Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAASB99071Light · failedCLT - MAINTENANCE FOUND THE FLOOR EMERGENCY LIGHTS AT SEAT ROW 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 10. OPS CHECK GOOD. (M)SDR USAASB99064Shutoff Valve · malfunctionedCLT - FLT 8054 - SHORTLY AFTER TAKEOFF, THE CREW NOTICED A BANGING NOISE COMING FROM THE LEFT PACK. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK 35 DEGREE SHUTOFF VALVE AND THE TEMPERATURSDR 99ZZZM229Control Box · malfunctionedCLT - FLT 8054 - SHORTLY AFTER TAKEOFF, THE CREW NOTICED A BANGING NOISE COMING FROM THE LEFT PACK. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK 35 DEGREE SHUTOFF VALVE AND THE TEMPERATURSDR USAA990180Web · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 233, BL 0, WL 192.5 WEB. INSTALLED DOUBLER PER BOEING SRM 51-70-13. (M)SDR USAASB99058Coupling · leakingBOS - FLT 2673 - SHORTLY AFTER TAKEOFF, TOWER NOTIFIED CAPTAIN THAT FUEL WAS VENTING/LEAKING OUT OF THE RIGHT WING. TOWER NOTED THAT SEVERAL AIRCRAFT HAD REPORTED THE SAME. AT THE SAME TIME, THE CALL BELL IN THE AIRCRAFT WAS GOING OFF, AS PASSENGERS ALSO REPSDR USAASB99053Snubber · misinstalledTPA - FLT1795 - CAPTAIN REPORTED THAT DURING CLIMB-OUT FROM PBI, AN UNCOMFORTABLY LOUD NOISE WAS COMING FROM THE FORWARD ENTRY DOOR AREA. PRESSURIZATION AS NORMAL BUT A DECISION WAS MADE TO DIVERT TO TPA DUE TO EXCESSIVE NOISE. FLIGHT LANDED WITHOUT FURTHER SDR USAA990179Skin · crackedCLT - HFEC FOUND A .3 INCH CRACK OUTER SKIN AT AFT UPPER CARGO DOOR HANDLE CUTOUT. INSTALLED REP DOUBLER PER EA NR 63895. CARGO DOOR RETURNED TO STOCK. (M)SDR USAASB99051Windshield · failedBOS - FLT 1665 - ON CLIMB-OUT FROM PWM, AT FL190, THE FIRST OFFICERS WINDSHIELD SHATTERED. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. PRIOR TO THE WINDSHIELD SHATTERING, THE CSDR USAASB99042Battery Pack · dischargedROC - MAINTENANCE FOUND THE CENTER RIGHT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB99040Duct · brokenPVD - FLT 710 - FLIGHT WAS DISPATCHED WITH THE RIGHT PACK ON MEL DUE TO A RIGHT WING BODY OVERHEAT LIGHT ILLUMINATING. EN ROUTE FROM PIT TO PVD AT FL250, THE WARNING HORN SOUNDED DUE TO A PRESSURIZATION LOSS. CREW WAS UNABLE TO CONTROL PRESSURIZATION IN MANUASDR USAASB99039Controller · failedPHL - FL255 - ON CLIMB-OUT FROM ATL, FLIGHT LOST BOTH AUTO AND STANDBY PRESSURIZATION CONTROL AT FL310. CREW DECLARED AN EMERGENCY AND DESCENDED TO FL100. OXYGEN MASKS WERE NOT DEPLOYED. AFTER DESCENDING TO FL090, THE CAPTAIN FELT IT WAS SAFE TO CONTINUE TOSDR USAASB99055Battery Pack · dischargedIAH - MAINTENANCE FOUND THE RIGHT FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB99038Controller · failedPIT - FL777 - EN ROUTE FROM PIT-DFW, IN THE CMH AREA, CREW RECEIVED A WARNIGN OF PRESSURIZATION LOSS DURING CLIMB FROM FL330 TO FL350. FLIGHT DESCENDED TO FL250 AND WAS UNABLE TO MAINTAIN PRESSURIZATION. DESCENT WAS MADE TO FL110 AND DECISION WAS MADE TO RETSDR USAA990087Skin · crackedCLT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN EXTERNAL SKIN AT STA 380 AND BL 3 LEFT E/E COOLING DUCT EXHAUST CUT-OUT. INSTALLED DOUBLER PER SRM 53-30-07. (X)SDR USAASB99035Battery Pack · dischargedLGA - MAINTENANCE FOUND THE LEFT MID AISLE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR 99ZZZM168Charger · inoperativeLGA - MAINTENANCE FOUND THE LEFT MID AISLE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR DL733990251Iru · inopNR 1 COMPASS FAILED. CYCLED CB, NO CHANGE. REPLACED NR 1 IRU.SDR USAA99068Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND THREE 2 INCH LONG CRACKS BETWEEN BS 663 AND BS 727 AT LBBL 6 AND RBBL 6 LOWER KEEL BEAM SKIN. INSTALLED INTERIM REPAIR DOUBLERS PER SRM 53-60-12. (M)SDR USAASB99017Retract Mech · malfunctionedPIT - ON FINAL APPROACH AT 220 KNOTS, CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT COME DOWN WHEN THE GEAR HANDLE WAS LOWERED. CREW RECYCLED THE GEAR AND ALL GEAR CAME DOWN NORMALLY. DURING FIRST ATTEMPT, CREW DID NOT HEAR ANY NOISE FROM THE NOSE LANDINGSDR USAASB99012Acm · failedMCO - FLT 808 - CLIMBING THROUGH FL270, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 11,000 FEET AND CLIMBED AS HIGH AS 13,000 FEET. EMERGENCY DESCENT WS MADE TO 10,000 FEET. FLIGHT RETURNED TO FIELD TO MCO AND LANDED WITHOUT FURTHER INCIDSDR 99ZZZM157Control Box · failedMCO - FLT 808 - CLIMBING THROUGH FL270, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 11,000 FEET AND CLIMBED AS HIGH AS 13,000 FEET. EMERGENCY DESCENT WS MADE TO 10,000 FEET. FLIGHT