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 CA140325001Window · cracked(CAN) WHILE IN CRUISE, EN-ROUTE CREW REPORTED THE L1 WINDOW OUTER PANE SHATTERED. FLIGHT CARRIED ON TO ITS DESTINATION WHERE THE L1 WINDOW ASSEMBLY WAS INSPECTED & WAS REPLACED IAW AMM 56-11-1.SDR CA140320007Valve · failed(CAN) AFTER DEPARTURE, THE FLIGHT CREW REPORTED THE LT BLEED TRIP OFF LIGHT ILLUMINATED. THE BLEED SYS WAS RESET & SHORTLY AFTER TRIPPED AGAIN. THE ACFT DIVERTED & SUCCESSFULLY LANDED. MX CARRIED OUT THE FOLLOWING ACTIONS BEFORE RETURNING THE ACFT TO SERVICSDR CA140313014Display · failed(CAN) ON DESCENT CREW REPORTED FAILURE OF THEIR ISFD. FLIGHT OPERATIONS DECIDED TO DIVERT ACFT FOR MAINTENANCE. ISFD CIRCUIT BREAKER FOUND OPEN ON ARRIVAL, P18-2, PANEL, IT WAS RESET AND THE IFSD WAS REPLACED IAW AMM 34-13-01. THERE WAS NO HISTORY OF PROBLESDR CA140312006Brake Assy · failed(CAN) MAINTENANCE DISCOVERED DURING ROUTINE MAINTENANCE A SEVERELY DAMAGED BRAKE ASSEMBLY. DAMAGE TO THE BRAKE PREVENTED THE MAIN WHEEL FROM BEING REMOVED FROM THE BRAKE AND THE WHEEL AND BRAKE ASSY HAD TO BE REMOVED TOGETHER. PIECES OF THE DAMAGED BRAKE WERE SDR CA140303004Unknown · smoke(CAN) UPON ARRIVAL AND SHUTDOWN OF ENGINES WHEN APU PUT ON BUSES COCKPIT AND AFT GALLEY FILLED WITH SMOKE, THERE WAS MORE SMOKE IN COCKPIT AND WAS BELIEVED TO BE RESIDUAL DE-ICE FLUID FROM APU INTAKE. SMOKE AND FUMES DISIPATED WITHIN 2-3 MINUTES - THERE WAS ASDR CA140225012Unknown · smoke(CAN) UPON ENTERING ACFT AT GATE, SMOKE WAS IN REAR OF CABIN, THEN STARTED AT FRONT, FILLING CABIN WITH SMOKE FROM FRONT TO BACK. DUE TO APU RUNNING, PACKS OFF. HEAVY DE-ICING WAS CARRIED OUT. SWEET SMELL OF SMOKE OBSERVED. PACKS RAN AND CABIN CLEARED. GENSDR CA140129007Sliding Window · failed(CAN) FO`S NR 2 SLIDING WINDOW SHATTERED WHILE AT THE GATE. R2 WINDOW WAS REPLACED IAW AMM TASK 56-12-11-000-801 AND TASK 56-12-401-801. FUNCTION TEST SERVICEABLE.SDR CA140121005Fuel Sys · leaking(CAN) DURING TAKEOFF ABOVE 80KTS AIR TRAFFIC CONTROL ADVISED THE FLIGHT CREW OF FUEL LEAKING FROM THE NR 2 ENGINE. THE FLIGHT CREW REJECTED THE TAKEOFF AND SAFELY RETURNED BACK TO THE GATE. MAINTENANCE TRACED THE LEAK BACK TO THE RT SURGE TANK VENT. THE FOLSDR CA140120015Display · failed(CAN) MCC HAS BEEN ADVISED THAT ACFT CONDUCTED AN AIR TURN BACK DUE TO A DISPLAY SOURCE ANNUNCIATION PREVENTING THEM FROM CONDUCTING A REQUIRED CAT IIIA APPROACHED IN POSSIBLE CAT IIIA CONDITIONS. NR 2 DEU WAS REPLACED AND TESTED SERVICEABLE IAW MM 31-62-21. SDR CA140115001Valve · failed(CAN) IN CRUISE, FLIGHT CREW REPORTED THE NR 2 BLEED TRIP OFF LIGHT ILLUMINATE. THE CREW COMPLETED THE BLEED TRIP CHECKLIST AND SUCCESSFULLY RESET THE SYSTEM. 