (TO WING REAR SPAR ATTACH).SDR CA030704004Light · failed(CAN) WHILE CLIMING THROUGH 23,000 FT. THEY EXPERIENCED A RAPID DEPRESSURIZATION, LOSS OF CABIN PRESSURE (O2 MASKS WERE DONNED BY FLT CREW). CREW MANUALLY CLOSED OUTFLOW VALVE HOWEVER AIRCRAFT WOULD NOT PRESSURIZE. CREW REQUESTED DESCENT AND RETURN TO BASE - NSDR CA030527002Bypass Valve · malfunctioned(CAN) ON TOP OF CLIMB NR 1 ENGINE OIL FILTER BY-PASS CAME ON STEADY. CHECK LIST WAS PERFORMED AND LIGHT REMAINED ON. ENGINE SHUT DOWN HAD TO BE COMPLETED AS PER QRH, AIRCRAFT RETURNED TO TORONTO.SDR CA030331004Line · leaking(CAN) ON DEPARTURE, OIL QUANTITY ON NR 2 ENGINE AT OR NEAR ZERO AS THEY PASSED THROUGH 300 FT. CREW ELECTED TO CONTINUE FLT & MONITOR. PASSING THROUGH 22,000 FT. OIL PRESSURE STARTED TO FLUCTUATE, CREW IMMEDIATELY CONDUCTED ENG SHUTDOWN CHECKLIST. A/C RETSDR CA030204001Control Panel · smoke(CAN) AT 33000 FT, SMOKE WAS NOTICE COMING FROM THE OVERHEAD COCKPIT FUEL PANEL P5-2. PUMPS SELECTED OFF. DECLARED AN EMERGENCY LANDING. REPLACED PANEL.SDR CA021213001Static Inverter(CAN) DATE OF REMOVAL NOV 25/02 DATE OF ARRIVAL IN SHOP SNAG DESCRIPTIONWHEN CONDUCTING W/C 12010 ITEM 8 B737 DAILY CHECK,STNDBY PWR CHECK AC VOLT METER FULL DEFLECTING RIGHT 130 VOLTS. #1 AND 2 AUTO XFMR C/B POPPED AND CADC AC & 26VAC C/BS POPPED, UNABLE TO SDR CA030103022Static Inverter · malfunctioned(CAN) WHEN CONDUCTING AN EMERGENCY POWER CHECK THE AC VOLT METER WENT FULL DEFLECTION TO 130 VOLTS. NR 1 AND 2 AUTO TRANFORMER C/B POPPED AND CADC AC AND 26 VAC C/B'S POPPED. SHOP REPORT CONFIRMED THE FAULT THAT THE INVERTER WAS PUTTING OUT 155 VAC. THIS WASSDR CA021115011Engine · failed(CAN) DURING TAKEOFF AT HIGH SPEED, CREW EXPERIENCED TWO BANGS. TAKEOFF REJECTED AT 140 KNOTS. NR 2 ENGINE REPLACED AND HIGH ENERGY STOP INSPECTION CARRIED OUT AS PER MM 05-51-11 PARA D.SDR CA020830022Engine · vibration(CAN) RT ENGINE VIBRATION FELT FROM TOP OF DESCENT TO LANDING. NR 2 FUEL LEVER VIBRATING AND DURING TAXI WHEN POWER ADDED. TURBINE VIBRATION GOES UP TO 2.5 TO 3.SDR CA020826007Fuel Control · failed(CAN) ON LANDING ENGINE 1 AND 2 ONLY GO INTO IDLE REVERSE. UNABLE TO PULL ANY REVERSE POWER. NR 1 ENGINE FCU REPLACED AND CHECKED SERVICEABLE AS PER AMM.SDR CA020731009Controller · malfunctioned(CAN) OUTER PANE OF F/O,S NR 1 FORWARD WINDOW CRACKED AND DELAMINATED WHILE CRUSING AT 330. ALTITUDE REDUCED, DIFFERENTIAL REDUCED AS PRECAUTION. F/O,S WINDOW AND HEAT CONTROLLER REPLACED AS PER AMM.SDR CA020610005Gasper Fan · failed(CAN) WHILE BOARDING PAX. SMOKE STARTED ENTERING CABIN IN MID-CABIN RIGHT SIDE AREA.