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 USAA990882Web · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK SHEAR BEAM WEB SHELF 18A AFT WW BULKHEAD. INSTALLED DOUBLER PER EA 65323. (M)SDR USAA990877Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. INSTALLED DOUBLER PER SRM 52-10-01. (M)SDR USAA990876Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION STATIO N1006, LBL 26 FLOORBEAM. CORROSION LEVEL 1. INSTALLED REPAIR STRAP PER EA 65360 AND SRM 53-00-51 FIG 203. (M)SDR USAA990875Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION LBL 21, 28, 35, 42 AND 45, BS 344, WL 208.1 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M)SDR USAA990855Angle · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK AT BS 289.5 STRINGER 10R WEB ANGLE. INSTALLED NEW WEB ANGLE PER SRM 51-10-02. (M)SDR USAA990843Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616, STRINGER 8L TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)SDR USAA990842Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616, STRINGER 4R TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)SDR USAA990841Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 663.75 AT STRINGER 10R. REPLACED CLP PER SRM 51-10-02. (M)SDR USAA990840Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 727D STRINGER 4R. REPLACED CLIP PER SRM 51-10-02. (M)SDR USAA990839Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 887, STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA990838Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 5R SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)SDR USAA990837Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 4L SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)SDR USAA990824Shear Tie · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SHEAR TIE STATION 639 STRINGER 7R AND 8R. REPAIRED PER SRM 51-40-02. (M)SDR USAA990823Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727D STRINGER 7R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA990822Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 3R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA990821Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 5L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)SDR SWAA991437Lens · missingDURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING AT ROW 15. REPLACED LENS PER MM.SDR AWXA9900329Skin · crackedFUSELAGE SKIN CRACKED JUST AFT OF E & E EXHAUST OUTLET. REPAIRED IAW EO 53-30-13.SDR USAASB99207Window · crackedTPA - FLT 2335 - EN ROUTE FROM FLL TO CLT, THE CAPTINS L2 SLIDING WINDOW CRACKED. FLIGHT DIVERTED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS L2 SLIDING WINDOW AND THE WINDOW HEAT CONTROLLER (P/N 231-2). OPERATISDR USAA990884Support · corrodedTPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION AFT CARGO FLOOR SUPPORT STATION 860. CORROSION LEVEL 1. INSTALLED ANGLE PER TR 53-10-06. (M)SDR USAA990883Floorbeam · crackedTPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK FLOORBEAM AT BS 807 AFT CARGO COMPT. INSTALLED DOUBLER PER EA 65091 SRM 51-70-10/53-00-51 SECT 41, 43 PAGE 201 AND 202. (M)SDR USAA990928Frame · crackedPIT - DURING RON, FOUND .8750 INCH CRACK IN RADIUS OF Z-ANGLE DOOR FRAME AT R1 ABOVE BOTTOM HINGE CUT-OUT IN DOOR OPENING. STOP DRILLED CRACK, INSTALLED TITANIUM DOUBLER PER SRM 53-10-15, FIG 3, SH 2/ER 07-07-90/EA 52711. (X)SDR AWXA9900267Skin · crackedC-CHECK, FUSELAGE SKIN DOUBLER/TRIPLER CRACKED AT C2 DOOR CUTOUT, FWD LOWER CORNER. FASTENERS REMOVED FOR ACCESS, SUSPECT AREA INSPECTED WITH HIGH FREQ EDDY CURRENT. NO CRACKS FOUND. NEW DOUBLER REPAIR MANUFACTURED AND INSTALLED AS PER ER 3-53-36-08. PRESSSDR AWXA9900266Skin · delaminatedC-CHECK, FWD LOWER SPAR FLANGE DELAMINATED AND DAMAGED IN 3 SPOTS ON LT AILERON. REPAIRED PER AWA ER 3-57-51-17A.SDR AWXA9900265Skin · wornC-CHECK, WEAR MARK IN UPPER SURFACE OF LT O/B FOREFLAP MID SECTION. REMOVED FOREFLAP, REPAIRED PER ER 3-57-52-162, REINSTALLED FOREFLAP AND OPERATIONALLY CHECKED OK PER AWA T/C R3M27002.SDR AWXA9900264Support · crackedC-CHECK, CRACKED NLG ACTUATOR SUPPORT BEAM VERTICAL WEB AT FWD END. REMOVED AND REPLACED WEB PER DWG 65-45819.SDR AWXA9900260Spar · delaminatedC-CHECK, RT AILERON FRONT SPAR LOWER FLANGE DELAMINATED AT