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 USAA010753Frame · crackedCLT - FOUND SIDE CHORDS WITH TWO CRACKS .25 INCH AT RBL 26, 1 INCH AT LBL 24, BS 178 WL 195 AT LBL 24 AND WL 207 AT RBL 26. DAMAGED SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157. (M)SDR USAA010642Skin · crackedTPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER SRM 53-30-3 FIG 1 AND MPP 308-25. (M)SDR USAA010643Skin · crackedTPA - FOUND SKIN CRACKED 2.5 INCH AND 2.75 INCH, STATION 873 AND 885 ABOVER 19R. INSTALLED DOUBLER .063 INCH CLAD 2024TB USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)SDR CA010703003Skin · cracked(CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L. REPAIR AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88,88A.SDR CA010625002Skin · cracked(CAN) CRACKED FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 ABD 767, STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1 PAGES 87,88 & 88A.SDR USAA010679Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BETWEEN BS 727A AND 727B, BELOW S13L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)SDR CA010703004Skin · cracked(CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, 8 INCHES AFT. OF STATION 750 AT STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88, 88A.SDR CA010625003Skin · cracked(CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, 8 INCHES AFT. OF STATION 750 AT STRINGER 17L.REPAIRED AS PER SRM 53-30-3, TABLE 1, PAGES 87, 88 & 88A.SDR USAASB01169Battery Pack · dischargedBDL - MAINTENANCE FOUND THE L1 AND R1 DOOR EMERGENCY EXIT IDENTIFIER LIGHTS DIM DURING TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB01149Light · inoperativeIAD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR CA010627010Connector · dirty(CAN) WHIE ENROUTE TO YYC, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. NO EVERHEAT LIGHT CAME ON. ENGINE SECURED AND AIRCRAFT LANDED IN YYC WITHOUT INCIDENT. ALL CONNECTOR PLUGS CHECKED AND CLEANED. MEL 26-2 RAISED. DMI 29776. FIRE BOTTLES REPLACED IAW MMSDR USAA010569Bulkhead · crackedCLT - FOUND PRESSURE WEB WITH CRACKS RANGING IN SIZE FROM .375 INCH TO 1.5 INCH, BS 178, WL 199 TO WL 234 LBL 10.5 TO RBL 10.5. DAMAGE REMOVED, REPAIR FILLERS AND DOUBLER INSTALLED PER EO 5300V153, EA 69712, SRM 53-10-11 FIG 1. (M)SDR USAA010570Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCHES AND 1.25 INCHES, BS 178, LEFT AND RIGHT SIDE CHORD, WL 195. DAMAGED SECTIONS CUTOUT, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157 AND SRM 51-10-02. (M)SDR USAA010571Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1.5 INCHES, BS 178, WL 195, LBL 25 AND RBL 25. REMOVED AND REPLACED INTERCOSTAL. (M)SDR USAA010572Bulkhead · crackedCLT - FOUND WEB CRACKED .250 INCH, BS 178 WL 195.7, LBL 23. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER PER EA 69714 AND SRM 53-10-11 FIG 2. (M)SDR USAASB01143Battery Pack · dischargedBWI - THE FORWARD DOOR EMERGENCY EXIT SIGNS AND EXTERIOR SLIDE ESCAPE LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER PACK MODULE. (M)SDR USAA010573Keel · corrodedCLT - FOUND KEEL CHORD OUTBOARD FLANGE WITH 3 INCH AREA OF CORROSION, BS 727A, RBL 7, BELLY AREA. REMOVED DAMAGE, INSTALLED SPLICE REPAIR PER TR 53-10-24, EA 69672, SRM 51-20-1 FIG 10, 53-10-6 FIG 3. (M)SDR USAA010556Shear Tie · corrodedCLT - FOUND FRAME SHEAR TIE CORRODED 5 INCHES BY 1 INCH, BS 986 STRINGER 24R/25R. FABRICATED AND REPLACED SHEAR TIE PER BAC DRAWING 65-46564, SRM 51-10-0 AND 51-30-0. (M)SDR USAA010557Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 712, LBL 24. INSTALLED REPAIR DOUBLER, REPLACEMENT WEB AND 4 VERTICAL STIFFENERS PER EA 69504. (M)SDR USAA010558Floorbeam · crackedCLT - FOUND FLOORBEAM T-CAP CRACKED, BS 520, RBL 25, WL 208. INSTALLED DOUBLER AND PIVOT LINK ASSY PER SB 737-53-1120 AND EA 69537. (M)SDR USAA010559Frame · crackedCLT - FOUND CHORD CRACKED 1 INCH, BS 663, LBL 24, WL 203. INSTALLED REPAIR CHORD PER EA 69538 AND SB 737-53-1184. (M)SDR USAA010560Web · crackedCLT - FOUND PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH TO 1 INCH, BS 178, LBL 12 TO RBL 17, WL 188 TO WL 214. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69493. (M)SDR USAA010561Frame · crackedCLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M)SDR USAA010562Attach Fitting · corrodedCLT - FOUND FUSELAGE ATTACH LUGS CORRODED 3 SQUARE INCHES, VERT FIN, AFT OUTBOARD LEFT AND AFT OUTBOARD RIGHT ATTACH POINTS. CORROSION REMOVED AND LUGS REWORKED PER EA 69591 AND EO 5593G087. (M)SDR USAA010563Beam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M)SDR USAA010564Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M)SDR USAA010565Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M)SDR USAA010566Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M)SDR USAA010552Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M)SDR USAA010553Frame · crackedCLT - FOUND FRAME CRACKED .375 INCH, LATERALLY THROUGH EDGE OF FRAME BS 440, LBL 21. INSTALLED FORMED FRAME REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)SDR USAA010555Doubler · crackedCLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M)SDR CA010626021Pin · bent(CAN) DURING CLIMB FIRE WARNING INDICATION WAS OBSERVED ON NR 2 ENGINE. AIRCRAFT RETURNING WITHOUT INCIDENT. UPPER & LOWER FIRE LOOP WAS REPLACED ALONG WITH FIRE DETECTION UNIT. GROUND CHECKED SERVICEABLE. DURING SUBSEQUENT FLIGHT FIRE WARNING INDICATION WAS OSDR USAA010525Skin · crackedCLT - FOUND FUSELAGE SKIN WITH TWO CRACKS 1 INCH EACH, BS 727 PLUS 1 INCH AT STRINGER 17R AND BS 727A PLUS 6 INCHES AT STRINGER 19R. INSTALLED REPAIR DOUBLER. (M)SDR USAA010524Frame · crackedCLT - FOUND FRAME CRACKED 1.125 INCH, BS 277, STRINGER 16L. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-2, FIG 1. (M)SDR USAA010523Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)SDR USAA010522Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED 1.5 INCH, BS 727, LBL 27, WHEEL WELL COMPRESSION CHORD. INSTALLED REPAIR STRAPS AND DOUBLER ANGLE PER BOEING DRAWING NR 691A0068 AND EA 69571. (M)SDR USAA010521Stringer · crackedCLT - FOUND STRINGER CRACKED .070 INCH, BS 380, STRINGER 2L. REMOVED DAMAGE SECTION, SPLICED IN NEW STRINGER SECTION PER SRM 53-10-3. (M)SDR USAA010518Web · crackedCLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M)SDR USAA010520Pressure Panel · damagedCLT - FOUND UNBEADED PRESSURE WEB APPROX 3 SQUARE FEET, BS 666 WL 55. REINFORCING ANGLES INSTALLED PER SB 737-57-1234 AND EA 69561. (M)SDR USAA010519Frame · crackedCLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 195 LEFT SIDE CHORD. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)SDR USAASB01126Battery · dischargedBWI - THE LEFT AND RIGHT FORWARD DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK. (M)SDR USAA010497Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED 2 INCH BY 3 INCH AREA, BS 468 BL 0. DAMAGED AREA CUTOUT, REPAIR DOUBLER INSTALLED PER SRM 53-30-3. (M)SDR USAA010496Stringer · corrodedCLT - FOUND STRINGER CORRODED 1 INCH BY 10 INCH AREA, BS 1006 TO 1016, S24R. REMOVED DAMAGE, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-2. (M)SDR USAA010493Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED .125 INCH, BS 967, RBL 42. DAMAGE REMOVED, SPLICED IN T-CAP REPLACEMENT PER SRM 53-10-9. (M)SDR USAA010491Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 13 SQUARE INCHES, BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-60-01 REV ''A''. (M)SDR USAA010475Angle · corrodedCLT - FOUND AFT SERVICE DOOR Z-ANGLE CORRODED 40 INCHES BY .5 INCH, BS 947 TO 987, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-01. (M)SDR USAA010474Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY .5 INCH AREA, BS 312, BL 0. DAMAGE REMOVED, SPLICED IN REPAIR ANGLES AND T-CAP SECTION PER TYPICAL REPAIR 53-10-13. (M)SDR USAA010473Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BS 1006, LBL 10. DAMAGE REMOVED, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-10-9 FIG 2. (M)SDR USAA010503Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA010502Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M)
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