10 MINUTES LATER THE NR 2 BLEED TRIP OFF LIGHT ILLUMINATED AGAIN. THE CREW REPEATED THE CHECKLIST SDR CA140102002Acm · seized(CAN) AFTER TAKEOFF CLIMBING THROUGH 500FT STRONG ODOR OF BURNED RUBBER WAS NOTICED IN THE FLIGHT DECK FOLLOWED BY A CALL FROM THE F/A`S THAT THE SAME WAS OCCURRING IN THE CABIN. F/A`S REPORTED A HAZE IN THE CABIN. LASTED FOR ABOUT 30-40 SECS AND THEN DISSIPASDR CA131224001Transmitter · failed(CAN) AFTER TAKEOFF THE FLAPS WOULD NOT RETRACT FROM 1 UNITS TO 0 UNITS. ALTERNATE FLAPS EXTENSION TO 15 UNITS WAS CARRIED OUT AND THE ACFT LANDED WITHOUT INCIDENT. MAINTNENACE CARRIED OUT THE APPLICABLE FAULT ISOLATION PROCEDURES AND FOUND A FAULT WITH THE LSDR CA131211004Fan · failed(CAN) DURING FLIGHT, CREW REPORTED: BURNING ELECTRICAL ODOR UPON TAXI AND SHUTDOWN, ODOR NOTICED IN COCKPIT. FORWARD, AFT GALLEY. LIVETV SYSTEM WAS PUT ON MEL. LIVETV ELECTRICAL ODOR SYS INTEGRITY CHECK WAS CARRIED OUT. NO ODORS NOTED. SCREENS AT 5A AND 10SDR CA131209003Water System · leaking(CAN) ADIVERTED DUE TO A SUSPECTED POTABLE WATER LEAK. MAINTENANCE CARRIED OUT THE FOLLOWING ACTIONS BEFORE THE AIRCRAFT WAS SUCCESSFULLY RETURNED TO SERVICE. FOUND POTABLE WATER DRAIN IN AFT GALLEY R/H SIDE IN ON POSITION CAUSING ALL POTABLE WATER TO DRAIN OUSDR CA131203002Switch · failed(CAN) AT THE TOP OF CLIMB THE NR 2 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. ENGINE PARAMETERS REMAINED NORMAL. IAW THE FLIGHT OPERATIONS MANUAL THE CREW DECIDED TO RETURN TO DEPARTURE. THE FUEL FILTER SWITCH WAS REPLACED IAW AMM 73-34-01 AFTER A SUBSEQSDR CA131127002Anti-Ice Valve · failed(CAN) DURING CRUISE THE FLIGHT CREW REPORTED THE TAI INDICATION ON THE NR 2 ENGINE REMAINED AMBER WHEN SELECTED ON. DUE TO FORECASTED ICING CONDITIONS THE FLIGHT CREW DECIDED TO DIVERT TO WHERE MEL 30-3-2 COULD BE APPLIED, NR 2 ENGINE COWL ANTI-ICE VALVE INOSDR CA131126004Pressure Switch · failed(CAN) ON DEPARTURE, AUTOPILOT B WOULD NOT STAY ENGAGED. TRIED AUTOPILOT A AND IT WAS TOTALLY LOCKED OUT, B WOULD ENGAGE FOR ONLY A SECOND OR TWO. ACFT DID AN AIR TURNBACK FOR MAINTENANCE. FAULT WAS ISOLATED TO THE A SYSTEM ELEVATOR PRESSURE SWITCH. UNIT WASDR CA131120005Transmitter · failed(CAN) ON APPROACH WHEN THE FLAP HANDLE WAS MOVED FROM 5 UNITS TO 15 UNITS THE FLAPS STOPPED AT 10 UNITS. DURING ALTERNATE FLAP EXTENSION A FLAP ASYMMETRY OCCURRED AND THE FLAPS STAYED AT 10 UNITS. THE LT FLAP TRAVELED TO 15 UNITS. MAINTENANCE REPLACED THE RSDR CA131120003Switch · out of rig(CAN) AFTER TAKEOFF THE LANDING GEAR DID NOT RETRACT WHEN GEAR WAS SELECTED UP. THE ACFT DID AN AIR TURNBACK AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED WITH THE LANDING GEAR PINS INSTALLED. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS AND COULD NOT DUPLICSDR CA131120001Lavatory · failed(CAN) DURING CLIMB, THE FLIGHT CREW REPORTED BOTH LAVS TO BE INOPERATIVE. DUE TO THE LENGTH OF THE FLIGHT THE CREW ELECTED TO RETURN TO THEIR DEPARTING STATION. THE FOLLOWING MAINTENANCE WAS CARRIED OUT BEFORE THE ACFT WAS SUCCESSFULLY RETURNED TO SERVICE, WSDR CA131118014Window · failed(CAN) THE F/O NR 1 WINDOW SHATTERED WHILE IN CRUISE, FLIGHT CONTINUED WHERE THE WINDOW WAS REPLACED IAW AMM 56-11-11.SDR CA131112011Warning Light · false activation(CAN) IN THE CLIMB OUT, THE FUEL FILTER BYPASS LIGHT ILLUMINATED FOR THE NR 2 ENGINE. THE CREW COMPLETED THE NON-NORMAL CHECKLIST ASSOCIATED WITH 1 FILTER BYPASS LIGHT AND RETURNED. TROUBLESHOOTING CARRIED OUT IAW FIM 73-05, TASK 801, OPERATE IAW MEL 73-4-1. SDR CA131031002Valve · failed(CAN) DURING DESCENT THE FLIGHT CREW REPORTED A LT BLEED TRIP OFF LIGHT ILLUMINATE. THE APPLICABLE NON-NORMAL CHECKLIST WAS COMPLETED SUCCESSFULLY RESETTING THE BLEED SYSTEM. THE ACFT COMPLETED THE FLIGHT WITHOUT FURTHER INCIDENCE. MAINTENANCE CARRIED OUT THSDR CA131015007Radar · failed(CAN) FLIGHT CREW CALLED TO ADVISE MAINTENANCE CONTROL THAT THE WEATHER RADAR CB WAS POPPED. THE CREW WAS UNSURE IF THE CB HAD TRIPPED OR IF IT WAS ALREADY OUT. AFTER TALKING WITH MCC THE CREW RESET THE CIRCUIT BREAKER. THEY SNAGGED THE RESET IN LOGBOOK AND DSDR CA131010006Coffeemaker · odorTHE AFT COFFEEMAKER CIRCUIT BREAKER 1-2 POPPED, THERE WAS A ODOR OF SMOKE WHICH DISIPATED. BOTH COFFEEMAKERS WERE REMOVED AND INSPECTED. LT COFFEEMAKER CHECKED SERVICEABLE. RT COFFEEMAKER HAD DISCOLORED TERMINALS. RT COFFEEMAKER WAS REPLACED.SDR CA130930002Light · shorted(CAN) ACFT RETURNED TO GATE DUE TO SMOKE COMING FROM BACKLIGHTING OF F/O CONTROL COLUMN REMINDER UNIT. THE BRIGHTNESS WAS TURNED DOWN AND THE SMOKE STOPPED. DEFECT J55648 RAISED AND CONTROL COLUMN REMINDER UNIT REPLACED. NO FURTHER PROBLEM.SDR CA130927001Limit Switch · failed(CAN) ON DEPARTURE THE LANDING GEAR DID NOT RETRACT WHEN GEAR UP WAS SELECTED. THE AIRPLANE FLEW GEAR DOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED THE LANDING GEAR PINS AND THE ACFT WAS FERRIED. UPON INSPECTION MAINTENANCE DISCOVERED A FAULTED MASDR CA130913003Adiru · failed(CAN) ACFT ELECTED TO DO AN AIR TURNBACK DUE TO THE AVAILABILITY OF MAINTENANCE AT DESTINATION. THE ACFT EXPERIENCED AN IRS MESSAGE IN FLT VERIFY POSITION IRS. ACFT RETURNED. MAINTENANCE REPLACED THE LT ADIRU. SYSTEM WAS TESTED SERVICEABLE IAW AMM 34-21-01SDR CA130903010Control Panel · failed(CAN) THE AIRCRAFT WAS ENROUTE WHEN IT LOST COMM 1. THE ACFT RETURNED AND THE AUDIO CONTROL PANEL AND THE PTT SWITCH WERE REPLACED. THE ACFT WAS RETURNED TO SERVICE WITH NO FURTHER FAULTS.SDR CA130903006Fire Detector · malfunctioned(CAN) WHILE TAXIING IN AFTER LANDING THE AFT FIRE LIGHT CAME ON. THE CREW STOPPED THE ACFT. NO FIRE AND THE INDICATION WENT AWAY ON ITS OWN. SMOKE DAMAGE WAS FOUND ON THE LIVE TV RF DISTRIBUTION AMPLIFIER. THE LIVE TV SYSTEM AND THE AFT CARGO FIRE DETECTISDR CA130829006Warning Light · false indication(CAN) ACFT HAD A REJECTED TAKEOFF, AFTER THE FLIGHT CONTINUED, BELOW PRESSURE LIGHT ILLUMINATED AT APPROXIMATELY 70 KNOTS. MAINTENANCE TESTED