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 USAA990431Stringer · corrodedTPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH SECTION OF STRINGER 27L CORRODED AT STAITON 1010. SPLICES STRINGER PER SRM 53-10-3 FIG 1. (M)SDR USAASB99114Connector · looseBWI - FLT 2681 - DURING CLIMB-OUT FROM BWI, THE NR 2 ENGINE FUEL HEAT LIGHT ILLUMINATED. THE NR 2 ENGIN OIL TEMP BEGAN TO EXCEED LIMITS. CREW TRIED DIFFERENT POWER LEVELS, BUT THE OIL TEMPERATURE REMAINED IN THE YELLOW TO RED BAND. CREW DECIDED TO RETURN TOSDR USAA990430Skin · crackedTPA - DURING CX-1 EDDY CURRENT CHECK INSPECTION, FOUND A 2 INCH CRACK LOWER FORWARD ENTRY DOOR HINGE CUT OUT SKIN. INSTALLED DOUBLER PER TR 52-10-5. (M)SDR USAA990423Stringer · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT TERMINAL END STRINGER 26R AT STATION 540. INSTALLED NEW END FITTING PER SRM 51-10-01. (M)SDR USAA990391Web · crackedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 259 BL 0 CEILING ON NWW VERT STIFFENER WEB. REPAIRED PER SRM 51-10-01 PAGE 5. (M)SDR USAA990390Floorbeam · corrodedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 12 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M)SDR USAA990382Floorbeam · corrodedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 1 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M)SDR USAA990364Frame · crackedCLT - DURING A Q-C CHECK, VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727 LEFT STRINGER 18A OUTER CHORD FRAME. INSTALLED NEW CHORD PER EO 5394G068 AND EO 5394G076. (M)SDR USAA990363Angle · crackedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH CRACKS AT BS 727 BETWEEN STRINGER 24R AND 25R CHORD ANGLE. REPAIRED PER EA 64377, 64403 AND EO 5394G068. (M)SDR USAA990353Stringer · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2.5 INCH CORRODED AREA AT STRINGER 20L AND STATION 911 AFT CARGO. INSTALLED J ANGLE, U CHANNEL, SHIMS AND CLIP PER SRM 53-10-3 AND SRM 51-20-1. (M)SDR USAA990314Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER T/R 53-10-19 REV A AND EA 64244 AND 64167. (M)SDR USAA990313Skin · crackedCLT - DURING Q-2 CHECK HFEC INSPECTION, FOUND A .09375 INCH CRACK IN FORWARD ENTRY DOOR LOWER HINGE CUTOUT FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 31. (M)SDR USAA990312Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FLOORBEAM TO FUSELAGE ATTACH ANGLE AT BS 597, RBL 70.85 AND WL 204-208. INSTALLED ANGLE REPAIR PER EA 64287. (M)SDR USAA990309Creasebeam · corrodedCLT - DURING VISUAL CHECK INSPECTION, FOUND SEVERAL AREAS OF CORROSION AT BS 270 TO BS 360 STRINGER 17L CREASEBEAM INNER CHORD ANGLE. REPAIRED PER BOEING DRAWING 65-17688 AND SRM 51-30-3. (M)SDR USAA990303Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 947 RBL 6 FLOORBEAM. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-10-09 PAGE 26 THROUGH PAGE 30. (M)SDR USAA990302Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 986.5. SPLICED IN NEW SECTION OF FLOORBEAM 'T' CAP PER TR 53-60-01 AND EA 64288. (M)SDR USAA990301Floorbeam · corrodedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND CORROSION ALONG TOP SURFACE OF FLOORBEAM AT STATION 967, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP AND DOUBLER PER SRM 53-10-9 FIG 2 AND EA 64204. (M)SDR USAA990300Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 328 LBL 12 AND RBL 1. INSTALLED NEW 'T' CAP REPAIR ANGLES AND STRAPS PER TR 53-10-13. (M)SDR USAA990299Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 294.5 BL 0. SPLICED IN NEW 'T' CAP PER TR 53-10-04B. (M)SDR USAA990298Cap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION AT BS 344 LBL 6 AND LBL 10 FLOOR 'T' CAP, CORROSION TASK NR C53-107-01. INSTALLED NEW 'T' CAP REPAIR ANGLES AND CAPS PER TR 53-10-13. (M)SDR USAA990297Floorbeam · corrodedCLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH AREAS OF CORROSION AT STATION 967 BETWEEN LBL 10 AND RBL 50 FLOORBEAM. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64202. (M)SDR USAA990296Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE TOP OF FLOORBEAM STATION 1006, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64206, R 53-10-13. (M)SDR USAA990291Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT STATION 947 RBL 6 ON FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED ANGLE PER SRM 53-10-9. (M)SDR USAA990290Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH AREA OF CORROSION AT STATION 947 TO STATION 1016 LBL 53 INNER CHORD ANGLE, CORROSION TASK NR C53-107-02. REPAIRED PER SRM 51-10-1. (M)SDR USAA990289Floorbeam · corrodedCLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM AT STATION 328 LBL 12 AND RBL 1, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER TR 53-10-13. (M)SDR USAA990259Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 16R TIE CLIP. REPAIRED PER SRM 51-10-01. (M)SDR USAA990220Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 847 STRINGER 1 TIE CLIP. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)SDR USAA990214Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 10R TIE CLIP. REPLACED PART. (M)SDR USAA990213Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRCK BS 787 STRINGER 10L TIE CLIP. REPLACED PART. (M)SDR USAA990212Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727 STRINGER 8L TIE CLIP. REPLACED PART. (M)SDR USAA990211Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727A STRINGER 1 TIE CLIP. REPLACED PART. (M)SDR USAA990210Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 8R TIE CIP. REPLACED PART. (M)SDR USAA990209Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 15R TIE CLIP. REMOVED ORIGINAL CLIP AND HFEC PART AND STRINGER, NO CRACK FOUND. REINSTALLED ORIGINAL PART PER SRM 51-30-02. (M)SDR USAA990208Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 5R TIE CLIP. REPLACED PART. (M)SDR USAASB99104Transmitter · failedBWI - FL2785 - ON CLIMB-OUT FROM IAD, AT FL170, THE 'B' HYDRAULIC SYSTEM BRAKE PRESSURE INDICATOR FAILED AND INDICATED ZERO. ALL OTHER HYDRAULIC INDICATIONS WERE NORMAL. CAPTAIN ELECTED TO DIVERT TO BWI AND DECLARE EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT SDR USAASB99099Link · brokenBOS - FLT 2609 - AFTER GEAR RETRACTION, CREW HEARD A LOUD NOISE AND FELT A VIBRATION FROM THE NOSE GEAR AREA. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT NOSE LANDING GEAR LINK ASSEMBLY SDR USAASB99095Retract Mech · lack of lubeATL - FLT 2751 - AFTER TAKEOFF FROM IAD, THE LANDING GEAR FREE FELL (EXTENDED) WITH THE LANDNG GEAR HANDLE IN THE 'OFF' POSITION. CREW WAS ABLE TO RETRACT GEAR AND THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBRICATED THE NOSE AND SDR USAASB99094Wire · brokenROC - MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRE AT STATION 360 TERMINAL BLOCK. OPERATIONAL CHECK GOOD. (M)SDR USAASB99089Actuator · failedCLE - FL2636 - CAPTAIN STATED THAT THE NR 4 LEADING EDGE SLAT AMBER LIGHT ILLUMINATED ON INITIAL APPROACH. CREW CONFIRMED VISUALLY THAT THE SLAT WAS NOT FULLY EXTENDED AND DECLARED AN EMERGENCY. AFTER ABOUT 5 MINUTES AT FLAPS 15, THE SLAT DID FULLY EXTEND. SDR USAASB99075Battery Pack · dischargedCLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPPSDR 99ZZZM244Power Supply · failedCLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE, AND THE POWER SUPPSDR USAASB99074Battery Pack · dischargedALB - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)SDR USAASB99060Line · failedPIT - FLT 2333 - FLIGHT DIVERTED TO PIT DUE TO AN 'A' SYSTEM HYDRAULIC FAILURE. FLIGHT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE DUE TO THE LOSS OF NOSE GEAR STEERING. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLEX LINE TO THE SDR USAASB99067Battery Pack · dischargedTPA - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHT ON THE FUSELAGE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB99052Pcu · malfunctionedBWI - FLT 2710 - EN ROUTE FROM MCO-BDL, AT FL330 AND .74 MACH, FLIGHT WAS APPROACH SBY ON 'A' AUTOPILOT WHEN THE A/C STARTED PITCHING UP AND ROLLING TO RIGHT 80 DEGRES. CAPT USED FULL POWER AND FULL AILERON TO GET THE AIRCRAFT LEVEL. CAPT STATED THAT WHEN HESDR USAASB99047Power Supply · inoperativeCLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXSDR USAASB99046Battery Pack · dischargedBWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR 99ZZZM195Battery · dischargedCLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXSDR 99ZZZM194Battery Pack · dischargedCLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXSDR USAASB99041Battery Pack · dischargedTPA - MAINTENANCE FOUND THE AFT ESCAPE DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
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