Boeing 737-7CT
Service difficulty reports · 2,415
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 = '7377CT' 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 = '7377CT' 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 CA130404002Window · cracked(CAN) ON DEPARTURE, WINDOW CRACKED AND ACFT RETURNED FOR LANDING. R1 WINDOW WAS REPLACED IAW AMM 56-11-11 AS WELL AS THE WINDOW HEAT CONTROLLER, PN: 83000-05604, SN: 9428D.SDR CA130318017Flap System · faulted(CAN) DURING APPROACH THE FLIGHT CREW REPORTED A T/E FLAP DISAGREE AND SHUTDOWN PRIOR TO 1 UNIT. THE APPROPRIATE NON-NORMAL CHECKLIST WAS CARRIED OUT ENABLING THE CREW TO DEPLOY THE FLAPS TO 15 UNITS USING THE ALTERNATE METHOD. AN EMERGENCY LANDING WAS DECLARESDR CA130225016Unknown · odor(CAN) AFTER TAKEOFF CLIMBING THROUGH 10,000 FT ON FLIGHT 611 A STRONG ELECTRICAL BURNING SMELL WAS NOTED IN THE FLIGHT DECK. F/A IN THE CABIN ALSO REPORTED TO THE FLIGHT CREW A STRONG BURNING ODOR IN THE CABIN BUT THERE WAS NO VISIBLE SMOKE. THE CREW ELECTEDSDR CA130128021Processor · failed(CAN) CREW REPORTED THAT THEY HAD AN ATC NR 1 AND NR 2 FAILURE. CREW ALSO REPORTED TCAS FAILURE. DUE MEL RESTRICTIONS FOR DUAL ATC FAILURE, ACFT WAS UNABLE TO CONTINUE FLIGHT AND DIVERTED. MAINTENANCE CARRIED-OUT TROUBLESHOOTING, THEY FOUND TCAS COMPUTER ATSDR CA130123008Actuator · failed(CAN) IN CRUISE A HIGHER THAN NORMAL FUEL IMBALANCE TREND WAS NOTICED. THE CREW CONFIRMED THE CROSSFEED CIRCUIT BREAKER WAS POPPED AND THEY WERE UNABLE TO CORRECT THE IMBALANCE USING THE FUEL CROSS FEED SYSTEM. DUE TO THE DURATION OF THE REMAINING FLIGHT AND SDR CA130117009Sensor · failed(CAN) DURING APPROACH THE FLIGHT CREW REPORTED THE FLAPS FAILED TO EXTEND WHEN SELECTED. A GO-AROUND WAS CARRIED OUT AND THE T/E FLAP ASYMMETRY NON-NORMAL CHECKLIST WAS COMPLETED. THE ACFT MADE AN UNEVENTFUL LANDING WHERE IT WAS THEN MET BY MAINTENANCE. MAISDR CA130116017Heater · failed(CAN) DURING CLIMB THE F/O`S SIDE WINDOW ELEMENT WAS GLOWING ORANGE AND SEVERAL WHITE FLASHES WERE NOTICED. THE R2 WINDOW HEAT WAS TURNED OFF AND ALL VISIBLE INDICATIONS CEASED. FLIGHT CONTINUED. TECH OPS PERFORMED WINDOW HEAT OPS TEST IAW AMM 30-40-00 AND SDR CA130111001Sliding Window · failed(CAN) JANUARY 10, 2013 FLIGHT 1207 WHILE AT THE GATE, THE R2 WINDOW SHATTERED. THE ASSOCIATED OVERHEAT ANNUNCIATOR ALSO ILLUMINATED. THE F/O NR 2 WINDOW WAS REPLACED IAW AMM 56-12-11.SDR CA121221004Indication Sys · failed(CAN) DURING CLIMB WHILE FOLLOWING NORMAL PROCEDURES THE FLIGHT CREW REPORTED BOTH LOW PRESSURE LIGHTS FOR THE CENTER FUEL TANK PUMPS FAILED TO EXTINGUISH WHEN THE PUMPS WERE SELECTED ON. THE FLIGHT CREW IN CONJUNCTION WITH OPS DECIDED TO DIVERT TO A BASE WHESDR CA121220004Monitor · odor(CAN) PASSENGER REPORTED SMELLING SMOKE FROM TV SCREENS 23 E & F. IFE WAS SELECTED TO OFF AND FLIGHT CONTINUED WITH NO FURTHER INCIDENCE. MAINTENANCE CONTROL