Boeing 737-201
Service difficulty reports · 2,471
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 = '737201' 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 = '737201' 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 USAA0212Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 727B, STRINGER 2L TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0213Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 747, STRINGER 4R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0214Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 807, STRINGER 11R TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA0215Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0216Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 639, STRINGER 4L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0217Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 578, STRINGER 5L TIE CLIP. REPAIRED PER EO 5393G227. (M)SDR USAA0218Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT STATION 344, LBL 9 FLOORBEAM. CORROSION LEVEL 1. INSTALLED FILLER AND REPAIR ANGLE PER SRM 53-10-9. (M)SDR USAA0219Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES STATION 947.5 FROM LBL 17 - RBL 17 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-9, TR 53-10-05A, AND EA 66592. (M)SDR USAA0220Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 312, LBL 11 AND BL 0 FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-0 FIG 5 AND IAW 51-10-9 FIG 5. (M)SDR USAA0221Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 500B ABOVE STRINGER 26R FRAME. CORROSION LEVEL 1. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. (M)SDR USAA0222Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 234, WL 190, RBL 6 ON NG TRAVERSE BEAM. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)SDR USAA0223Stringer · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION STATION 1006, STRINGER 24R. CORROSION LEVEL 2. TASK NR C53-202-01. REPLACED PART PER SRM 51-10-1. (M)SDR USAA0224Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 40 INCH AREA OF CORROSION STATION 957-1006, RBL 54 FLOOR LEVEL Z-ANGLE. CORROSION LEVEL 1. TASK NR C553-107-02. REPLACED PART PER BOEING DWG 65-45855 AND SRM 51-10-1. (M)SDR USAA0225Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 46 INCH AREA OF CORROSION FLOORBEAM 986.5 BETWEEN BBL 0 - RBL 46. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0226Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 986.5 LBL 17. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0227Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND PATCHES OF CORROSION WITHIN 34 INCHES STATION 986.5 BETWEEN LBL 17 AND RBL 17 FLOORBEAM. CORROSION LEVEL 1. TASK NR C53-107-02. REPLACED T-CAP PER TR 53-60-01 REV A. (M)SDR USAA0228Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 24 INCH AREA OF CORROSION LEFT AFT ENTRY Z-ANGLE. CORROSION LEVEL 1. TASK NR C53-107-02. FAB REPAIR DOUBLERS AND FILLER PER SRM 51-40-03 FIG 1. (M)SDR USAA0208Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B, STR 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)SDR USAA000200Skin · crackedCLT - FOUND LOWER FORWARD CORNER OF AFT SERVICE DOOR CUTOUT SKIN HAS A 2 INCH CRACK. INSTALLED REPAIR PLATES PER SRM 53-30-3. (M)SDR USAA000201Stringer Clip · crackedCLT - STRINGER CLIP HAS A .25 INCH CRACK AT BS 727B STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-00. (M)SDR USAA000202Stringer · crackedCLT - STRINGER 18A HAS A 1.5 INCH CRACK AT BS 727. REPAIRED PER SRM 51-10-01. (M)SDR USAA0203Gusset · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS OF GUSSET AT BS 259, BBL 0, WL 193 TOP OF NG W/W. REPLACED GUSSET PER SRM 51-10-01. (M)SDR USAA0204Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 727A STRINGER 5L TIE CLIP. REMOVED AND REPLACED CLIP PER EO 5393G227. (M)SDR USAA0205Floorbeam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SIX .5 INCH CRACKS BL 0 LONGITUDINAL FLOORBEAM WEB LOWER FASTENERS STATION 707 TO 715. REPAIRED NEW SECTION PER TR 57-10-05. (M)SDR USAA0207Stringer Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B, STRINGER 7L TIE CLIP. INSTALLED DOUBLER PER SRM 51-10-01. (M)SDR USAA000193Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 7 INCHES, STATION 328, BETWEEN LBL 26 AND 33 FLOOR LEVEL. INSTALLED NEW SECTION/SPLICE PER TR 