I/B HINGE AND I/B CLOSING RIB. RT AILERON REMOVED PER J/C R3M27015, REPAIRED PER ER3-57-51-17A, BALANCE CHECKED AND REINSTALLED PER J/C R3M27015. FUNCTIONAL CHECKED GOOD PER J/C R3M27015.SDR USAA990795Stringer · crackedCLT - ON PARKED, OUT OF TIME AIRCRAFT, FOUND 1.5 INCH CRACK AT STR 22R, STA 809. INSTALLED DOUBLER PER SRM 53-00-01. (X)SDR USAASB99194Fuse · blownPHL - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM ON OVERNIGHT CHECK, MAINTENANCE FOUND THE FIRST CLASS SEAT EMERGENCY LIGHTS FAILED TO FULLY ILLUMINATE. MAINTENANCE REPLACED A BLOWN FUSE FOUND IN THE BATTERY CHARGER AND REMOVED AND REPLACED THE BATTERYSDR USAA990811Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT HORIZONTAL STABILIZER CROSSBEAM ATTACH ANGLE 7 INCH LBL. FABRICATED NEW ANGLE SRM 51-40-02. (M)SDR USAA990810Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK BOTTOM END OF FRAME STA 616 INBOARD CHORD ANGLE RT SIDE FRAME. INSTALLED FILLER AND DOUBLER PER SB 737-53-1182 AND EA 64972. (X)SDR USAA990809Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 639 STR 5L TIE CLIP. REMOVED AND REPLACED PER SRM 51-10-02 AND SRM 51-40-03. (X)SDR USAA990808Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 639 STR 4L TIE CLIP. REMOVED AND REPLACED PER RM 51-10-02 AND SRM 51-40-01. (X)SDR USAA990807Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT STA 706 STR 1 TIE CLIP. REPLACED PER SRM 51-10-02. (X)SDR USAA990806Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 663 STR 14R TIE CLIP. REMOVED AND REPLACED PER SRM 51-10-02. (X)SDR USAA990805Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 663 STR 14L TIE CLIP. REMOVED AND REPAIRED PER SRM 51-10-02. (X)SDR USAA990804Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK AT STA 18A SHEAR BEAM WEB LEFT SIDE 1 INCH FORWARD OF STA 727, LBL 60, WL 188.5. REPAIRED PER SRM 53-10-02. (X)SDR USAA990803Bulkhead Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 204, RBL 5, PRESSURE BULKHEAD WEB. REPAIRED PER TR 53-10-07, REV A. (X)SDR USAA990802Bkhd Intercostal · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURENT INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 195, RBL 25, AFT SIDE PRESSURE BULKHEAD INTERCOSTAL. INSTALLED ACCESS COVER PER SRM 53-10-08. (X)SDR USAA990801Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 807 STR 8 AND 9L FUSELAGE FRAME AT FASTENER HOLE. REPAIRED PER SRM 53-00-07 FIG 202. (X)SDR USAA990800Tie Clip · crackedCLT- DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 639 AND STR 2L TIE CLIP. REPAIRED PER RM 51-10-02. (X)SDR USAA990799Stringer · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 908 STR 9L. REPAIRED PER SRM 51-10-02. (X)SDR USAA990797Floorpan · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION 2 INCH BY 2 INCH AT STA 1024, RBL 6, WL 208 FLOORPAN. CORROSION LEVEL 1, CORROSION NR C53-107-02. FABRICATED NEW STRAP PER DRAWING 6546812 AND SRM 51-10-02. (X0SDR USAA990796Intercostal · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES STA 1010, LBL 12, WL 208 INTERCOSTAL. CORROSION LEVEL 1, CORROSION NR C53-107-02. (X)SDR USAA990793Intercostal · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES STA 1020, LBL 9, WL 208 INTERCOSTAL. CORROSION LEVEL 1, CORROSION NR C53-107-02. REPLACED CAP PER SRM 53-10-51. (X)SDR USAA990764Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH SKIN ATTACH CHORD CRACK STA 1016 BETWEEN STR 3R AND STR 4L. FABRICATED, SPLICE ANGLES PER EA 65021. (X)SDR USAA990763Floorbeam · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 1 INCH AREA OF CORROSION AT STA 773, LBL 3 FLOORBEAM AFT CARGO. CORROSION LEVEL 2. CUT OUT CORROSION, INSTALLED REPAIR ANGLE, DOUBLER PER TR 53-10-06, SRM'S 51-30-09, 51-10-02, 51-20-01/05. (X)SDR USAA990762Floorbeam · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 21 INCH BY 1 INCH AREA OF CORROSION AT STA 773, RBL 14 FLOORBEAM AFT CARGO. CORROSION LEVEL 2. INSTALLED NEW SECTION OF FLOORBEAM AND SPLICE PER SRM 53-00-53. (X)SDR USAA990759Bulkhead Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, RBL 02, WL190 WEB. INSTALLED DOUBLER PER TR 53-10-08 FIG 203. (X)SDR USAA990758Bulkhead Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 02, WL 190 WEB. (X)
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