REQUESTED CABIN SMOKE INSPECTION BE CARRIED OUT IAW FIM 21-00, TASK 806 NO FAULT WHERE FOUND. LIVE SDR CA121205010Control Panel · failed(CAN) UNABLE TO ENGAGE EITHER AUTO-PILOT AFTER TAKEOFF. WITH NO AUTO PILOT, WE CANNOT FLIGHT RVSM. CREW WAS DIVERTED FOR MAINTENANCE. SEVERAL SECONDS AFTER TAKEOFF BOTH FLIGHT DIRECTORS DISAPPEARED ON CAPTAIN & F/O PRIMARY FLIGHT DISPLAYS. MODE CONTROL PANESDR CA121205008Gcu · failed(CAN) CREW REPORTED THAT NR 2 GENERATOR WAS OFFLINE AND WOULD NOT RESET ALSO THEY HAD A STRANGE ODOR IN THE CABIN. CREW DIVERTED FOR MAINTENANCE. MAINTENANCE FOUND NR 2 GENERATOR CONTROL UNIT UNSERVICEABLE. GCU WAS REPLACED IAW MM 24-21-81. ENGINE RUNS ANDSDR CA121126011Pitot System · malfunctioned(CAN) ON TAKEOFF AT 70 KNOTS, CREW OBSERVED AN IAS INDICATED AIRSPEED DISAGREE MESSAGE ON BOTH PRIMARY FLIGHT DISPLAYS. TAKEOFF WAS ABANDONED. MAINTENANCE PERFORMED FIM 31-62, TASK 876. FOUND RT, F/O PITOT SYS SLOW TO RESPOND AND LAGGING BY 4-6 KNOTS AT ALLSDR CA121120008Release Pin · failed(CAN) UPON ARRIVAL THE L1 DOOR WAS JAMMED AND WOULD NOT OPEN. INSPECTION FOUND THE GUIDE ARM RELEASE PIN, BROKEN. RELEASE PIN AND ATTACHING HARDWARE WAS REPLACED AND FUNCTIONAL CHECK WAS CARRIED OUT ON THE L1 DOOR WITH NO FAULTS FOUND. REPLACED PARTS: RELEASSDR CA121113001Regulator · failed(CAN) FLIGHT CONTACTED MAINTENANCE TO REPORTING DUCT PRESSURE AT 5 PSI ON CLIMB AND AT 10 PSI IN CRUISE. ACFT DIVERTED FOR MAINTENANCE. ENGINE BLEED AIR SYS HEALTH CHECK CARRIED OUT ON NR 2 ENGINE. HEALTH CHECK REVEALED EXCESSIVE AIR LEAKING FROM BAR. BLEEDSDR CA121106002Unknown · fumes(CAN) AFTER LANDING, F/A AND PILOT REPORTED A STRONG BURNING/CHEMICAL ODOR IN CABIN AND FLIGHT DECK. THE APU AND BLEED WAS NOT CONSIDERED THE SOURCE AT THAT TIME. MAINTENANCE WAS DISPATCHED AND CARRIED OUT FIM 21-00, TASK 806, SMOKE OR FUME IN CABIN, SOURCE USDR CA121101003Switch · inoperative(CAN) FOLLOWING DEPARTURE, THE FLIGHT CREW WAS UNSUCCESSFUL IN RETRACTING THE LANDING GEAR. AFTER NON-NORMAL CHECKLIST COMPLETION, THE GEAR WAS STILL UNABLE TO BE RETRACTED. THE FLIGHT CREW CARRIED OUT AN AIR TURN BACK FOLLOWED BY AN UNEVENTFUL LANDING. MAINSDR CA121031006Sliding Window · failed(CAN) WHILE ON THE GROUND THE F/O`S NR 2 WINDOW OVERHEATED AND SHATTERED. THE WINDOW WAS REPLACED IAW AMM 56-12-11 AND TESTED SERVICEABLE. R2 WINDOW ASSY PN: 141A4810-39, SN:09127H9878 WINDOW PANE, PN: 5-89355-88, SN:0912H8978.SDR CA121022018Entertain Sys · odor(CAN) SHORTLY AFTER T/O, F/A REPORTED STRONG FUMES AND SMOKE NEAR MID-CABIN. SMOKE, FUMES, ODOR EMERGENCY CHECKLIST CARRIED OUT. FUMES AND SMOKE STARTED TO CLEAR. ACFT DID AN AIR TURNBACK. MAINTENANCE CARRIED OUT FIM 21-00, TASK 806 WITH NO EVIDENCE OF SMOKSDR CA121009015Wire · broken(CAN) CREW ABORTED TAKEOFF DUE TO RT OVERWING EXIT LIGHT ON. FIM TASK 52-20, TASK 801 C/O INCLUDING CHECK OF SOLENOID AND LOCK SWITCH OPERATION WITH