RETURNED TO FIELD TO MCO AND LANDED WITHOUT FURTHER INCIDSDR USAASB99006Battery Pack · dischargedIAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR DL733982622Anti Ice Valve · failedRIGHT ENGINE ANTI-ICE FAILED CLOSED POSITION. AIR TURN BACK. REPLACED ANTI-ICE VALVE.SDR USAASB98337Charger · failedCLT - THE LEFT AFT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND CHARGER. (M)SDR 99ZZZM32Light · failedCLT - THE LEFT AFT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND CHARGER. (M)SDR USAASB98334Battery Charger · inoperativeCLT - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M)SDR USAA980647Floorbeam · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION UNDER SIDE FLOORBEAM STATION 986 LBL 3. CORROSION TASK NR C 53-107-02. INSTALLED 'T' CAP PER SRM 53-00-51 FIG 202. (M)SDR USAA980641Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH HOLE IN FRAME/APU BLEED DUCT STATION 1040. INSTALLED REPAIR DOUBLER PER EA 63138 AND TR 53-80-02. (M)SDR USAA980640Floorbeam · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 88 INCH BY 1 INCH BS 1016 RBL 6 FLOORBEAM, CORROSION TASK NR C53-107-02. T-CAP FLOORBEAM REPLACED PER TR 53-10-05. (M)SDR USAA980639Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK BS 727 STRINGER 14L FRAME WEB. INSTALLED FILLER AND DOUBLER PER EA 63060. (M)SDR USAA980638Angle · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE STATION 222 RT 27 INCH ABOVE FLOORLINE ANGLE. CORROSION TASK NR C53-101-01. REMOVED SURFACE CORROSION PER SRM 51-10-6. (M)SDR USAA980624Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK MLG WHEEL WELL LBL 30 WEB PANEL. INSTALLED WEB AND STIFFENER PER EA 63025 AND SRM 53-60-51. (M)SDR USAA980623Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 867, 1 INCH ABOVE S 9R FRAME. INSTALLED DOUBLER AND FILLER PLUG PER SRM 53-00-07 FIG 202. (M)SDR USAA980622Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 440, 1 INCH ABOVE S 9R FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA980621Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 480, 1 INCH ABOVE S 9L FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M)SDR USAA980620Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 380, 1 INCH ABOVE S 9R FRAME WEB. FABRICATED A FILLER AND DOUBLER PER SRM 53-00-07. (M)SDR USAA980619Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA980618Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 907, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA980617Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK NOSE WHEEL WELL, NOSE GEAR ACTUATOR SUPPORT STRUCTURE ANGLE. REPLACED GUSSET AND ACTUATOR MOUNT PER BOEING DRAWING 65-45819. (M)SDR USAA980616Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 887, S 9R FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA980608Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH CORROSION AREA AND A .25 INCH CRACK STATION 295 TO STATION 360 RBL 60 INNER CHORD ANGLE. CORROSION TASK NR C53-107-02. INSTALLED PART PER SRM 51-10-02. (M)SDR USAA980607Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. INSTALLED PART PER SRM 51-10-2. (M)SDR 99ZZZM34Light · inoperativeCLT - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M)SDR USAA980646Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7R FUSELAGE ANGLE EXTERIOR. INSTALLED DOUBLER PER TR 53-50-03. (M)SDR USAA980645Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7L FUSELAGE ANGLE EXTERIOR. INSTALLED DOUBLER PER TR 53-50-03. (M)SDR USAA980642Web · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STATION 294 WL 209 RBL 56 WEB. INSTALLED DOUBLER PER BOEING 737-300 SRM 51-70-11. (M)SDR USAA980637Fuel Tank · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH CRACKS AUX FUEL TANK SHROUD AFT WALL LOWER CORNER SKIN. INSTALLED DOUBLER PER EA 63089. (M)SDR USAA980636Sill · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 70 INCH ALONG FORWARD SERVICE DOOR 'Z' ANGLE LOWER SILL INBOARD CHORD ANGLE AT BS 280-350 RBL 35. CORROSION TASK NR C53-107-01. REPLACED PART PER BOEING 737-300 SRM 51-40-02 AND 51-20-05. SDR USAA980635Web · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION SURROUNDING NUTPLATE HOLES 1 INCH BY 57 INCH FROM BS 790 TO 847 RBL 20 WEB. CORROSION TASK NR 53-202-01. INSTALLED NEW WEB AND FILLER PER SRM 51-30-01. (M)SDR USAA980633Floorbeam · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK STATION 520, LBL 24.75, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M)
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