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 USAASB98199Harness · failedIAH - FLT 1934 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT AND THE MASTER CAUTION LIGHT ILLUMINATED. CREW WENT THROUGH EMERGENCY PROCEDURES, DISCHARGED BOTH ENGINE FIRE BOTTLES AND SHUT DOWN THE NR 2 ENGINE. FLIGHT RETURNED TO FIELD AT IAH AND LASDR USAASB98198Light · inoperativePIT - DURING TRANSIT CHECK, MAINTENANCE FOUND TWO ADJACENT FLOOR TRACK EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED BROKEN WIRES AT WIRE SPLICES FOR BOTH LOCATIONS. OPERATIONAL CHECK GOOD. (M)SDR USAA980320Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 4 INCH CORROSION TOP OF FLANGE STA 312 CENTERLINE FLOORBEAM. CORROSION TASK NR C 53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 53-10-03. (X)SDR USAA980319Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION TOP OF FLANGE FLOORBEAM AT STA 312 RBL 30. CORROSION TASK NR C53-107-01. INSTALLED SPLICE PER SRM 53-10-03. (X)SDR USAA980318Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.50 INCH CRACK 727D BETWEEN STRINGERS 27 LT AND RT OF FRAME. INSTALLED DOUBLER, NEW SHEAR TIES AND FLOOR ANGLE SUPPORTS PER SRM 53-00-07 FIG 203. (X)SDR USAASB98191Battery Pack · dischargedSYR - FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK. (M)SDR USAASB98190Connector · failedSYR - FOUND AFT SECTIN OF FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A CANNON PLUG ON THE AFT SECTION OF THE TRACK LIGHTING. (M)SDR USAASB98188Door · openCLT - FLT 1475 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NOISE WAS HEART FROM AFT SERVICE DOOR ALTHOUGH NO DOOR WARNING INDICATIONS WERE PRESENT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUNDSDR USAASB98187Battery Pack · dischargedALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY/EVACUATION LIGHTS INOPERATIVE. BULLNOSE EVACUATION LIGHT AT SEAT ROW 1, ESCAPE SLIDE LIGHT FOR FORWARD PASSENGER DOOR, EXIT SIGN OVER FORWARD SERVICE DOOR AND COCKPIT EVACUATION LIGHT. MAINTENANCE REMOVED AND RSDR USAASB98186Check Valve · leakingPIT - FLT 1665 - AFTER TAKEOFF FROM PIT, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL AC. OUTFLOW VALVE INDICATED CLOSED. CREW WENT THROUGH PROCEDURES AND ADVISED TOWER THAT THEY WERE RETURNING TO FIELD TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NSDR USAA980263Skin · crackedCLT - DURING CX-5 CHECK VISUAL AND EDDY CURRENT, FOUND A 1.625 INCH CRACK IN SKIN STATION 380 BL 3L EQUIP COOLING DUCT OUTLET CUTOUT. INSTALLED DOUBLER PER T/R 53-30-04 AND EA 62079A. (M)SDR USAA980313Skin · crackedDURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION FOUND A .25 INCH CRACK IN AFT CARGO DOOR SKIN AT THE AFT UPPER CORNER FOR HANDLE. INSTALLED DOUBLER PR SRM 52-00-01 FIG 202. (M)SDR USAASB98171Heat Exchanger · failedDEN - FLT 8052 - UPON CLIMB-OUT, JUST BEFORE LEVEL OFF AT FL 290, CREW WAS ALERTED TO HIGH OIL TEMPERATURE ALONG WITH A BURNING SEMLL ON THE NR 1 ENGINE. CREW ACCOMPLISHED CHECKLIST, DECLARED AN EMERGENCY AND INITIATED PROCEDURES IN SHUTTING DOWN THE NR 1 ENGSDR USAASB98169Lock Actuator · failedROC - FL 1795 - SHORTLY AFTER RAISING THE LANDING GEAR AFTER TAKEOFF FROM DCA, THE NOSE LANDING GEAR GREEN LIGHT REMAINED ON ALONG WITH THE RED UNSAFE LIGHT. COCKPIT NOISE INDICATED THE GEAR DOORS WERE STILL OPEN. RECYCLED GEAR AND RECEIVED ALL THREE GEAR GRSDR USAASB98165Battery Pack · dischargedPIT - MAINTENANCE FOUND THE MID CABIN CENTER AISLE EMERGENCY EXIT SIGN AND THE LEFT OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)SDR 98ZZZM555Battery Charger · inoperativePIT - MAINTENANCE FOUND THE MID CABIN CENTER AISLE EMERGENCY EXIT SIGN AND THE LEFT OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)SDR USAASB98157Light · inoperativeSYR - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT JUST AFT OF THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB98151Battery Charger · dischargedLGA - MAINTENANCE FOUND THE AFT SECTION OF FLOOR EMERGENCY LIGHTS