NO FAULTS FOUND. DEFECT H77476, FLIGHT WAS ABORTED AGAIN DUE TO REOCCURRENCE OF THE RT OVERWING EXIT LIGHT ONSDR CA121009008Control Module · failed(CAN) DURING CRUISE, CREW DETECTED A ODOR OF HOT RUBBER IN AFT CABIN, ODOR WAS NARROWED DOWN TO TV SCREEN 18D. F/A`S TURNED TV POWER AND IFE/PASS SWITCH OFF AND THE ODOR DISSIPATED. LTV ELECTRICAL ODOR SYS INTEGRITY CHECK WAS CARRIED IAW LTV AMM 44-20-28. SSDR CA121009009Indicator · failed(CAN) DURING APPROACH WHEN THE FLIGHT CREW SELECTED FLAPS 1, THE L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. SOME FLAP ASYMMETRY WAS ALSO INDICATED ON THE FLAP POSITION GAUGE FOR A SHORT TIME BUT WAS LESS THAN 1 DEGREE LEVELING OFF AT AROUND .5 DEGREES SEPASDR CA121009007Line · leaking(CAN) DURING CRUISE THE FLIGHT CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. THE SYSTEM QTY WAS SUBSEQUENTLY CHECKED AND FOUND TO BE AT 21 PERCENT. THE FLIGHT CREW CARRIED OUT THE APPROPRIATE CHECKLIST AND THEN MADE AN UNEVENTFUSDR CA121002004Switch · failed(CAN) FOLLOWING A DEPARTURE, THE CREW WAS UNSUCCESSFUL IN RETRACTING THE LANDING GEAR. UPON COMPLETION OF THE NON-NORMAL CHECKLIST, THE GEAR WAS STILL UNABLE TO BE RETRACTED. THE CREW ADVISED ATC OF THE SITUATION AND RECEIVED VECTORS TO HOLD NORTH OF THE AIRSDR CA120924008Window · failed(CAN) CREW CARRIED OUT AN AIR TURNBACK DUE TO THE FO NR 2 WINDOW OUTER PANE SHATTERED DURING CLIMB. WINDOW WAS REPLACED IAW AMM 56-12-11.SDR CA120919007Pin · failed(CAN) THE L1 DOOR MAIN CABIN DOOR JAMS AT PARTIALLY OPEN POSITION. THE L1 GUIDE ARM RELEASE MECHANISM, GUST LOCK, PIN WAS FOUND FOUND TO BE FALLING APART INSIDE THE DOOR AND WAS REPLACED ALONG WITH ATTACHING HARDWARE. PIN, PN: 141A6076-1.SDR CA120904006Door · not closed(CAN) CREW PREFORMED AN AIR RETURN WHEN THE ACFT DID NOT PRESSURIZE DUE TO THE MAIN CABIN DOOR NOT BEING LATCHED PROPERLY WITH NO INDICATION IN THE FLIGHT DECK. MAINTENANCE CARRIED OUT L1 DOOR INSPECTION AND FOUND FWD PARTITION FOAM FILLER OUT OF PLACE AND OBSSDR CA120830003Fan · failed(CAN) FLIGHT CREW REPORTED THAT 3 TIMES ON DECENT THAT THERE WAS A SMELL OF HOT ELECTRICAL IN THE FLIGHT DECK. F/A ALSO REPORTED THE ELECTRICAL SMELL WAS PRESENT ON THE GROUND. FIM 21-00 WAS CARRIED OUT WITH NO EVIDENCE OF SMELL OR FUMES. THEN WHILE ON THE SDR CA120820007Wire Harness · failed(CAN) IN CLIMB, THROUGH 38,000 FT THE PILOTS REPORTED THE LT BLEED TRIP LIGHT ILLUMINATED. THE TRIP RESET PROCEDURE WAS UNSUCCESSFUL AND THE CREW PERFORMED AN AIR TURN BACK WHERE THE ENGINE WIRE HARNESS FOR THE BLEED AIR REGULATOR, MW 0311, WAS FOUND TO BE ATSDR CA120813032Limit Switch · dirty(CAN) AFTER TAKEOFF, ALL 3 LANDING GEAR DID NOT MOVE UP WHEN SELECTED BY THE FLIGHT CREW ILLUMINATING 3 GREEN AND 3 RED LANDING GEAR LIGHTS. THE GEAR NOT IN POSITION, NON NORMAL CHECKLIST WAS CARRIED OUT AND THE GEAR STOWED PROPERLY ON THE SECOND ATTEMPT. TO SDR CA120727016Controller · failed(CAN) ON TAKEOFF, AN ISSUE WITH THE CABIN PRESSURIZATION SYS RESULTED IN THE MASTER CAUTION, AUTO FAIL, AND ALTN PX LIGHTS TO ILLUMINATE. THE CREW ABORTED THE TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE FOR TROUBLESHOOTING WHERE THE NR 2 CABIN PRESSURE CONTRSDR CA120705003Landing Gear · malfunctioned(CAN) AIR TURNBACK. DURING TAKEOFF, AFTER THE LANDING GEAR LEVER WAS SELECTED UP, THE FLIGHT CREW NOTICED ALL 3 RED LANDING GEAR POSITION LIGHTS ILLUMINATE. THE CREW THEN DECIDED TO POSITION THE GEAR LEVER TO OFF AND THEN RESELECT GEAR UP. BY DOING SO THE LASDR CA120704011Light · burned out(CAN) DURING APPROACH, THE FLIGHT CREW EXPERIENCED AN INDICATED LANDING GEAR POSITION DISAGREE AFTER SELECTING GEAR DOWN. WHEN SELECTING GEAR DOWN ON APPROACH, THE RT MAIN GEAR INDICATED AN UNSAFE GEAR NOT LOCKED DOWN, RED-LIGHT WITH NO ASSOCIATED GREEN-LIGHTSDR CA120627008Pressure Switch · malfunctioned(CAN) DURING THE FLIGHT, THE CREW DIVERTED DUE TO THE RT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATING. ALL ENGINE PARAMETERS REMAINED NORMAL AND THE ACFT LANDED UNEVENTFULLY. MAINTENANCE CARRIED OUT FIM 73-05, TASK 801 AND FAULTED SWITCH PART NR QA07995. FUSDR CA120523014Fire Warning · activatedCREW REPORTED AN AFT CARGO FIRE INDICATION, AND FIRE BOTTLE WAS DISCHARGE. MAINTENANCE WAS UNABLE TO FIND FAULT WITH DETECTION SYS. ALL SMOKE DETECTORS IN THE AFT CARGO PIT WHERE REPLACED ALSO DISCHARGED BOTTLE AND DRIER WERE REPLACED IAW MM. ON SUBSEQUENT SDR CA120510006Door · lack of lube(CAN) L2 DOOR WAS DIFFICULT TO OPEN, BINDS APPROXIMATELY 90 DEGREES OPEN. THE UPPER AND LOWER DOOR HINGES WERE LUBRICATED IAW AMM 12-25-11 AND FUNCTION CHECK OF THE L2 DOOR WAS CARRIED OUT IAW AMM 52-13-00. DOOR SWUNG NORMALLY FOLLOWING LUBE. CURRENTLY REVISDR CA120501003Valve Stem · leaking(CAN) WHILE MAINTENANCE WAS CARRYING OUT TASK CARD DAILY, CK 737NG, IT WAS DISCOVERED THAT THE NR 1 MAIN WHEEL TIRE PRESSURE WAS BELOW SERVICEABLE LIMITS AT 105 PSI AND WAS LEAKING NITROGEN FROM THE VALVE STEM AREA. AS A RESULT BOTH NR 1 AND NR 2 MAIN WHEELS SDR CA120501002Rod End · worn(CAN) DURING TAKEOFF CABIN WOULD NOT PRESSURIZE DUE TO L1 DOOR NOT LATCHING PROPERLY. CREW RETURNED WHERE MAINTENANCE FOUND THE L1 DOOR GUIDE ARM ROD END AND BOLT WORN AND WAS REPLACED IAW AMM 52-11-00.SDR CA120430014A/C Pack · smoke(CAN) DURING TAKEOFF IN NORMAL CONFIGURATION, THE FLIGHT CREW REPORTED A STRONG ODOR IN THE CABIN AND A POSSIBLE PRESENCE OF SMOKE. THE FLIGHT CREW ELECTED TO PERFORM AN AIR TURNBACK AND RETURN TO THE DEPARTURE WHERE THEY WOULD BE MET BY FIRE AND RESCUE. THE SDR CA120430013Window · failed(CAN) WHILE ON THE GROUND, CAPT`S L2 WINDOW CRACKED AND OVERHEAT LIGHT ILLUMINATED. THE L2 WINDOW WAS REPLACED IAW AMM 56-12-11. ALSO THE WINDOW CONTROL UNIT WAS REPLACED IAW AMM 30-41-11. PN OFF: 83000-05604, SN OFF: 14883D WILL UPDATE WITH