Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA980338Skin · crackedTPA - DURING CX-5 CHECK EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN OUTER SKIN OF AFT ENTRY DOOR, LOWER AFT CORNER OF UPPER HINGE CUTOUT. ROUTED DAMAGE AND INSTALLED DOUBLER OF .071,2024-T3 PER SRM 52-10-01, 51-30-8 AND EA 62192. (M)SDR USAA980337Angle · crackedTPA - DURING CX-5 VISUAL INSPECTION, FOUND A 1 INCH CRACK IN ANGLE AT STATION 727 COMPRESSION CHORD RBL 25. INSTALLED DOUBLER PER TYPICAL REPAIR NR 53-10-03A PART 3. (M)SDR USAASB98200Light · inoperativePHL - WHILE TESTING EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 9A WITHOUT A LENSE AND SMOKING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 9A. OPERATIONAL CHECK GOOD. (M)SDR USAASB98194Coffee Maker · failedBWI - FLT 7095 - EN ROUTE FROM MIA-BWI, A STRONG ACRID ODOR EMINATED FROM THE AFT RIGHT GALLEY. ODOR WAS ISOLATED TO THE VENT IN THE AFT RIGHT GALLEY WHICH IS NOT PART OF THE AIR CONDITIONING SYSTEM. TURNED OFF GALLEY POWER AND PULLED GALLEY COFFEE CIRCUIT BSDR USAASB98192Fan · failedMIA - FLT 2649 - CAPTAIN REPORTED A SULFUR SMELL IN CABIN DURING FINAL APPROACH INTO MIA. MAINTENANCE FOUND THE GASPER FAN CIRCUIT BREAKER POPPED, AND REPLACED THE FAN. (M)SDR USAASB98189Fan · failedJAX - FLT 2606 - EN ROUTE FLL/BWI, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. CREW SECURED THE GASPER FAN AND RIGHT PACK. THE SMOKE APPEARED TO ABATE. FLIGHT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GASPER FAN CIRCUIT BSDR USAA980317Stringer · corrodedTPA - DURING A CX-6 CHECK VISUAL INSPECTION, FOUND 12 INCHES OF HEAVY CORROSION STRINGER 25L STATION 967 AND STATION 986 TO STATION 998. REPLACED SECTION OF STRINGER WITH JT NEW PART AND SPLICED PER SRM 53-10-3. (M)SDR USAA980316Stringer · corrodedCLT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND HEAVY CORROSION STRINGER 27L STATION 986 TO STATION 1006. REPLACED WITH NEW SECTION OF STRINGER PER EA 62127 AND SRM 53-10-3. (M)SDR USAA980315Skin · crackedCLT - DURING CX-6 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN FORWARD ENTRY DOOR FRAME LOWER AFT CORNER. INSTALLED DOUBLER OF .063 CRES 301 1/2 HARD AND A TRIPLER OF .063 CRES 301 1/2 HARD PER EA 62121B. (M)SDR USAA980312Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 9R TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M)SDR USAA980311Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727, STRINGER 4L TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M)SDR USAA980310Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 2R TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M)SDR USAA980309Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 787 STRINGER 10R TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M)SDR USAA980308Floorbeam · corrodedCLT - DURING Q-6 VISUAL INSPECTION, FOUND A 1 INCH BY 10 INCH AREA OF CORROSION AT STATION 294 LBBL 12 FLOORBEAM 'T' CAP CHORD. CORROSION TASK CARD NR C53-202-02. FABRICATED NEW 'T' CAP, DOUBLER AND STRAPS AND INSTALLED PER TYPICAL REPAIR NR 53-10-04B. (M)SDR USAA980307Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STATION 727A STRINGER 7L TIE CLIP. REPLACED CLIP PER EO 5393G227 9AD 93-08-04, SB 737-53-1085. (M)SDR USAA980306Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 616 AND STRINGER 4R TIE CLIP. REPLACED CLIP PER EO 5393G227 (AD 93-08-04, SB 737-53-1085). (M)SDR USAA980305Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 639 AND STRINGER 1L FRAME TIE CLIP. REPLACED CLIP PER EO 5393G227 9AD 93-08-04, SB 737-53-1085). (M)SDR USAA980304Clip · crackedCLT - DURING A Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STA 