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 USAA960411Floor Beam · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED FLOOR BEAM T-CAP STATION 328 RBL 12 TO RBL 48. REMOVED OUT OF LIMITS FLOOR BEAM, FABRICATED T-CAP AND SPLICED NEW SECTION IN, REPAIRED PER 737 TR 53-10-13 PART 2. (M)SDR USAASB96069Csd · failedCLT - FLT 1527 - AFTER TAKEOFF, CREW RECEIVED RIGHT GENERATOR HIGH OIL TEMPERATURE LIGHT. APU GENERATOR WAS ON MEL. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT CSD. (X)SDR USAASB96064Wire · brokenDCA - FLT 1126 - EMERGENCY FLOOR LIGHTING BROKEN RIGHT SIDE, ROW 9. MAINTENANCE FOUND BROKEN WIRE AT RIGHT SIDE, ROW 9. SPLICED BROKEN WIRE AND RESECURED LIGHT STRIP. (X)SDR USAA960366Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION ON FLOOR BEAM BS 312 8 INCH RBL. REPLACED T-CAP AND INSTALLED SPLICE ANGLES, REPAIRED PER TR NR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA960365Frame · corrosionDURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA ON FRAME AT BS 500 STRINGER 26R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA960364T-Cap · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT 2 NUT PLATE HOLES T-CAP, STATION 344 LBL 12 TO RBL 12. REPLACED T-CAPS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA960363Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER (APPROX 3 INCHES LONG) STRINGER 26L AT STATION 966. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA960362Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODED AREA STRINGER 26R BS 520-540. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA960361Chord · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT LOWER FAST HOLE OF INNER CHORD ANGLE BS 616 RIGHT FRAME WL 203. INSTALLED REPAIR ANGLE AND FILLER, REPAIRED PER EA 40996. (M)SDR USAA960360Floor Beam · gougesINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH GOUGES AT BS 360 BL ZERO LBL 12 FLOOR BEAM. INSTALLED REPAIR STRAPS, REPAIRED PER TR53-10-01A. (M)SDR USAA960359Floor Support · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 14 INCH CORRODED AREA COCKPIT ENTRANCE BS 270.0 4 INCHES LBL - 10 INCHES RBL FLOOR SUPPORT. INSTALLED Z-ANGLE REPAIR, REPAIRED PER TR 53-20-04. CORROSION TASK NR C53-107-01. CORROSION LEVEL 2. (M)SDR USAA960358Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 30 INCHES CORROSION FLOOR BEAM BS 947.5 LBL 51 TO RBL 20. REPAIRED FLOOR BEAM, REPAIRED PER TR 53-10-05C, EA 41019. (M)SDR USAA960357Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 3 INCHES CORROSION FLOOR BEAM BS 986.5 LBL 25 TO RBL 46. FILLER T-CAP AND SPLICES, REPAIRED PER SRM 53-10-9 TR 53-10-05C. CORROSION TASK NR C53-107-02. (M)SDR USAA960356Bracket · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH AT WEB NOSE GEAR ACTUATOR SUPPORT BRACKET STATION 233. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960354Tie Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 6L TIE CLIP. MODIFIED PART NR INSTALLED, 69-35352-14, REPAIRED PER EO 5393G227. (M)SDR USAA960353Tie Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 4L TIE CLIP. MODIFIED PART NR INSTALLED 69-35352-14, REPAIRED PER EO 5393G227. (M)SDR USAA960352Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER CHANNEL ,APPROX 10 INCHES IN LENGTH AND THREE 4 INCHES IN LENGTH, STATION 950-990 STRINGER 27L. REPLACED STRINGER FROM BS 950-990, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CSDR USAA360355Tie Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 747 AT STRINGER 5R TIE CLIP. MODIFIED PART NR 69-35352-14, REPAIRED PER EO 5393G227. (M)SDR USAASB96061Spoiler Actuator · crackedFLT NR 1126 - DCA - AIRCRAFT DIVERTED FROM BWO TO DCA DUE TO LOSS OF 'A' SYSTEM HYDRAULIC SYSTEM. MAINTENANCE FOUND NR 1 SPOILER ACTUATOR CRACKED. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR. AS A PRECAUTIONARY MEASURE BOTH 'A' SYSTEM HYDRAULIC PUMP WERE CHASDR USAASB96056Oil System · over servicedMIA FL - 652 - AFTER TAKEOFF, CREW NOTED OIL PRESSURE RISE ON LEFT ENGINE. CREW REDUCED POWER ON ENGINE AND NOTED OIL TEMPERATURE RISE. CREW SECURED THE LEFT ENGINE. FLIGHT RETURNED TO MIA AND LANDED WITH NO FURTHER INCIDENT. SET - 12 MINUTES. MAINTENANCESDR USAASB96055Engine · failedFLT NR 571 - CLT - NR 1 ENGINE WAS SHUT DOWN IN FLIGHT. LOUD BANG WAS HEARD AND SHORTLY THERE AFTER THE ENGINE FAILED. NO FIRE WARNING OR OTHER INDICATIONS WERE NOTED. TOTAL SINGLE ENGINE TIME WAS APPROXIMATELY 30 MINUTES. MAINTENANCE REPLACED NR 1 ENGINE SDR USAA960306Skin · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK SKIN LOWER HINGE CUTOUT LOWER CORNER OF SERVICE DOOR. INSTALLED DOUBLER, REPAIRED PER TR 52-10-05. (M)SDR USAA960305Frame · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK FRAME INNER CHORD, STATION 616 WL 203 LBL 60 LEFT SIDE. INSTALLED DOUBLER, PER EA 40894. (M)SDR USAA960304Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEB, FLOOR BEAM BS 709 TO 712 BL 25 R WL 203. CUT OUT CRACKED SECTION OF WEB, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 FIG 1. (M)SDR USAA960303Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 CRACKS .25 INCH AT WEB FOR FLOOR BEAM BL '0' BS 708 TO BS 713 WL 203. INSTALLED DOUBLERS, REPAIRED PER SRM 51-40-2. (M)SDR