(L1251724)PAX. DEPLANED VIA FWD ENTRY DOOR. FOUND GASPER FAN CONNECTOR & FUSILAGE INSULATION BLANKET BURNT. REPLACED AIR COND. MODULE & CIRCUIT BREAKER AS PER STANDARD PRACTICESDR CA020606002Keelbeam · corroded(CAN) FUSELAGE SKIN BULGED AND SUSPECT CORROSION RT KEELBEAM STA 520 STR 28 RT ALSO RIVETS HEADS SHEARED AND LOOSE STA 480 TO STA 520 (M1121878) SKIN CUT AND CORROSION REMOVED AS PER SRM 53-30-3 FIG 1.KEELBEAM STA 520 STR 28 RT WITHIN LIMITS AFTER CORROSION RESDR CA020725009Engine · failed(CAN) ON DEPARTURE FROM OTTAWA, CLIMBING THROUGH FL 270 TO 280, A LOUD BANG WAS HEARD AND A SHUDDER CAME FROM NR 1 ENGINE, POWER WAS REDUCED AND ENGINE WAS SHUT DOWN, OTHER THAN FLUCTUATING VIBRATION, OTHER PARAMETERS NORMAL.NUMBER ONE ENGINE REPLACED. MORESDR CA020531005Engine · failed(CAN) PRELIMINARY REPORT, NR 1 ENGINE SHUT DOWN , ENGINE STARTED ROUGH WITH VIBRATION , ANTI-SELECTED OFF WITH NO CHANGE,AIRCRAFT LANDED WITHOUT ANY INCIDENT. FOUND ENGINE TURBINE DAMAGEDSDR CA020528011Circuit Breaker · failed(CAN) ON DESCENT LOST THE NR 2 AND 3 TRANSFORMER RECTIFIERS, ONE FUEL PUMP ON THE NR 1 TANK AND BOTH FUEL PUMPS ON THE NR 2 TANK ALSO F/O'S INSTRUMENTS AND NR 2 RADIO. CREW NOTICED SLIGHT ELECTRICAL SMELL AND ON BASE LEG THE TRANSFER BUS LIGHT CAME ON. CAPTASDR CA020507001Transformer · malfunctioned(CAN) DURING FLIGHT NUMEROUS MOMENTARY POWER INTERUPTION CAUSING AUTO PILOT TO DISENGAGE AND NUMEROUS INSTRUMENT WARNING FLAGS. FOUND TO BE THE NR 1 ENGINE CURRENT TRANSFORMER AT FAULT. TRANSFORMER REPLACED. AIRCRAFT TIME 53656HRSSDR CA020502017Fuel Control · failed(CAN) 1ST ATTEMPT AT TAKEOFF NR 1 ENGINE STALLED AT APPROXIMATELY 1,70 EPR.RETURNED TO RAMP FOR MAINTENANCE (MAINTENANCE CHECKED AIRCRAFT SERVICEABLE). 2ND ATTEMPT TAKOFF NR 1 ENGINE STALLED TWICE BETWEEN V1 AND GEAR UP. IN BOTH CASES WHILE NR 1 ENGINE ACCELERSDR CA020502018Window · failed(CAN) ON GROUND FOUND FIRST OFFICER NR 4 WINDOW SHATTERED. RELACED NR 4 WINDOW.SDR CA020426004Latch · failed(CAN) CABIN OXYGEN PSUS NR 9 RT AND NR 14 RT, NO FLOW FOUND DURING FUNCTIONAL TEST. BOTH UNITS ARE FROM THE SAME BATCH NR. BATCH NR 99795 REPLACED LATCH ASEMBLIES.SDR CA020315006Panel · sheared(CAN) PRIOR TO DEPARTURE, FLAPS EXTENDED FOR SREVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS.FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01SDR CA020308010Panel · sheared(CAN) FLAPS EXTENDED FOR SERVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS.FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01. AIRCRAFT FERRIED FSDR CA020104009Engine · stalled(CAN) ON TAKE OFF OUT OF WHITEHORSE, FLIGHT CREW EXPERIENCED COMPRESSOR STALL. ENGINE THROTTLE BACK TO IDLE, ENGINE NORMAL, ADVANCED