Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA991214Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500 RIGHT STRINGER 15 SHEAR TIE DAMAGE AT STRINGER AND FRAME. REMOVED AND REPLACED PER SRM 51-10-2. (M)SDR USAA991213Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 2 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)SDR USAA991212Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 3 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)SDR USAA991211Skin · crackedCLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER PER EA 65982 AND TR 54-50-04D. (M)SDR USAA991210Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 10 INCH AREA OF CORROSION AT AFT ENTRY DOOR FLOOR Z-ANGLE, CORROSION LEVEL 1. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR USAA991208T-Cap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TEN 1 INCH BY 1 INCH AREAS OF CORROSION ON UPPER CAP OF T-CAP STATION 967, CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-05. (M)SDR USAA991207Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT AFT ENTRY DOOR Z-ANGLE (CHANNEL), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED AFT ENTRY DOOR Z-ANGLE PER SRM 51-10-02. (M)SDR USAA991206Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FLOOR), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR USAA991205Seat Track · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 727B-947 SEAT TRACK, CORROSION LEVEL 2. INSTALLED SEAT TRACK PER SRM 53-00-52. (M)SDR USAA991204Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH MULTIPLE AREA OF CORROSION AT BS 986.5, RBL 44 - LBL 45, FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED FLOORBEAM T-CAP PER TR 53-60-01 AND SRM 53-00-51 FIG 202. (M)SDR USAA991198Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 908 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07. (M)SDR USAA991197Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND SRM 53-00-07. (M)SDR USAA991196Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991195Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 827 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991194Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.2 5INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991193Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991192Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)SDR USAA991191Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727 STRINGER 14L OUTER CHORD ANGLE. REPAIRED DOUBLER AND TRIPLER PER EA 65952. (M)SDR USAA991190Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK IN FUSE FRAME AT FASTENER HOLE BS 480 BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)SDR USAA991189Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACKS IN 2 PLACES STATION 178 WEB A AND WEB B, LBL 1 AND RBL 1 SKIN. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA991188Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS AT BS 663, LBL 32 CEILING PRESSURE DECK. INSTALLED DOUBLER PER TR 53-60-04 AND SRM 53-60-51. (M)SDR USAA991187Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RIGHT HORIZONTAL STABILIZER LOWER SURFACE STATION 111-166 SKIN. INSTALLED DOUBLER AND FILLER PER SRM 55-10-01 AND TR 55-10-07A. (M)SDR USAA991186Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK THROUGH RIVET HOLE BS 847, STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991185Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .250 INCH CRACK AT BS 727B STRINGER 4L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991184Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 807 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991183Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 887 STRINGER 91 BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991182Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 787 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)SDR USAA991181Beam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES T-CAP STATION 967 BEAM. REPAIRED DOUBLER AND T-CAP PER TR 53-10-05. (M)SDR USAA991168Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178, 5 INCHES BELOW FLOOR AT STIFFENER 3 SKIN. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)SDR USAA991167Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178, 5 INCHES BELOW FLOOR AT STIFFENER 2, SKIN. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)SDR USAA991166Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950. (M)SDR USAA991159Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH AREA OF CORROSION AT STATION 312, LBL 21 TO RBL 22 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED IN NEW CAP SECTION PER SRM 53-10-51. (M)SDR USAA991158Shear Tie · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 597 STRINGER 1 SHEAR TIE SPLICE. INSTALLED SHEAR TIE PER SRM 51-10-02. (M)SDR USAA991157Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .500 INCH WIDE AREA OF CORROSION AT STATION 360, CORROSION LEVEL 2. INSTALLED STRAP PER SRM 53-00-51. (M)SDR USAA991156Shear Tie · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STATION 500 STRINGER 15R SHEAR TIE. INSTALLED SHEAR TIE PER SRM 51-10-02. (M)SDR USAA991155Splice · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 908 STRINGER 4L SPLICE. INSTALLED NEW SPLICE PER SRM 51-40-02. (M)SDR USAA991154Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616 STRINGER 2L CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991153Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 639 STRINGER 2L CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991152Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 639 STRINGER 1L CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991151Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616 STRINGER 1L CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAASB99270Light · inoperativeTPA - MAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE AT SEAT ROWS 17C AND 19C. MAINTENANCE REPAIRED BROKEN WIRES AT SEAT ROWS 17C AND 19C. OPERATIONAL CHECKED GOOD. (M)SDR USAASB99265Line · leakingPHL - FLT 2204 - AFTER TAKEOFF AND GEAR RETRACTION FROM PHL, FLIGHT LOST A SYSTEM HYDRAULICS. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. CAPTAIN TAXIED AIRCRAFT TO WITHIN 30 FEET OF GATE AND WAS THEN TOWED IN FROM THERE. NO EMERGENSDR USAA991270Fork · corrodedPIT - DURING CX6 CHECK, FOUND ROD END CORROSION AND FITTING THREADS STRIPPED (SPHERICAL FORK END AND ATTACH CASTING) AT RIGHT WING OUTBOARD AFT TRAILING EDGE FLAP CONTROL ROD FITTING. REPLACED FOR END AND ATTACH CASTING. (M)SDR 99ZZZM819Casting · corrodedPIT - DURING CX6 CHECK, FOUND ROD END CORROSION AND FITTING THREADS STRIPPED (SPHERICAL FORK END AND ATTACH CASTING) AT RIGHT WING OUTBOARD AFT TRAILING EDGE FLAP CONTROL ROD FITTING. REPLACED FOR END AND ATTACH CASTING. (M)SDR USAASB99264Sensor · failedCHS - FLT 542 - DURING CLIMB-OUT FROM CHS, FLIGHT EXPERIENCED A FAILURE OF BOTH ATC TRANSPONDERS AND THE LEFT NAV FUNCTION OF THE AUTOPILOT. FLIGHT RETURNED TO FIELD AT CHS AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT THEN TAXIED TO THE GATE. NO EMERGENCY WASDR USAA991209Skin · crackedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 380, DIRECTLY AFT OF EQUIPMENT COOLING DUCT OUTLET FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M)SDR USAASB99262Selector Panel · failedBWI - FLT 401 - CRUISING AT FL350, LGA-TPA, CABIN ALT WARNING HORN SOUNDED. THE CABIN ALTITUDE INDICATED 10,500 FT AND THE CABIN WAS CLIMBING AT APPROX 1,000 FT PER MINUTE. A DESCENT WAS INITIATED TO A FLT ALTITUDE OF 10,000 FT. DURING DESCENT, THE STANDBY SDR USAASB99261Coffeemaker · malfunctionedIAD - FLT 488 - EN ROUTE FROM PIT-BWI, F/A REPORTED SMELL OF BURNING WIRES AND FUMES IN THE AFT CABIN. NO VISIBLE SMOKE WAS NOTED. AN EMERGENCY WAS DECLARED AND FLT DIVERTED TO NEAREST AIRPORT AT IAD. FLT LANDED W/O FURTHER INCIDENT. MX RAN BOTH ENGINES TOSDR USAA991202Splice · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 0.01 INCH CRACK STA 908 STR 4R STRINGER SPLICE. REPLACED WITH IDENTICAL PART C/C 1122424. (X)SDR USAA991201Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 907 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65850. (M)
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