INOP. MAINTENACE REMOVED AND REPLACED THE BATTERY CHARGER AND BATERY PACK AND REPAIRED BURNED WIRES IN THE OVERHEAD ABOVE THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M)SDR USAA980260Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 378 AND LBL 6 (LOWER LOBE) SKIN. INSTALLED DOUBLER AND REPAIRED PER DRAWING 65C33930 AND SRM 53-00-01. (M)SDR 98ZZZM556Battery Pack · inoperativeLGA - MAINTENANCE FOUND THE AFT SECTION OF FLOOR EMERGENCY LIGHTS INOP. MAINTENACE REMOVED AND REPLACED THE BATTERY CHARGER AND BATERY PACK AND REPAIRED BURNED WIRES IN THE OVERHEAD ABOVE THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M)SDR USAASB98149Battery Pack · dischargedPIT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98141Switch · out of adjustPHL - FLT 701 - AFTER TAKEOFF OUT OF BTV, THE LANDING GEAR WOULD NOT RETRACT. CREW TRIED TO RECYCLE GEAR BUT IT WOULD NOT RETRACT. USED LANDING GEAR OVERRIDE TRIGGER AND GEAR RETRACTED. FLIGHT PROCEEDED ON NORMAL FLGHT AND LANDED WITHOUT FURTHER INCIDENT. SDR USAASB98133Light · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5, 6, 7, 9, AND 11. MAINTENANCE REPAIRED EMERGENCY LIGHT WIRING AT SEAT ROWS 7 AND 8, LEFT HAND SIDE. OPERATIONAL CHECK GOOD. (X)SDR USAASB98121Battery · dischargedIND - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY EXIT SIGNS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY IN CHARGER UNIT. OPS CHECK GOOD. (M)SDR USAASB98123Light · inoperativeTPA - DURING B-CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT THE AFT SERVICE DOOR INOP. MAINTENANCE FOUND THE LIGHT SOCKET WAS BROKEN DUE TO EXCESSIVE CORROSION. REPLACED ENTIRE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB98114Dadc · failedCLT - FLT 1435 - ON TAKEOFF ROLL AT 100 KNOTS, THE FIRST OFFICER'S AIRSPEED, ALTIMETER AND VERTICAL SPEED HAD FAILED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 2 DIGITAL AIR DATASDR USAA980197Floorbeam · corrosionCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 1.5 INCH ON FLOORBEAM FWD FLANGE LBL 45 BS 967 PAX FLOOR. CORROSION NR C53-107-02. INSTALLED FILLER AND DOUBLER ANGLES ON FWD FLANGE PER SRM 53-50-51 FIG 202 AND EA 61664. (M)SDR USAA980196Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO 2 INCH CRACKS BETWEEN BS 380 AND BS 400 AT BL 0 SHEAR WEB INSTALLATION. FABRICATED NEW ANGLE AND INSTALLED ANGLE ON SHEAR WEB PER REPAIR DOCUMENT SRM 51-40-02. (M)SDR USAA980195Floorbeam · corrosionCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK ON FLOORBEAM 344.17 UPPER 'T' CAP LBL 7 TO LBL 35. CORROSION NR C53-170-02. REPAIRED 'T' CAP TO FLOORBEAM PER TYPICAL REPAIR 53-10-03. (M)SDR USAA980194Floorbeam · corrosionCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 7.5 INCH CORROSION AREA ON FLOORBEAM 328 UPPER AND LOWER SURFACE OF UPPER T-CAP RBL 14.5 TO RBL 56.5. CORROSION NR C53-107-02. REPLACED T-CAP AND INSTALLED SPLICE ANGLES PER TYPICAL REPAIR 53-10-03. (M)SDR USAA980178Floorbeam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 18 INCH AREA OF SURFACE CORROSION STA 947, LBL 12 TO RBL 12 FLOORBEAM. CUT OUT CORRODED SECTION OF UPPER T-CAP ON FLOORBEAM AND SPLICED NEW SECTION. REPAIRED PER SRM 53-00-51. CORROSISDR USAA980177Skin · damagedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 4 INCH BY 6 INCH TEMPORARY REPAIR DOUBLER INSTALLED PER EA 59798 BS 188, WL 190 ON LEFT SIDE FUSELAGE SKIN. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (X)SDR USAASB98105Mechanism · out of adjustBWI - FLT 2150 - UPON CLIMB-OUT FROM BWI, AIRCRAFT HAD A PRESSURIZATION PROBLEM AND A BANGING NOISE COULD BE HEARD FROM THE REAR OF THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUSDR USAASB98108Battery Pack · dischargedIAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ON THE FORWARD ENTRY DOOR INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATION CHECK GOOD. (X)SDR USAA980174Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 2.675 INCH CRACK IN THE SKIN AT RIGHT BS 727D AT S23R. INSTALLED