THROTTLE AND STALLED AGAIN. FLIGHT CREW ELECTED TO RETURNED TO WHITEHORSE. ENGINE TRIM RUN CARRIED OUT. IDLE AND EPR ADJUSSDR CA020104012Gyro · failed(CAN) ON TAKE OFF FROM EDMONTON, ELECTRICAL SPIKE MOMENTARILY FLAG CAPT.'S ADI AUTOPILOT, WHEN SELECTED ON TRIPPED, TRIED ONE MORE TIME AND WITH LIGHT PRESSURE ON ELEVATOR ON AUTOPILOT TRIPPED AGAIN. NUMBER 1 VERTICAL GYRO AND AIR DATA COMPUTER REPLACED. SYSTESDR CA010905007Module · shorted(CAN) ON LANDING IN YHZ LOWER PANEL CAUTION LIGHTS CAME ON & WOULD NOT EXTINGUISH. FOUND SCREW SHORTING TERMINAL OF LANDING GEAR WARNING INDICATION MODULE SOCKET. REMOVED SCREW AND CHECKED INDICATION SYSTEM & ASSOCIATED SYSTEMS. ALL INDICATIONS & OPEATIONS NOSDR CA010906019Valve · failed(CAN) TWO AIR TURN BACK DUE TO A #1 START VALVE OPEN LIGHT ILLUMINATED DURING FLIGHT. ACCOMPLISHED #1 ENGINE FAILURE SHUTDOWN TWICE.AFTER THE FIRST INCIDENT, THE STARTER, START VALVE AND ACTUATOR PRESSURE SWITCH WERE CHANGED, & THE SECOND TIME THE START VALVE SDR CA010622013Controller · malfunctioned(CAN) AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE IN STANDBY MODE. FLIGHT RETURNED.CABIN PRESSURZATION CONTROLLER REPLACED.SDR CA010522005Duct · separated(CAN) ON CLIMB NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. THRUST REDUCED AND LIGHT EXTINGUISHED. RETURNED. MAINTENANCE INSPECTION FOUND RIGHT ANTI-ICE DUCT SEPARATED FROM ANTI-ICE VALVE. DUCT REPLACED GROUND RUN, SYSTEM CHECKED SERVICEABLE.SDR CA010522006Case · cracked(CAN) AFTER TAKEOFF TRAILING EDGE FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS RETRACTED. FLIGHT CONTINUED, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED TRAILING EDGE FLAP BYPASS VALVE MALFUNCTIONING. VALVE REPLACED. SUBSEQUENT VALSDR CA010404010Control Unit · leaking(CAN) DURING FLIGHT A SYSTEM HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP, AT A RATE OF 1 GALLON PER HOUR. DUE TO POOR WEATHER ELECTED TO DIVERT. GEAR EXTENDED NORMALLY AND QUANTITY REMAINED STEADY. FLIGHT LANDED WITHOUT INCIDENT. FOUND A SYSTEM AILERON POWER CONTRSDR CA010313023Strut · bent(CAN) ON TAKEOFF WHEN THE GEAR WAS SELECTED UP THE CREW HEARD A BANG FOLLOWED BY A LOUD NOISE AND ACCOMPANIED BY A VIBRATION IN THE AIRFRAME. THE CREW ELECTED TO RETURN. UPON LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE NOSE GEAR ATTACHSDR CA010301022Wire · failed(CAN) IN CRUISE, LT ELEVATOR PITOT HEAT SYSTEM INDICATED HEATER SYSTEM UNSERVICEABLE. DUE TO WEATHER CONCERNS DIVERTED. REPAIRED WIRING TO LT PITOT TUBE.SDR CA010105003Transmitter · failed(CAN) EPR INDICATION UNSERVICEABLE. REPLACED INDICATOR AND TRANSMITTER. A/C RETURNED TO