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 CA120130013Warning Message · false activation(CAN) DURING TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS THE MASTER CAUTION AND ENGINE ANNUNCIATOR LIGHTS, ON THE GLARESHIELD ILLUMINATED. FLIGHT CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE UNEVENTFULLY. MAINTENANCE CARRIED OUT AN ELECTRONIC ENGINE SDR CA120130012Feeder Cable · failed(CAN) ON A FLIGHT, BEFORE ENTERING THE ETOPS ZONE, THE WINDOW OVERHEAT CAUTION LIGHT ILLUMINATED FOR THE LT SIDE SLIDING WINDOW, L2. THE CREW CONSULTED THE NON NORMAL CHECKLIST AND PERFORMED A RESET. THE OVERHEAT LIGHT ILLUMINATED A SECOND TIME AND THE CREW SDR CA120116006Electrical Box · smoke(CAN) FLIGHT DIVERTED DUE TO ELECTRICAL SMOKE DETECTED IN CABIN. SOURCE SEEMED TO BE AT OR NEAR THE LIVE TV IFE BOX AT 6B. FIM TASK 21-00, TASK 806 CARRIED OUT. SOURCE OF ELECTRICAL FUMES FOUND TO BE INTERNAL COMPONENTS OF SEB AT 6B. SEB WAS REPLACED PN 304SDR CA120106003Thrust Reverser · malfunctioned(CAN) AFTER TAKEOFF THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY THE OVERHEAD NR 2 ENGINE REVERSER LIGHT AND THE NR 2 ENGINE CONTROL LIGHT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT FOR MAINTENANCE AND LANDED UNEVENTFULLY. FOLLOWING THE PROCEDURE IAW MELSDR CA111228008Relay · failed(CAN) DURING TAKEOFF AFTER GEAR RETRACTION THE FLIGHT CREW OBSERVED SEVERAL WARNING LIGHTS ILLUMINATE, THEY ARE LISTED AS FOLLOWS. SPEED BRAKE ARMED, SPEED BRAKE DO NOT ARM, STABILIZER OUT OF TRIM, AUTO BRAKE DISARM, ANTI-SKID INOPERATIVE, L/E FLAPS TRANSIT, SDR CA111213010Sensor · faulty(CAN) DURING APPROACH, THE FLIGHT CREW REPORTED THEY HAD A FLAP ASYMMETRY PROBLEM WHEN FLAPS WERE SELECTED DOWN. THE LOG BOOK ENTRY IS AS FOLLOWS, ON APPROACH WHEN FLAPS WERE SELECTED, LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED & TE FLAPS STUCK BETWEEN UP & SDR CA111205014Unknown · odor(CAN) AFTER TAKEOFF, FLIGHT REPORTED THE ODOR OF SMOKE IN THE CABIN. THE CREW ELECTED TO DECLARE AN EMERGENCY AND RETURN TO DEPARTURE AIRPORT. SMOOTH UNEVENTFUL LANDING WAS CARRIED OUT. MAINTENANCE CARRIED OUT FIM 71-05, TASK 807 FOR FUMES IN THE CABIN. DSDR CA111202003Sensor · failed(CAN) WHILE ON APPROACH THE FLIGHT CREW REPORTED THEY HAD A FLAP ASYMMETRY PROBLEM CAUSING THE FLAPS TO LOCK. THE LOG BOOK ENTRY IS AS FOLLOWS. FLAPS JAMMED PRIOR TO REACHING "FLAP". RIGHT INDICATOR SHOWS ALMOST UP. LT INDICATOR SHOWS ALMOST 1. THE FLIGHSDR CA111122003Switch · frozen(CAN) CREW ABORTED TAKEOFF AT 20KTS DUE TO A RT OVERWING EXIT DOOR WARNING LIGHT ILLUMINATED. INVESTIGATION FOUND THE OVERWING EXIT AFT SWITCH ICED UP THEREFORE WAS NOT WORKING CORRECTLY. SWITCH WAS FREED UP WITH ALCOHOL AND FIM 52-20 WAS CARRIED OUT WITH NOSDR CA111116009Controller · failed(CAN) DURING TAKEOFF ROLL THROUGH 40KTS, MASTER CAUTION AIR CONDITIONING AND AUTO FAIL LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. NR 2 CABIN PRESSURE CONTROLLER WAS REPLACED. REMOVED UNIT WAS HIGH TIME WITH 27,000 HOURS SINCE NEW.SDR CA111114010Controller · unserviceable(CAN) REF SDR 20111107007, OCCURRENCE DATE NOV 5 2011. REJECTED TAKEOFF DUE TO LT NR 2 WINDOW OVERHEAT. INVESTIGATION FOUND WINDOW HEAT CONTROLLER COOLING HOLES WERE FOUND PLUGGED WITH DUST. CONTROLLER WAS CLEANED, TESTED & SWAPPED FROM POSITION NR 1 TO POSSDR CA110419002Warning Light · illuminated(CAN) SPEED "DO NOT ARM" LIGHT ILLUMINATED ON BEGINNING OF TAKEOFF ROLL. TAKEOFF ABANDONED, ACFT RETURNED TO GATE. ACFT IS CURRENTLY OPERATING UNDER MEL 27-7-1. FURTHER DETAILS OF THIS INCIDENT WILL BE PROVIDED AS THEY BECOME AVAILABLE.SDR CA110426005Fuse · fractured(CAN) MAINTENANCE DISCOVERED A HYD FLUID LEAK IN THE RT WHEEL WELL. THE RT NORMAL BRAKE HYDRAULIC FUSE WAS FOUND TO BE LEAKING FLUID. THE FUSE WAS SUBSEQUENTLY REPLACED IAW THE AMM 32-41-72. THE REPAIR VENDOR REPORTED THE FOLLOWING FINDINGS AND A TEAR DOWN SDR CA110407004Collar · worn(CAN) WHILE TAXIING STEERING INTERMITTENTLY FROZE WITH BOTH RUDDER PEDALS & TILLER COULD BE OVERPOWERED & THEN SEEMED TO BREAK FREE WITH ENOUGH FORCE. FOUND THE NLG STEERING COLLAR EXCESSIVELY WORN & ROCKING DURING ALTERNATING TURNING ACTION. COLLAR REPLACEDSDR CA110228014Inlet · vibration(CAN) CREW REPORTED NR 2 ENGINE WAS AT 4.0 UNITS OF FAN VIBRATIONS DURING CLIMB AND AT CRUISE, FLT LEVEL 33, IT WAS 3.4. ACFT TURNED BACK TO BASE. MAINTENANCE CARRIED OUT A FAN BLADE LUBE IAW AMM 72-21-00 AND FOUND 12 PLATFORMS WITH SEALS DAMAGED ALL WITHIN
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