Boeing 737-201

Service difficulty reports · 2,471

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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.

SDR USAASB00169Connector · damagedIAD - FLT 797 - ON APPROACH TO IAD, THE FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES. CRWE COMPLETED CHECK FOR FLAPS AND FIRST OFFICER WENT BACK INTO CABIN FOR VISUAL CHECK. INDICATOR REMAINED AT 10 DEGREES REGARDLESS OF FLAP HANDLE POSITION. FLIGHT LANDED WITHJun 17, 2000 · N240AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAA000854Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 12 INCHES BY 1 INCH, 3 AREAS AT STATION 344, LBL 8 THROUGH LBL 18. REPAIRED T-CAP PER TR 53-10-13. CORROSION LEVEL 2. (M)Jun 15, 2000 · N244US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000852Frame · corrodedCLT - FOUND FRAME CORRODED 2.5 INCHES, BS 967, STRINGER 26R AT SKIN ATTACH POINT. INSTALLED DOUBLER FRAME REPAIR PER SRM 53-10-4. CORROSION LEVEL 2, C53-208-01. (M)Jun 15, 2000 · N244US · Boeing 737201 · Fuselage Main, FrameSDR USAA000851Skin · crackedTPA - FOUND FUSELAGE SKIN CRACKED 3.5 INCHES, LT FUSELAGE SKIN STATION 727A PLUS 13 JUST BELOW STRINGER 17. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 1. (M)Jun 15, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000836Web · crackedCLT - FOUND WEB/STIFFENER CRACKED 6 INCHES, STATION 727, LBL 13 BETWEEN VERT SUPPORT BEAMS. REPLACED PART PER SRM 51-10-1. (M)Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000837Angle · crackedCLT - FOUND ANGLE CRACKED 4 INCHES, STATION 727B LBL 40. REPLACED PER SRM 51-10-1. (M)Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000839Stringer · crackedCLT - FOUND SEVERAL CRACKS .125 INCH OR LESS, INSIDE CHANNEL STRINGER 15L, BETWEEN STATION 520 AND 540. INSTALLED STRINGER REPAIR SECTION PER SRM 53-10-3. (M)Jun 13, 2000 · N244US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000833Skin · crackedTPA - FOUND DOOR EXT SKIN CRACKED 1.75 INCH, AFT ENTRY DOOR FWD LOWER CORNER. INSTALLED DOUBLER PER SRM 52-10-1. (M)Jun 13, 2000 · N228US · Boeing 737201 · Passenger/Crew DoorsSDR USAA000813Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, STRINGER 5R. REMOVED AND REPLACED PER SRM 51-10-1. (M)Jun 12, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB00163Connector · looseCLT - FLT 2673 - EN ROUTE FROM BOS TO TPA, THE APU EGT GAUGE WENT TO ZERO DURING FLIGHT. THE APU WAS IN USE AS THE NR 1 GENERATOR WAS ON MEL. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A LOOSE CJun 10, 2000 · N261AU · Boeing 737201 · APU Indicating SystemSDR USAASB00161Generator · failedORF - FLT 1297 - A FEW MINUTES AFTER TAKEOFF FROM ORF, THE FILGHT LOST THE NR 2 GENERATOR WHICH CAUSED THE GASPER FAN AND NR 2 AND NR 3 TRANSFORMER RECTIFIER CIRCUIT BREAKERS TO POP. CREW TRIED TO RESET CIRCUIT BREAKERS BUT THEY WOULD NOT RESET. THE GENERATOJun 9, 2000 · N263AU · Boeing 737201 · AC Generator-AlternatorSDR USAA000808Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787 STRINGER 7R. REPLACED TIE CLIP PER SRM 51-10-1. (M)Jun 8, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000804Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH AND 2 INCHES, FLOOR SUPPORT BETWEEN STATION 380 TO 400 BL 0. REPAIRED PER SRM 51-10-01. (M)Jun 8, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000797Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 767, STRINGER 11R. FABRICATED NEW CLIP PER SRM 51-10-1 AND DWG 6945156. (M)Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000798Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 663, STRINGER 10L. REPAIRED PER EO 5393G227. (M)Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000799Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. (M)Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000800Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 706, STRINGER 3R. REPAIRED PER EO 5393G227. (M)Jun 5, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000802Skin · crackedTPA - FOUND SKIN CRACKED 2.125 INCH, STATION 747, BELOW STRINGER 17 LT. REMOVED AND REPLACED PER SRM 53-30-3 FIG 1. (M)Jun 5, 2000 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000801Skin · crackedTPA - FOUND SKIN CRACKED .25 INCH, STATION 920 PLUS 1.5 JUST ABOVE STRINGER 22L AFT FUSE. INSTALLED DOUBLER PER 53-30-3 PAGES 2C, 2D, 2E. (M)Jun 5, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00157Controller · failedMKE - FLT 891 - ON CLIMB-OUT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CAPT TOOK OVER FOR THE FIRST OFFICER, WHO WAS FLYING THE A/C, AND THE FIRST OFFICER WENT THROUGH THE QUICK REFERENCE HANDBOOK PROCEDURES. SWITCHED TO STANDBY SYSTEM AND CABIN WENT Jun 5, 2000 · N223US · Boeing 737201 · Cabin Pressure ControllerSDR USAA000775Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 685, STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000776Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000777Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 3R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000778Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 5R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000779Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 