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 USAA011054Skin · dentedCLT - FOUND SKIN DENTED 2 INCHES BY 8 INCHES BY .250 INCH, BS 827 STRINGER 27L. PREVIOUS REPAIR, FOUND AT S27L, REPORT STATES S27R, PER SRM 53-30-3. (M)SDR USAA011053Pressure Panel · damagedCLT - FOUND BEADS MISSING IN PRESSURE WEB, BS 662 TO BS 673 WL 203. INSTALLED ANGLE STIFFENERS PER EA 85189 REF SB 737-57-1234. (M)SDR USAA011051Support · crackedCLT - FOUND FRAME SUPPORT HAS .25 INCH CRACK, S19R BS 520. REMOVED AND REPLACED FRAME SUPPORT PER SRM 51-10-1. (M)SDR USAA011047StringerCLT - FOUND STRINGER WITH 1.5 INCH INDENTIONS CAUSED BY DRILLING TOO DEEP, ON STRINGER 16R CHANNEL LEG BETWEEN BS 787 AND 807. INSTALLED FILLER AND CHANNEL DOUBLER PER SRM 53-10-3 DETAIL V REPAIR. (M)SDR USAA011046Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706 S3L. REPLACED WITH MOD CLIP PER EO 5393G227. (M)SDR USAA011048Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH, BS 986.5 TO S 1006 BL 0 FLOOR LEVEL. REPLACED FLOOR SUPPORT PER SRM 51-10-1. (M)SDR USAA011049Brace · corrodedCLT - FOUND DIAGONAL FLOOR BRACE CORRODED 1 INCH, BS 986.5 TO 1006, LBL 10 TO LBL 19. REPLACED BRACE PER SRM 51-10-1. (M)SDR USAA011050Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 70 INCHES, BS 986.5 RBL 40 TO LBL 30. REPLACED T-CAP PER SRM 53-10-9. (M)SDR USAA011041Web · gougedCLT - FOUND WEB GOUGED .750 INCH, RBL 60 BS 328 BETWEEN BS 17R AND 18R. INSTALLED WEB REPAIR, FILLER SHIM, AND REPAIR PLATE PER SRM 51-40-2 FIG 1, AND SRM 51-30-3, 5300V153. (M)SDR USAA011040Angle · crackedCLT - FOUND ANGLE WITH TWO CRACKS .750 INCH EACH, STR 11R AND STR 13R, BS 290. INSTALLED NEW ANGLE PER SRM 51-30-2 AND 51-10-1. (M)SDR USAA011043Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 30 INCHES, FORWARD SERVICE DOOR Z-ANGLE BS 300. REMOVED AND REPLACED WITH PART NR 1138222 PER SRM 51-10-01. (M)SDR USAA011044Angle · corrodedCLT - FOUND ANGLE CORRODED 1 INCH BY 27 INCHES, BS 303 TO RBL 55. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED WITH PART NR 1123138 PER SRM 50-10-1. (M)SDR USAA011042Floorbeam · corrodedCLT - FOUND FLOORBEAM UPPER CHORD 2 INCHES BY 31 INCHES, BS 344, FLOORBEAM LBL 11-42. SPLICED IN NEW SECTION OF T-CAP BETWEEN LBL 30 TO RBL 17 PER TR 737-200, 53-10-13. (M)SDR USAASB01225Battery Pack · inoperativeBWI - MAINTENANCE FOUND THE FORWARD EXTERIOR ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB01226Wire · brokenBDL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING. OPERATIONAL CHECK NORMAL. (M)SDR USAA011027Crease Beam · crackedCLT - FOUND CREASE BEAM CRACKED .750 INCH, BS 520 LBL 64. EXTRUDED SECTION REPAIR, SPLICE REPLACEMENT PER SRM 51-40-4 FIG 1. (M)SDR USAA011026Web · crackedCLT - FOUND WEB CRACKED .125 INCH, BS 178 BULKHEAD AT WL 234 AT RBL 10. INSTALLED DOUBLER PER SRM 53-10-11 FIG 1, 53-10-1. (M)SDR USAA011038Tie Clip · gougedCLT - FOUND TIE CLIP GOUGED .5 INCH, BS 727A AT 518R. INSTALLED NEW TIE CLIP PER SRM 51-10-101. (M)SDR USAA011037Frame · gougedCLT - FOUND FRAME GOUGED AND DENTED .040 INCH, BS 1006 LBL 41 WL 207. FASTENER INSTALLED PER SRM 53-10-1 FIG 1 SRM 51-30-02. (M)SDR USAA011036Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED 5 INCHES, BS 727 BL 0 WL 203. REMOVED AND REPLACED SUPPORT FITTING PER EO 5394G176. (M)SDR USAA011035Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 767 AT S13L. REMOVED DAMAGE, INSTALL CHANNEL AND FILLER PER SRM 53-10-4. (M)SDR USAA011034Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 807, S13L. REMOVED DAMAGE, INSTALLED CHANNEL AND FILLER PER SRM 53-10-4. (M)SDR USAA011033Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 747, STRINGER 13L. REMOVED DAMAGED AREA, INSTALLED CHANNEL AND FILLER PER SRM 53-10-4. (M)SDR USAA011032Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706 S2L. REMOVED AND REPLACED TIE CLIP PER EO 5393G-227. (M)SDR USAA011031Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597 S9L. REMOVED AND REPLACED THE TIE CLIP CCN 1122006 PER SRM 737-200 51-30-2. (M)SDR USAA011030Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 685 S2L. REMOVED AND REPLACED TIE CLIP PER EO 5393L-227. (M)SDR USAA011025Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706 STRINGER 10L. REMOVED AND REPLACED TIE CLIP PER PCI JOB