DOUBLER PER REPAIR DOCUMENT EA 61668. (X)SDR USAA980170Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK IN STATION 500 FRAME RBL 1.75 INCH BELOW TOP OF FRAME. INSTALLED DOUBLER, REPAIRED PER EA 43886. (M)SDR USAA980169Floorbeam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION TOP OF FLOORBEAM BS 947, BL 8L. REMOVED DAMAGED SECTION, INSTALLED NEW T-CAP LBL 37 RBL 32 BS 947. REPAIRED PER 737-300 SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02, CORROSION SDR USAASB98098Seal · failedPHL - FLT 1934 - AFTER TAKEOFF AND DURING CLIMB-OUT FROM PHL, THE FLIGHT ATTENDANTS REPORTED TO THE CAPTAIN OF HEARING A LOUD NOISE AROUND THE MAIN ENTRY DOOR. CREW STOPPED CLIMB AT 10,000 FT AND ELECTED TO RETURN TO FIELD AT PHL DUE TO LOUDNESS OF NOISE. FLSDR USAASB98096Battery Pack · dischargedROC - DURING TRANSIT CHECK WHILE ACCOMPLISHING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND THE FORWARD ENTRYWAY EMERGENCY EXIT LIGHTS DIM AND AFTER 30 SECONDS OF OPERATION, LIGHTS WENT OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PASDR USAA980171Floorbeam · corrosionCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .50 INCH CORROSION AREA AT FLOORBOARD HOLES TOP OF FLOOR BEAM T-CAP STA 344 LBL ZERO TO LBL 48. CORROSION TASK CARD NR C53-107-01. INSTALLED NEW T-CAP REPAIR ANGLE AND SPLICES PER REPAIR DOCUMENT TRM 53-10-03SDR USAASB98094Pmc · failedCLT - FLT835 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE N1 AND ALL ENGINE PARAMETERS BEGAN FLUCTUATING. CREW COULD HEAR THAT THE ENGINE WAS SURGING. FLIGHT RETURNED TO FIELD AT CLT. ON APPROACH, ENGINE STABILIZED. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH SDR USAASB98092Seal · leakingIND - FL 1588 - DURING CRUISE, CREW NOTICED THE NR 1 ENGINE OIL QUANTITY HAD DECREASED FROM 4 GALLONS TO 1-3/4 GALLONS DURING FLIGHT. THE ONLY INDICATION THE CREW HAD WAS LOW OIL QUANTITY. FLIGHT DIVERTED TO IND DUE TO OIL LOSS AND LANDED WITHOUT FURTHER INCSDR USAASB98090Seal · leakingMEM - FL 175 - AT 28,000 FEET, 138 MILES WEST OF MEM, THE NR 1 ENGINE HAD A LOSS OF OIL AS INDICATED ON THE OIL QUANTITY INDICATOR. FLIGHT DIVERTED INTO MEM AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. THE NR 1 ENGINE WAS NOT SHUT DOWN IN-FLISDR USAA980B1Frame · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG BY 1 INCH WIDE CORROSION BS 847 OVER STRINGER 26R TO STRINGER 25R FRAME. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-00-51 FIG 203. CORROSION LEVEL 2, CORROSION TASK NR C53-208-01. (M)SDR USAA980130Keel Beam · corrosionINT - DUIRNG Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENER HOLES .5 INCH BY .5 INCH BS 707-727 RT KEEL BEAM. INSTALLED REPAIR ANGLE, REPAIRED PER EA 43726A. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M)SDR USAA980129Keel Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENERS HOLES .5 INCH BY .1875 INCH BS 707-727 LT KEEL BEAM. INSTALLED REPAIR STRAPS, REPAIRED PER EA 43725A. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M)SDR USAASB98074Separator Bag · cloggedPHL - FLT 1486 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. DUCT PRESSURE WAS GOOD AT 40 PSI AND OUTFLOW VALVE WAS FULL CLOSED. THE LEFT PACK WAS ON MEL. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLASDR USAASB98072Fan · failedCLT - FLT 703 - AFTER TAKEOFF, PASSING THROUGH 1,700 FEET, CREW BEGAN TO SMELL A BURNING ELECTRICAL ODOR. SMEL APPEARED TO BE STRONGER IN REAR OF AIRCRAFT THAN THE COCKPIT AND FRONT GALLEY. FLIGHT RETURNED TO FIELD AT CLT. ON APPROACH TO CLT, CREW SHUT DOWNSDR USAA980128Floorbeam · corrosionCLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES STATION 1016 BEAM IN LEFT LAV AREA. INSTALLED REPAIR STRAP REPAIR DOCUMENT SRM 53-00-51 FIG 203. (M)SDR USAA980127Floorbeam · corrosionCLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES THE ENTIRE LENGTH STATION 986 FLOORBEAM. REPLACED T-CAP PER TYPICAL REPAIR NR 53-10-05. (M)
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