THE SYSTEM WITH NO FAULTS FOUND, IAW FAULT ISOLATION PROCEDURES AND A HIGH ENERGY STOP INSPECTION WAS CARRIED OUT WITSDR CA130829005Hydraulic System · overserviced(CAN) ON TAKEOFF, THE CREW DETECTED A STRONG ODOR THROUGHOUT THE ACFT. THE ACFT RETURNED WITHOUT INCIDENT. MAINTENANCE DISCOVERED BOTH A AND B SYS HYDRAULIC RESERVOIRS SLIGHTLY OVER SERVICED. THE RESERVOIRS WERE DRAINED TO THE PROPER LEVEL AND HIGH POWER ENSDR CA130829003Trim Motor · failed(CAN) THE FLIGHT CREW REPORTED A STABILIZER OUT OF TRIM INDICATION ON DECENT. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE, IAW FAULT ISOLATION PROCEDURES, RESET SYSTEM LOGIC, REPLACED THE STABILIZER TRIM MOTOR, AND THE SYSTEM SDR CA130807009Engine · malfunctioned(CAN) ON CLIMBOUT THE CREW REPORTED HEARING A LOUD BANG FROM THE NR 1 ENGINE. THE CREW FOLLOWING QRC PROCEDURES SHUTDOWN THE ENGINE. CONFIRMATION OF THE EVENT WAS RECEIVED VIA ACMS MESSAGING WHICH REPORTED AN ENGINE FLAMEOUT AND REDLINE TEMPERATURE EXCEEDANCESDR CA130809007Fuel Control · leaking(CAN) ON ENGINE START CREW WAS ADVISED BY GROUND HANDLERS OF A LARGE FUEL LEAK WHEN STARTING NR 2 ENGINE. START TERMINATED. MAINTENANCE INVESTIGATED AND IAW AMM 71-00-00 RAN THE ENGINE FOR 5 MINUTES AND THERE WAS NO FURTHER LEAKS. RELIABILITY FOLLOW-UP ACTIOSDR CA130806004Coffeemaker · overheated(CAN) THE AFT LT COFFEEMAKER STARTED SMOKING IN FLIGHT. THE CREW REMOVED POWER TO THE COFFEEMAKER, PULLED THE ASSOCIATED CIRCUIT BREAKER AND THE SMOKE DISSIPATED. THE COFFEEMAKER WAS DIFFERED THEN LATER REPLACED. NO OTHER ISSUES WERE NOTED.SDR CA130807008Entertain Sys · odor(CAN) F/A NOTICED AN ODOR OF BURNING ELECTRICAL COMPONENT THROUGHOUT THE ACFT CABIN. THE FORWARD GALLEY POWER, LIVE TV SYS AND IFE/PASS SWITCHED TURNED OFF, SMELL DISSIPATED. LIVE TV SYSTEM PLACED ON MEL NO FURTHER REPORT OF ISSUES. SYSTEM STILL NEEDS TROUBSDR CA130726014Electrical Box · overheated(CAN) DURING ACFT TURNAROUND, THE F/A INFORMED THE CREW OF A PLASTIC/ELECTRICAL ODOR IN THE CABIN AROUND ROW 23 ABC. MAINTENANCE INVESTIGATED AND FOUND THE SEB BOX UNDER SEAT 23ABC WAS WARM TO THE TOUCH AND HAD THE ODOR. AFTER CHECKING IT FOR ANY OBVIOUS DAMSDR CA130723006Fitting · sheared(CAN) DURING HEAVY MAINTENANCE, WASHER WAS FOUND CRACKED ON LT OTBD FLAP FITTING. IT WAS NOTED DURING WASHER REPLACEMENT IAW 27-51-23 THAT THE REMOVAL OF THE NUT WAS ABNORMALLY HIGH. DURING A WALK AROUND AFTER THE AIRPLANE HAD BEEN REPAINTED THE LT FITTING SDR CA130709014Gearbox · making metal(CAN) CREW REPORTED THE NR 1 ENGINE OIL FILTER BYPASS INDICATION ILLUMINATED JUST PRIOR TO DECENT. INDICATION WOULD NOT EXTINGUISH WITH THRUST REDUCED RESULTING IN ENGINE BEING SHUTDOWN IAW FOM. EMERGENCY LANDING WAS REQUESTED AND THE ACFT LANDED UNEVENTFULLSDR CA130710002Heater · failed(CAN) ON CLIMB THROUGH FL360 OVER SPEED WARNING SOUNDED AND IAS DISAGREE ILLUMINATED ON BOTH