CARD J253-10-10R. (M)SDR USAA011024Clip · crackedCLT - FOUND CLIP CRACKED 1 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED CLIP PER SRM 51-10-02. (M)SDR USAA011023Web · crackedCLT - FOUND WEB CRACKED .125 INCH, BS 178 BULKHEAD AT WL 234 AT LBL 10. INSTALLED EXTERNAL DOUBLER PER SRM 53-10-11 FIG 1. (M)SDR USAA011029Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3.5 INCHES, BS 294.5 LBL 1.5 TO RBL 1.5. CORROSION LEVEL 1, TASK NR C53-107-01. UPPER T-CHORD REPAIRED PER TR 53-10-04 B. (M)SDR USAA011028Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 294.5 LGL 709. CORROSION LEVEL 1, TASK NR C53-107-01. UPPER T-CHORD REPAIRED PER TR 53-10-04 B. (M)SDR USAASB01216Battery · dischargedBWI - THE EMERGENCY EXIT SIGN AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. (M)SDR USAASB01211Light · failedLGA - THE AFT SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)SDR USAASB01210Power Supply · dischargedBWI - MAINTENANCE FOUND THE MID-CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY. OPERATIONAL CHECK GOOD. (M)SDR USAA010864Skin · crackedCLT - FOUND SKIN CRACKED .0625 INCH, BS 303, WL 259.88 MED UPPER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 AND EA 85093. (M)SDR USAA010868Skin · crackedCLT - FOUND UPPER WING SKIN CRACKED .25 INCH, LEFT WING WBL 165.5 AT REAR SPAR, BS 178. INSTALLED DOUBLER AND TRIPLER PER EA 85075. (M)SDR CA010815002Pump · failed(CAN) 1. EXTENGUISHED. NR 1 115 VAC TR BUS INOP. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN FUEL TANK, AFT FUEL BOOST PUMP UNSERVICEABLE. BOOST PUMP CHANGED IAW MM 28-22-41. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.SDR USAA010880Angle · crackedCLT - FOUND WEB ANGLE CRACKED 1.25 INCH, BS 303.9, STRINGER 10L. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)SDR USAA010879Frame · crackedCLT - FOUND SIDE CHORDS WITH TWO CRACKS LEFT AND RIGHT .250 INCH, BS 178 WL 206 RBL 28 AND LBL 28. DAMAGE SECTION REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)SDR USAA010866Frame · crackedCLT - FOUND VERTICAL CHORD CRACKED .25 INCH, BS 178, LBL 5.7, WL 184. DAMAGE REMOVED, INSTALLED REPAIR ANGLES AND STRAP PER EO 5300V155. (M)SDR CA010815001Transformer · faulty(CAN) AT CRUISE, A SNAPPING NOISE WAS HEARD. NR 1 TR CB POPPED. NR 1 MAIN FUEL TANK AFT FUEL BOOST PUMP CB POPPED ALONG WITH NUMEROUS C/P LIGHTS. #1 ENGINE OIL TEMP INDICATOR, CAPT'S AUX. PITOT STATIC AND NO SMOKING & FASTEN SEAT BELT SIGNS ALL NOT OPERATING. SDR USAA010757Keelbeam · corrodedCLT - FOUND KEEL BEAM CORRODED 1 INCH DIAMETER BY .020 INCH DEEP, BS 727 PLUS 16, S27L. CORROSION REMOVED, AND REPAIR INSTALLED PER EA 94208, ALONG WITH ACCESS SKIN REPAIR PER SRM 53-30-3. (M)SDR USAA010764Keelbeam · corrodedTPA - FOUND LEFT HAND KEEL BEAM CORRODED .75 INCH DIAMETER BY .020 INCH DEEP, BS 727 PLUS 16, LOWER SURFACE. DAMAGE REMOVED, KEEL BEAM REPAIRED PER EA 94208. ACCESS REQUIRES SKIN REPAIR PER SRM 53-30-3, FIG 6. (M)SDR USAASB01181Battery · dischargedBOS - THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAA010765Stringer · corrodedCLT - FOUDN STRINGER CORRODED 10 SQUARE INCHES, BS 967, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3, FIG 1. (M)SDR USAA010748Stringer · corrodedTPA - FOUND STRINGER CORRODED 10 SQUARE INCHES, PREVIOUSLY SPLICED SECTION OF STRINGER 27L AT STATION 967. CORROSION LEVEL 1. SPLICED IN NEW SECTION OF STRINGER USING SPLICES RETAINED FROM PREVIOUS REPAIR PER SRM 53-10-3 FIG 1. (M)SDR USAA010749Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, AFT OF STATION 907 STRINGER 18L. INSTALLED DOUBLER PER EA 71383 AND SRM 53-00-01 FIG 223. (M)SDR USAA010766Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, BS 907, STRINGER 18L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-01, AND EA 7183. (M)SDR USAA010751Bulkhead · crackedCLT - FOUND BULKHEAD WEB WITH NUMEROUS CRACKS RANGING FROM .125 INCH TO .75 INCH, BS 178 WL 207 TO 234, LBL 12.6 TO RBL 11.7. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153, EA 69807 AND 69774. (M)SDR USAA010752Frame · crackedCLT - FOUND VERTICAL CHORD WITH TWO CRACKS EACH 1 INCH LONG, BS 178 WL 181 AT RBL 5.7 AND WL 184 AT LBL 5.7. DAMAGE REMOVED, INSTALLED REPAIR ANGLES ADN STRAPS PER EO 5300V155. (M)
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