664, STR 10L, FRAME TIE CLIP. REPLACED CLIP PER EO 5393G227 (AD 93-08-04, SB 737-53-1085. (X)SDR USAA980303Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STA 727B, STRINGER 1 FRAME TO TIE CLIP. REPLACED CLIP PER EP 5393G227 (AD 93-08-04, SB 737-53-1085). (X)SDR USAA980302Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STA 807 STR 10R TIE CLIP. REPLACED CLIP PER EO 5393G227 (AD 93-08-04, SB 737-53-1085). (X)SDR USAASB98181Uplock · malfunctionedCLT - FLT 798 - CAPT REPORTED AT FL180 AND 310 KNOTS, ALL THREE LANDING GEAR EXTENDED WITH THE GEAR SELECTOR IN THE 'OFF POSITION. CREW SLOWED A/C DOWN AND RAISED THE GEAR SELECTOR TO THE 'UP' POSITION. NOSE GEAR RETRACTED AND THE MAINS STAYED DOWN FOR ABOUTSDR USAASB98174Heat Valve · failedMSY - FLT 1184 - ON CLIMB-OUT FROM MSY, THE NR 2 ENGINE FUEL HEAT VALVE TRANSIT LIGHT ILLUMINATED. THE NR 2 ENGINE OIL TEMPERATURE WAS IN THE YELLOW BAND. CRWE COULD NOT CONTROL FUEL HEAT VALVE WITH SWITCH AND TRIED RESETTING CIRCUIT BREAKER WITH NO HELP. RSDR USAASB98173Outflow Valve · failedPHL - FLT 221 - AIRCRAFT DEPARTED PHL WITH THE RIGHT AIR CONDITIONING PACK ON MEL. AFTER TAKEOFF, CREW COULD NOT GET THE LEFT PACK TO PRESSURIZE AIRCRAFT. DECISION WAS MADE TO RETURN TO FIELD AT PHL. FLT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. SDR USAASB98170Anti-Ice Duct · blownPHL - FLT 993 - AFTER TAKEOFF FROM PHL, CREW OBSERVED A RAPID RISE IN THE NR 2 ENGINE CSD OIL TEMPERATURE FOLLOWED BY A NR 2 ENGINE OVERHEAT LIGHT. CREW REDUCED THRUST ON ENGINE AND OVERHEAT LIGHT WENT OUT. AIRCRAFT WAS AT FL 080 WHEN CREW MADE DECISION TO RSDR USAASB98168Battery Pack · dischargedRDU - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY AND REPOSITIONED WIRE ON LIGHT SOCKET AT SERVICE DOOR. SYSTEM OPERATIONAL CHECK GOOD. (M)SDR USAA980301Skin · crackCLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN SKIN RT AFT SERVICE DOOR LOWER HINGE CUT-OUT ON SKIN. INSTALLED DOUBLER AND TRIPPLER PER SRM 53-30-3 FIG 33. (X)SDR USAA980296Skin · crackedCLT - DURING A DROP-IN VISUAL INSPECTION, FOUND A CRACK AT FORWARD ENTRY DOOR SKIN AT LOWER AFT CUT-OUT. INSTALLED DOUBLER/TRIPLER PER EA 41616. (X)SDR USAA980295Skin · crackedCLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN SKIN RIGHT AFT SERVICE DOOR LOWER HINGE CUT-OUT. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 33. (X)SDR 98ZZZM553Power Supply · inoperativeRDU - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY AND REPOSITIONED WIRE ON LIGHT SOCKET AT SERVICE DOOR. SYSTEM OPERATIONAL CHECK GOOD. (M)SDR USAASB98158Duct · crackedTPA - FLT 940 - DURING CLIMB-OUT FROM TPA AT FL200, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN RETARDED THROTTLE ON THE NR 1 ENGINE TO IDLE AND THE LIGHT EXTINGUISHED. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. FLT LANDED WITHOUT INSDR USAASB98150Controller · malfunctionedPHL - FLT 993 - AIRCRAFT DEPARTED PHL WITH THE LEFT PACK ON MEL DUE TO A LEFT PACK TRIP OFF LIGHT THAT WOULD NOT RESET. ON CLIMB-OUT OF PHL, AIRCRAFT WOULD NOT PRESSURIZE. CREW WENT THROUGH CHECK LIST WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDEDSDR USAASB98138Shutoff Valve · failedDAY - FLT 317 - CAPTAIN REPORTED A LOUD BANG/NOISE AT 3,000 FEET ON CLIMB-OUT OF DAY. FLIGHT ATTENDANTS FELT A VIBRATION IN THE FLOOR ALSO. CAPTAIN DID NOT NOTICE ANY CHANGE IN FLIGHT CONTROLS OR PRESSURIZATION. FLIGHT RETURNED TO FIELD AT DAY AND LANDED WISDR USAASB98129Switch · failedPIT - FLT 8565 - ON DESCENT INTO PIT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. CREW DECLARED AN EMERGENCY AND SHUT DOWN THE NR 2 ENGINE PER APPROPRIATE CHECKLIST. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GSDR USAASB98126Transmitter · malfunctionedSAV - FL1896 - CAPTAIN REPORTED THE NR 2 ENGINE INDICATED HIGH OIL PRESSURE WAS IN THE YELLOW BAND. POWER WAS REDUCED AND OIL PRESSURE DROPPED SLOWLY TO THE BOTTOM OF THE YELLOW BAND. FLIGHT DIVERTED TO SAV AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY SDR 98ZZZM487Regulator · failedSAV - FL1896 - CAPTAIN REPORTED THE NR 2 ENGINE INDICATED HIGH OIL PRESSURE WAS IN THE YELLOW BAND. POWER WAS REDUCED AND OIL PRESSURE DROPPED SLOWLY TO THE BOTTOM OF THE YELLOW BAND. FLIGHT DIVERTED TO SAV AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY SDR USAASB98125Light · inoperativeBWI - PILOT REPORTED THREE SEAT MOUNTED SINGLE BULB FIXTURES WERE FOUND INOPERATIVE AT THE EMERGENCY EXIT ROW. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN LIGHT ASEMBLY AND WIRE SAME. OPERATIONAL CHECK GOOD. (X)SDR USAA980226Skin · crackedROA - DURING J28 (BX) FOUND 1.50 INCH CRACK AT BS 767 S19L ON FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (X)SDR USAA980225Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.5 INCH LONG CRACK LOWER FUSELAGE BS 727D PLUS 1B LBL 1 SKIN. REMOVED DAMAGED NDT CONFIRM CRACK CONTAINMENT, INSTALLED AND COMPLETED REPAIR PER SRM 53-00-01. (M)SDR USAA980224Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH LONG CRACK FORWARD SIDE OF BS 727D FRAME RBL 2 FRAME. CUTOUT DAMAGED AREA, INSTALLED DOUBLER, REPAIRED PER 737-300 SRM 51-70-11 FIG 1. (M)SDR USAA980193Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK IN SKIN FORWARD SIDE OF LOWER HINGE CUTOUT AT FORWARD ENTRY DOOR. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 31. (M)SDR USAA980192Skin · scratchROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 3 INCH SCRATCH APPROX .025 INCH DEEP IN CROWN SKIN STATON 687, STRINGER 1L. BURNISHED AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAASB98111Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE CENTER AISLE CEILING BETWEEN THE EXIT HATCHES INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAASB98106Engine · failedPHL - FLT 1717 - UPON CLIMB-OUT FROM PHL, THE NR 1 ENGINE EXPERIENCED LOW POWER AND ABNORMAL ENGINE PARAMETERS. EGT, N2, AND FUEL FLOW WERE ABNORMALLY HIGH. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAISDR USAA980176Stringer · corrosionROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 1.333 INCH BY 2.5 INCH CORROSION BS 967 STRINGER 25 LEFT. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 9. (M)SDR USAASB98102Battery Pack · dischargedCLE - MAINTENANCE FOUND THE AFT CENTER OVERHEAD EMERGENCY LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (X)SDR USAASB98099Switch · failedBWI - FLT 8026 - AFTER TAKEOFF, THE NR 1 START VALVE 'OPEN' LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED AFTER THE ENGINE POWER WAS REDUCED TO IDLE. THE FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE START VALVE PRESSURE SSDR USAASB98091Fuel Pump · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN ESDR USAASB98089Battery Pack · dischargedALB - MAINTENANCE FOUND FOUR ROWS OF LOW LEVEL LIGHTING, AFT OF THE OVERWING EXIT IN THE MID CABIN, INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR 98ZZZX1641Fuel Control · defectiveBWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. AN ESDR USAA980155Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE 3 INCH BY 1.5 INCH BS 1016 BULKHEAD (FORWARD FACE) JUST ABOVE DRAIN HOLE BBL '0'0. INSTALLED CHANNEL REPAIR AND SKIN REPAIR, REPAIRED PER SRM 51-40-3 FIG 1 AND SRM 53-10-4 FIG
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