USAA960302Stringer · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CORRODED AREAS 7 INCH BY 1 INCH AT STRINGER BS 967 TO BS 974 AND BS 976 TO BS 982, S-25 L. REMOVED CORRODED STRINGER SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-3. (M)SDR USAA960301Floor Beam · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SIX 1 INCH BY 1 INCH CORRODED AREA AT FLOOR BEAM BS 344 LBL 50 INCH TO BL 'O'. SPLICED IN NEW SECTION OF T-ANGLE CAP. INSTALLED REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSIONSDR USAA960300Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 10 INCH BY 2 INCH, 2 INCH BY 33 INCH FLOOR BEAM STATION 987 RBL 12 TO RBL 45, LBL TO LBL 30. INSTALLED T-CAP REPAIR ENTIRE LENGTH, REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LESDR USAA960299Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 5 INCH BY 2 INCH, 1 INCH BY 2 INCH AND 1 INCH BY 4 INCH FLOOR BEAM STATION 967 LBL 6, LBL 30, LBL 20 TO LBL 25. INSTALLED T-CAP, REPAIRED ANGLES AND STRAPS. REPAIRED PER TR 53-10-05C. CORROSION TASK SDR USAA960298Stringer · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA ON STRINGER 20L, BS 767 STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR USAA960297Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 30 INCH BY 1 INCH FLOOR BEAM STATION 1006 BL '0' TO LBL 30. INSTALLED FILLER AND STRAPS, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960296Gate Hinge · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 13 INCH CRACK FORWARD RIGHT SERVICE DOOR, LOWER GATE HINGE. REPAIRED PER EA 40887. (M)SDR USAASB96039Filter Bypass Sw · intermittentFLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON. RETARDED THROTTLES, NO HELP. SHUT DOWN ENGINE AND RETURNED TO MCO. MAINTENANCE REPLACED THE FILTER BYPASS SWITCH. (M)SDR USAASB96036Engine · vibrationFLT NR 885 - GSO - ON INITIAL CLB FLIGHT ATTENDANT NOTICED A VIBRATION THROUGH THE CABIN. AT CRUISE VIBRATION CONTINUES WIHT CAPTAIN ISOLATING PROBLEM TO NR 1 ENGINE. ALL ENGINE READINGS CONTINUED TO BE NORMAL. AIRCRAFT DIVERTED TO GSO. (M)SDR USAASB96033Overheat Light · illuminatedFLT NR 800 - MCI - DURING CLIMB AT APPROXIMATELY 10,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. THE CAPTAIN REDUCED POWER AND THE LIGHT WENT OUT. PULLED NR 2 ENGINE BACK TO IDLE AND RETURNED TO MCI. (M)SDR USAASB96031T3 Blade · failedFLT 1930 - PHL - NR 1 ENG COMPRESSOR STALLED, WOULD NOT SPOOL UP AFTER. DURING TAXI BACK IDLE EGT KEPT CREEPING UP, SHUT IT DOWN A T530. AT GATE GROUND PERSONNEL REPORTED TAIL PIPE FIRE. FIRED BOTH BOTTLES AND EVACUATED AIRCRAFT. NO FIRE WARNING, FIRE WARNSDR USAA960240Fitting · crackedINT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A RIGHT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 POUND. REPAIRED PER EA 40644. (M)SDR USAA960239Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB. FABRICATED NEW WEB, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-52878. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)SDR USAA960238Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR. REPLACED WITH IDENTICAL PART NR 65-52878-533, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960237Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 RBL 36, LBL 5, RBL 5. INSTALLED DOUBLERS, REPAIR PER SRM 53-10-9 FIG 7. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960236Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RBL 20. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-46812. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)SDR USAA960235Floor Beam · gougedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES. CUT OUT DAMAGED AREA AND INSTALLED NEW SECTION WITH REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSDR USAA960234Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, STRINGER 28L. REPLACED STRINGER SECTION REPAIRED PER SRM 51-10-1, PAGE 5, STEP 4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA960233Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCHES. INSTALLED T-CAP, REPAIR PLUS 2.6 LB WT CHANGE, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960232Seat Track · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STATION 986.5. INSTALLED NEW SEAT TRACK SECTION, REPAIRED PER SRM 51-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960231Floor Support · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986.5 LNL 15 INCHES. REPLACED WITH IDENTICAL PART NR 65-46812-191, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. SDR USAA960230Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES. SPLICED IN NEW SECTION OF FLOOR BEAM, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960229Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL. REPLACED WITH INDENTICAL PART NR 65-46812-170, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA960228Intercostal · corrosionINT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INCHES BETWEEN BS 328 AND BS 344. REPLACED WITH IDENTICAL PART NR 65-45834-259, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSDR USAA960227Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 65-45834-260, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
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