SERVICE.SDR CA001214004Fire Detector · failed(CAN) ON CLIMBOUT FROM YVR, CREW SAW A MOMENTARY FLASH OF NR 1 ENGINE FIRE HANDLE LIGHT. IT BECAME INTERMITTENT AS CLIMB CONTINUED. CREW ELECTED TO RETURN, REQUESTED CFR ON ARRIVAL. AFTER CLEARANCE TO RETURN RECEIVED AND DESCENT STARTED, FIRE HANDLE WARNING LISDR CA001214002Switch · failed(CAN) TOP OF CLIMB, NR 3 SLAT INTRANSIT LIGHT ON OVERHEAD PANEL AND LEADING EDGE FLAP INTRANSIT LIGHT ON, FORWARD PANEL, INTERMITTENTLY, WITH ASSOCIATED MINOR AIRFRAME VIBRATION. FLIGHT RETURNED. REPLACED NR 3 SLAT ACTUATOR RODEND SWITCH ASSEMBLY, SYSTEM CHECKSDR CA001201010Check Valve · leaking(CAN) NR 2 ''A'' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WHEN FLAPS SELECTED. DECLARED AN EMERGENCY, LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TOWED FROM RUNWAY. FOUND ''A'' SYSTEM HYDRAULIC TANK PRESSURE LEAKING FROM SERVICING PORT. CHECK VALVE CLSDR CA000901007Indicator · failed(CAN) IN CRUISE CAPTAINS HORIZONTAL SITUATION INDICATOR STOPPED TURNING WHEN AIRCRAFT WAS IN A TURN. COMPARATOR LIGHT CAME ON. RETURNED. CAPTAINS HSI REPLACED.SDR CA000901005Filter · obstructed(CAN) A/C 741, AUGUST 14/2000, FLT 906, YYC, LOG SEQUENCE 0281117. ENGINES WERE ACCELERATED FOR TAKEOFF AND NR 2 ENGINE COMPRESSOR STALL OCCURRED. TAKEOFF WAS ABANDONED AT 15 KNOTS. AIRCRAFT RETURNED TO RAMP. MAINTENANCE REQUESTED ENGINE TO BE RUN. ENGINE STALSDR CA000731003Splice · overheated(CAN) SEVERAL RPTS OF REJECTED TAKEOFFS, DUE TO NR 1 GEN DROPPING OFF LINE & LEADING EDGE DEVICES INTRANSIT LIGHT ILLUMINATING. INSP FOUND, NR 1 ENGINE GEN AL TO CU SPLICE OVERHEATED. SPLICE LOCATED AT WING STATION WBL 157, ABOVE ENGINE ELECT. DISCONNECTS IN DSDR CA000804015Tire · failed(CAN) CREW REPORTED LOUD BANG FROM NOSE WHEEL AREA ON TAKEOFF ROLL AND JUST BEFORE ROTATION. THEY ALSO NOTICED SOMEHTING GO PAST THE WINDSCREEN. A FLY PAST THE CONTROL TOWER AND DEBRIS FOUND ON THE RUNWAY CONFIRMED TREAD SEPARATION FROM ONE OF THE NOSE WHEEL TSDR CA000718006Circuit Breaker · failed(CAN) NEARING TOP OF CLIMB, CIRCUIT BREAKERS BEGAN TO TRIP. FUEL PUMP CIRCUIT BREAKERS FOR LEFT SIDE, TCAS, STALL WARNING, EQUIPMENT COOLING, WINDOW ANTI-ICE, RADIO ALTIMETER. RETURNED TO YUL, NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. REPLACED NR 1 GENERSDR CA000731004Connector · loose(CAN) ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND FIRE AND OVERHEAT ESDR CA000718008Connector · loose(CAN) 85 MILES OUT OF MEM, NR 2 ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED TO MEM. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INC
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