53-10-13. CORROSION LEVEL 1. (M)SDR USAA000192Skin · crackedTPA - FOUND .5 INCH SKIN CRACK, STATION 540, JUST BELOW LAP AND STRINGER 14L SKIN. INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 AND EA 66144. (M)SDR USAA000191Skin · crackedCLT - FOUND SKIN WITH 1 INCH CRACK, BS 755, STRINGER 18R, RT FUSELAGE SKIN. CUTOUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1. (M)SDR USAA000188Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 727 STRINGER 24R CHORD ANGLE. INSTALLED NEW CHORD AND DOUBLER PER EA 66451 AND SRM 51-40-2. (M)SDR USAASB00037Line · leakingTYS - FLT 2700 - EN ROUTE FROM BWI TO MSY, AT FL350, A PASSENGER SEATED AFT OF THE NR 2 ENGINE ADVISED FLIGHT ATTENDANT OF AN OIL LEAK ON THE INBOARD SIDE OF THE NR 2 ENGINE. FLIGHT ATTENDANT ADVISED CAPTAIN. CAPTAIN WALKED TO BACK OF CABIN AND SAW A LARGE ASDR USAASB00036Charger · failedCLE - WHILE ACCOMPLISHING A CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT AND ASSOCIATED INTERIOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M193 BATTERY PACK (P/N 61-0478-9) AND CHARGER ASSEMBLY. OPERATIONAL CHESDR USAASB00035Harness · chafedDTW - FLT 517 - INBOUND TO DTW FROM CLT, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED WITH LOSS OF ASSOCIATED SYSTEMS. THE AIRCRAFTS APU WAS ON MEL FOR NOT BEING ABLE TO START. THIS RESULTED IN THE AIRCRAFT BEING REDUCED TO ONE POWER SOURCE AVAILABLE. CAPT SDR USAA000186Frame · crackedCLT - FOUND 2 INCH CRACK, BL 0, STATION 727 COMPRESSION CHORD. REPAIRED PER TR 53-10-03. (M)SDR USAA000185Frame · crackedCLT - FOUND .5 INCH CRACK, STATION 727, RBL 28 COMPRESSION CHORD. REPAIRED PER TR 53-10-03. (M)SDR USAA000160Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, STATION 295.5 FLOOR LEVEL 54 INCHES FROM RBL. INSTALLED DOUBLER AND FILLER PER SRM 51-40-3 FIG 1. (M)SDR USAA000152Skin · crackedTPA - FOUND .25 INCH SKIN CRACKED AT STATION 305.9 FORWARD ENTRY DOOR UPPER HINGE. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 76. (M)SDR USAASB00032Pump · failedCLT - FLT 2876 - EN ROUTE FROM MIA TO IAD, FUEL GAUGES BECAME UNRELIABLE. LEFT FUEL QTY INDICATOR STUCK AT 10.5 AND THE CENTER TANK RIGHT FUEL PUMP WOULD NOT PRESSURIZE. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SDR USAA000137Floorbeam · corrodedCLT - Q-1, BS 1016 LT LENGTH OF FLOORBEAM HAS CORROSION LEVEL 1. REPLACED WEB, T-CAP PER TR 53-60-02 AND SRM 51-40-02. (M)SDR USAA000136Seat Track · corrodedCLT - Q-1, FOUND CORROSION AT RBL 39 STATION 1000 TO 1014 FLOOR SEAT TRACK 1 INCH BY 14 INCH CORROSION LEVEL 1. INSTALLED NEW SEAT TRACK PER SRM 51-10-2 AND 51-30-03. (M)SDR USAA000135Skin · crackedCLT - Q-1, FOUND .25 INCH CRACK, LOWER FORWARD CORNER AFT ENTRY DOOR CUTOUT. REPLACED PARTS PER SRM 53-30-3 FIG 24. (M)SDR USAA000134Fitting · crackedCLT - Q-1, FOUND .5 INCH CRACK, LOWER DOOR STOP FITTING. REPLACED FITTING PER DRAWING 6517685. (M)SDR USAA000133Tie Clip · crackedCLT - Q,1, FOUND .1 INCH CRACK STATION 578, STRINGER 7R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-1 AND EO 5393G227. (M)SDR USAA000132Strap · crackedCLT - Q-1, FOUND 1 INCH CRACK, STRINGER 5A JUST AFT STATION 1138. INSTALLED REPAIR DOUBLER PER EA66501 AND SRM 53-00-1. (M)SDR USAA000131Tie Clip · crackedCLT - Q-1, STRINGER 17 TIE CLIP AT STATION 1138, HAS 1 INCH CRACK. REPLACED TIE CLIP PER SRM 51-10-1. (M)SDR USAA000130Tie Clip · crackedCLT - Q-1, STRINGER 161 TIE CLIP AT STATION 1138, HAS A .75 INCH CRACK. REPLACED TIE CLIP PER SRM 51-40-1. (M)SDR USAA000129Shear Tie · crackedCLT - Q-1, STATION 1104 STRINGER 161 INBOARD SIDE FRAME SHEAR TIE HAS A .5 INCH CRACK. INSTALLED SHEAR TIE PER SRM 51-10-1. (M)SDR USAA000128Tie Clip · crackedCLT - Q-1, STRINGER 21 AT FRAME 616 TIE CLIP HAS A .5 INCH CRACK. REPLACED TIE CLIP PER EO5393G227 PART 3. (M)SDR USAA000127Floorbeam · crackedCLT - Q-1, STATION 707, LBL 25, WL 202.5 FLOORBEAM WEB HAS A 1.5 INCH CRACK. REPLACED PARTS PER SRM 51-40-2. (M)SDR USAA000126Frame · crackedCLT - Q-1, STATION 663 BULKHEAD UPPER FRAME RBL 23, WL 201.5 HAS A .5 INCH CRACK. REPLACED VERTICAL ANGLES AND CHORD PER BOEING 65C37732. (M)SDR USAA000125Crease Beam · crackedCLT - Q-1, STRINGER 17R CREASE BEAM 8 INCH AFT STATION 639 FRAME CREASE BEAM WEB HAS A .375 INCH CRACK AT WL 208. REPLACED WEB PER SRM 51-10-02. (M)
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