PFD`S, AFTER 10-15 SECONDS ALL INDICATIONS RETURNED TO NORMAL. REACHING FL390, IAS DISAGREES ILLUMINATED AGAIN. CREW HAD THE CLACKER AND THEY HAVE NOTED THE F/O`S PFD SDR CA130610009Anti-Skid Valve · failed(CAN) DURING SHORT FINAL, THE FLIGHT CREW REPORTED AN ANTI-SKID INOPERATIVE LIGHT ILLUMINATE FORCING A MISSED APPROACH. DUE TO POTENTIAL MEL RESTRICTIONS LIMITING THE ACFT OPERATIONALLY, IT WAS DECIDED A DIVERSION TO A STATION WITH MORE FAVORABLE WEATHER CONDSDR CA130605008Wire · chafed(CAN) ON APPROACH, ELECTRIC HYDRAULIC NR 2, OVERHEAT, ANNUNCIATOR ILLUMINATED. CREW ELECTED TO CARRY OUT A MISSED APPROACH TO APPRAISE THE SITUATION. INSTRUCTIONS WITHIN THE NON-NORMAL CHECKLIST FOLLOWED AND NR 2 HYDRAULIC PUMP SELECTED OFF, ANNUNCIATOR EXTINGSDR CA130604001Transceiver · failed(CAN) FLT EXPERIENCED AN HF SYS FAILURE IN FLIGHT. DUE TO ROUTING INTO NON-WATER THE ACFT HAD TO DIVERT FOR MORE FUEL. FLIGHT CREW APPLIED MEL TO HF SYS. SYSTEM WAS REPAIRED THAT NIGHT, HF TRANSCEIVER, PN 964-0452-011, SN 03975,TSI 378.5, CSI 173 WAS REPLACSDR CA130531012Engine · warning message(CAN) WHILE THE ACFT WAS ENROUTE, THE FLIGHT CREW ELECTED TO SHUTDOWN THE NR 1 ENGINE FOR ILLUMINATION OF THE OIL FILTER BYPASS LIGHT. FOLLOWING THE FOM AND REDUCING THRUST DID NOT EXTINGUISH THE LIGHT. THE FLIGHT RETURNED TO POS AND MADE AN UNEVENTFUL LANDISDR CA130527007Wire Harness · damaged(CAN) DURING CRUISE, THE FLIGHT CREW REPORTED THE RT SIDE WING-BODY OVERHEAT ANNUNCIATOR ILLUMINATE AND THEN EXTINGUISH AFTER 20 SECONDS. DUE TO FORECAST ICING CONDITIONS WHICH WOULD LIMIT THE ACFT OPERATIONALLY UNDER MEL 26-13-1, WING-BODY OVERHEAT DETECTOR SDR CA130517001Lever · dirty(CAN) ON APPROACH, THE FLIGHT CREW OBSERVED A LANDING GEAR INDICATION DISAGREE REQUIRING A GO-AROUND. DURING THE SECOND APPROACH, NORMAL LANDING GEAR POSITION INDICATION WAS REPORTED RESULTING IN A SUCCESSFUL LANDING. MAINTENANCE CARRIED OUT THE FOLLOWING ACSDR CA130507006Coffeemaker · overheated(CAN) FLIGHT CREW REPORTED THAT JUST PRIOR TO REACHING THE GATE THAT THE F/A THOUGHT SHE COULD SMELL SMOKE COMING FROM THE REAR-LEFT COFFEEMAKER. SHE TURNED OFF THE COFFEEMAKER AND THE ODOR WENT AWAY. THE SUSPECT COFFEEMAKER WAS REPLACED IAW CMM 25-31-101 ANSDR CA130419005Control Valve · failed(CAN) ON CLIMB THROUGH 19,000 FT THE RT BLEED TRIP LIGHT ILLUMINATED. THE BLEED TRIP RESET PROCEDURE WAS UNSUCCESSFUL AND THE CREW PERFORMED AN AIR TURN BACK WHERE PARTS AND MANPOWER WERE AVAILABLE. MAINTENANCE PERFORMED A BLEED AIR HEALTH CHECK AND REPLACED SDR CA130416017Door · malfunctioned(CAN) DURING ROUTINE MAINTENANCE TO REPLACE BOTH OVERWING EXIT WINDOW SHADES, THE LT AND RT OVERWING EMERGENCY EXIT DOORS DID NOT EXTEND WHEN RELEASE HANDLE WAS PULLED AND WERE ALSO DIFFICULT TO CLOSE. LT AND RT OVERWING EMERGENCY EXITS WERE INSPECTED AND ADJ
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