TEARDOWN INFO WHENSDR CA120420008Apu · failed(CAN) FLIGHT CREW REPORTED THAT ANOTHER ACFT NOTICED, MORE SMOKE THAN NORMAL, COMING FROM THE APU TAIL PIPE ON SHUTDOWN. NO OTHER INDICATIONS WERE REPORTED BY THE FLIGHT CREW. CRASH, FIRE, RESCUE ATTENDED THE ACFT ON THE TAXIWAY AND AFTER FINDING NO INFRA REDSDR CA120417019Oil Tank · cracked(CAN) AFTER LANDING AND ON TAXI TO THE GATE A TRAIL OF OIL WAS NOTICED FROM THE NR 1 ENGINE. MAINTENANCE INVESTIGATED AND FOUND A 2" CRACK AT THE BOTTOM OF THE ENGINE OIL TANK. THE OIL TANK ASSEMBLY WAS REPLACED IAW AMM 79-11-01.SDR CA120416002Adiru · failed(CAN) AIR TURNBACK DUE IRS INOPERATIVE. ACFT HAD NR 2 IRS INOPERATIVE. RT IRS FAULT LIGHT ILLIMINATED IN FLIGHT. NR 2 ADIRU REPLACED AND TESTED SERVICABLE IAW MM 34-21-01. THIS DIVERSION WAS OPS IN NATURE DUE TO PARTS AND MANPOWER AVAILABILITY AT BASES IN SDR CA120330009Snubber · damaged(CAN) ON OPENING OF THE AFT ENTRY DOOR, L2, IT JAMMED HALF WAY AND REQUIRED JOSTLING OF THE DOOR FOR IT TO FULLY OPEN. THE L2 DOOR SNUBBER WAS ADJUSTED AND RESOLVED THE FAULT. AS A PREVENTATIVE MEASURE AN OPEN DEFECT WAS RAISED AND THE SNUBBER REPLACED.SDR CA120323003Door · false indication(CAN) ON TAKEOFF, RT OVERWING EXIT LIGHT ILLUMINATED WHEN POWER WAS APPLIED FOR TAKEOFF. TAKEOFF WAS ABORTED. NO FAULTS WERE FOUND ON THE PSEU, DOOR SWITCHES WERE INSPECTED, RIGGING CHECKED AND NO FAULTS WERE FOUND. NO FAULTS WERE NOTICED ON LAST 9 FLIGHT LEGSDR CA120228013Module · failed(CAN) THE ACFT HAD A REJECTED TAKEOFF DUE TO FUEL CROSSFEED, VALVE OPEN, LIGHT ILLUMINATING AT APPROXIMATELY 40 KNOTS. THE FUEL SYSTEM MODULE, P5-2 WAS REPLACED AND SYSTEM TESTED SERVICABLE.SDR CA120227008Motor · failed(CAN) ON APPROACH, THE FLIGHT CREW SWITCHED THE FLAP SYS INTO ALTERNATE MODE & NOTED THE LE SLATS DEPLOYED TO FULL EXTEND POSITION BUT TE FLAPS WOULD STILL NOT DEPLOY PASSED 5 UNITS. THE ACFT MADE A SAFE LANDING UNDER THIS CONFIGURATION. CARRIED OUT AN FSEU SDR CA120227006Transmitter · malfunctioned(CAN) AN ACFT ON APPROACH EXPERIENCED A FLAP ASYMMETRY CONDITION CAUSING THE TE FLAPS TO LOCK & NOT EXTEND PASSED 5 UNITS. DUE TO THE INITIAL FLAP SELECTION LOCKING THE LE IN THE MID-EXTEND POSITION & WEATHER CONDITIONS, ELECTED TO DIVERT WHERE INCREASED FUELSDR CA120215005Connector · contaminated(CAN) AIR TURNBACK DUE TO C/B P6-2, D19 TRIM CONTROL. RUD POPPED DEFECT STATES: RUDDER TRIM CONTROL C/B FOUND POPPED RESOLUTION STATES: INSPECTED RUDDER TRIM ACTUATOR CONNECTOR D2932, FOUND GLYCOL PUDDLES IN THE VICINITY. CLEANED CONNECTOR AND FUNCTION CHECSDR CA120131001Tire · failed(CAN) AN ACFT FLYING, EXPERIENCED A NR 1 MAIN WHEEL FAILURE WHILE LANDING DURING INITIAL BRAKE APPLICATION IN GUSTY CONDITIONS. AFTER THE ACFT CAME TO A COMPLETE STOP ON THE RUNWAY, THE FLIGHT CREW ELECTED TO POWER OFF TO A TAXI WAY WHERE THEY COULD SAFELY BE
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