7R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Jun 2, 2000 · N244US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000774Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCHES, STATION 767, STRINGER 19L. PREVIOUS REPAIR TOO CLOSE TO DAMAGE. REMOVED IT AND INSTALLED LARGE REPAIR PER SRM 53-30-3 FIG 6. (M)May 29, 2000 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000736Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 30 INCHES, STATION 328, LBL 28, AND RBL 20 - RBL 50. T-CAP REPLACEMENT PER SRM 53-10-2. (M)May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000735Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED, 1 INCH BY 8 INCH, BS 259 FLOORBEAM. INSTALLED DOUBLER AND NEW T-CAP PER TR 53-10-16 AND EA 67170. CORROSION LEVEL 2. (M)May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000726Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344 UPPER CHORD LBL 15 TO LBL 50. REPAIRED T-CAP PER TR 53-10-13. (M)May 23, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000725Fitting · crackedCLT - FOUND .5 INCH CRACK IN FITTING, OUTBOARD SUPPORT FITTING MLG BEAM AT CUTOUT, REMOVED AND REPLACED. (M)May 23, 2000 · N246US · Boeing 737201 · Main Landing Gear Attach SectionSDR USAASB00148Battery · dischargedCLT - FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 1 THROUGH 6. MAINTENANCE REPLACED THE BATTERY PACK. (M)May 19, 2000 · N233US · Boeing 737201 · Emergency LightingSDR USAASB00144Connector · dirtyCLT - WHILE A/C WAS ON THE GROUND, PILOT REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED MOMENTARILY AND EXTINGUISHED ON THEIR OWN. HOWEVER, DURING FLT, THE EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH UNLESS LIGHT SWITCH WAS TURNED OFF. MX CYCLMay 17, 2000 · N228US · Boeing 737201 · Emergency LightingSDR USAA000715Fitting · crackedCLT - Q-1, EXPANSION BEAM FITTING CRACKED 1.5 INCHES, BS 520, RBL 25. INSTALLED DOUBLER AND NEW CHANNEL PER EA 67143. (X)May 16, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000711Beam · crackedCLT - Q-1, BEAM WEB HAD 2 EACH .75 INCH CRACKS, BL ZERO, STA 706 TO STA 713, WL 203 BEAM WEB. INSTALLED DOUBLER PER EA 67224. (X)May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000710Fitting · crackedCLT - Q-1, EXPANSION BEAM FITTING HAD .50 INCH CRACK, STA 520, LBL 25 EXPANSION BEAM FITTING . INSTALLED DOUBLER AND REPAIR ANGLES PER EA 67143. (X)May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000704Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 3 INCHES BY 15 INCHES, BS 986.5 LBL 14 TO RBL 16. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000694Beltframe · corrodedCLT - BELT FRAME HAD LEVEL 2 CORROSION, .250 INCH BY .250 INCH, BS 727B, RBL 04. INSTALLED DOUBLER PER SRM 53-10-4. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000692Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 1 INCH, BS 986.5 LBL 43. INSTALLED T-CAP PER TR 53-60-01. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000690Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 6 INCH, AT BS 986.5, RBL 27, RBL 33. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000688Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 40 TO RBL 42. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000687Skin · crackedCLT - SKIN CRACKED 2.7 INCHES, STR 19L, STA 726 - STA 765, STR 18L 765-780. REPAIRED FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 17. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000686Floorbeam · crackedCLT - FLOORBEAM CRACKED .50 INCH, UPPER FLANGE STA 520, LBL 45. INSTALLED DOUBLER AND PIVOT LINK PER EA 67143. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000685Attach Angle · crackedCLT - ATTACH ANGLE CRACKED 1.50 INCHES, AT FRAME TO STRINGER ATTACH ANGLE STA 360, STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Attach FittingsSDR USAA000684Frame · crackedCLT - FRAME HAD A 4 INCH CRACK AT STA 360, JUST ABOVE STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, FrameSDR USAA000683Floorbeam · corrodedCLT- FLOORBEAM HAD LEVEL 1 CORROSION, .250 INCH BY .250 INCH, BS 312, LBL 08 TO RBL 08. INSTALLED NEW T-CAP PER TR 53-10-13. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000682Floorbeam · corrodedCLT- FLOORBEAM HAS LEVEL 1 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 37 TO RBL 45. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000681Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BL 1006, LBL 19. REPAIRED ANGLE, INSTALLED PER EA67218 AND SRM 51-10-6. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000680Skin · crackedCLT - SKIN CRACKED 3.125 INCHES, LT FUSELAGE EXT SKIN BETWEEN BS 770 AND BS 773, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6. (X)May 10, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000679Angle · crackedCLT - WEB AND ANGLE HAD 6 EACH CRACKS, 4 EACH AT .50 INCH AND 2 EACH AT .1250 INCH, BL ZERO FROM BS 927 TO BS 947. FABRICATED AND INSTALLED NEW ANGLE PER DWG 6936656. (X)May 9, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000678Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 18. REPLACED T-CAP PER SRM 53-10-2. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor Beam
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