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 USAASB01079Battery Pack · dischargedBWI - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M)Mar 16, 2001 · N241US · Boeing 737201 · Emergency LightingSDR USAASB01078Battery Pack · dischargedBDL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS FROM ROWS 10 TO 14 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Mar 15, 2001 · N241US · Boeing 737201 · Emergency LightingSDR USAASB01075Wire · damagedLGA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 7 WAS INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY LIGHT WIRING TO THE SEAT ROW EMERGENCY LIGHT. (M)Mar 8, 2001 · N264AU · Boeing 737201 · Light System WiringSDR USAA010265Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, RBL 5.7. REMOVED CRACKED AREA, INSTALLED DOUBLER. (M)Mar 7, 2001 · N249US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010261Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .125 INCH, BS 178, RBL 5, WL 189, 190 AND 191.5. REMOVED DAMAGE INSTALLED DOUBLER PER EA 69132. (M)Mar 5, 2001 · N249US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010198Skin · crackedBOS - FOUND SKIN CRACKED 1.375 INCH, STATION 807 ABOVE STRINGER 19L. INSTALLED DOUBLER AT STATION 807 STRINGER 19L. (M)Mar 2, 2001 · N257AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010264Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 LBL 7, WL 213.5. REMOVED DAMAGE, INSTALLED DOUBLER. (M)Mar 2, 2001 · N249US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010263Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .25 INCH, STATION 178, RBL 10.5, WL 234. REMOVED DAMAGE, INSTALLED DOUBLER. (M)Mar 2, 2001 · N249US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010188Web · crackedCLT - FOUND DOOR WEB CRACKED .5 INCH, AFT SERVICE DOOR TORQUE BOX WEB BS 947 BELOW STRINGER 11R. INSTALLED DOUBLER PER TR 53-30-07A. (M)Feb 28, 2001 · N249US · Boeing 737201 · Passenger/Crew DoorsSDR USAA010267Skin · crackedTPA - FOUND SKIN CRACKED 2.5 INCHES, STATION 951, STRINGER 20L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)Feb 28, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01068Wire · damagedMCO - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 15 WAS INOPERATIVE. MAINTENANCE CLEARED THE AIRCRAFT TO OPERATE PER MEL PROCEDURES. DURING THE MAINTENANCE OVERNIGHT THE WIRING TO THE EMERGENCY LIGHT WAS REPAIRED. (M)Feb 28, 2001 · N256AU · Boeing 737201 · Light System WiringSDR USAA010266Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, EQUIPMENT COOLING EXHAUST STATION 380 STRINGER 28L. INSTALLED .100 2024 T3 CLAD DOUBLER IAW TYPICAL REPAIR 53-30-04. (M)Feb 26, 2001 · N241US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01061O-Ring · leakingBDL - FLT 2978 - EN ROUTE FROM PVD-BWI, THE NR 1 GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. THE NR 1 GENERATOR DRIVE OIL TEMPERATURE ''IN'' INDICATION WAS OFF SCALE AND NO HIGH OIL TEMPERATURE LIGHT ILLUMINATED. AFTER PLACING APU ON LINE, THE APU LATER Feb 26, 2001 · N257AU · Boeing 737201 · APU Oil SystemSDR USAASB01062Csd · overservicedMCO - FLT 2802 - ON CLIMB-OUT FROM MCO, AT ABOUT 4,000 FEET, THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO FIELD AT MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE NORMALLY.Feb 26, 2001 · N257AU · Boeing 737201 · Alternator-Generator DriveSDR USAASB01055Hydraulic Line · leakingPIT - FLT 2622 - EN ROUTE FROM BWI TO MDW, AT FL280, FLIGHT EXPERIENCED A LOSS OF SYSTEM A HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF HYDRAUIC PRESSURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THEFeb 23, 2001 · N253AU · Boeing 737201 · Hydraulic System, MainSDR USAA010223Frame · crackedCLT - FOUND VERTICAL CHORD CRACKED 1 INCH OUTBOARD RADIUS AND 1.8 INCH INBOARD, BS 178 BULKHEAD, LBL 5-7, WL 184. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO 5300V155. (M)Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, FrameSDR USAA010222Frame · crackedCLT - FOUND CHORD VERTICAL CRACKED .9 INCH IN INBOARD RADIUS, RBL 5-7, WL 184, BS 178 BULKHEAD. INSTALLED VERTICAL CHORD REPAIR PARTS PER EA 68935/EO5300V155. (M)Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, FrameSDR USAA010221Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, 178 BULKHEAD, RBL 26, WL 195. MODIFIED PART INSTALLED PER EA 68934. (M)Feb 20, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 20010426AP004Tie Clip · crackedCLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. REF USAA010224. (M)Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010224Stringer · crackedCLT - FOUND STRINGER AND TIE CLIP CRACKED .250 INCH, BS 520 STRINGER 19L. REMOVED AND REPLACED TIE CLIP AND INSTALLED STRINGER 18 INCH SECTION PER SRM 53-10-03, 51-10-01, 51-10-02. (M)Feb 20, 2001 · N249US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB01051Duct · failedBWI - FLT 2639 - ON CLIMB-OUT FROM BWI, AT FL120, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. CREW REDUCED POWER ON NR 2 ENG TO IDLE AND LIGHT EXTINGUISHED. CREW DECLARED AN EMERG AND RETURNED TO FIELD AT BWI. FLT LANDED W/O FURTHER INCIDENT. PRIOR TO LANDINGFeb 20, 2001 · N248US · Boeing 737201 · Engine Anti-Icing SystemSDR USAA010237Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BS 380 AT E/E EQUIPMENT COOLING DUCT OUTLET. INSTALLED INTERIOR SKIN DOUBLER PER T/R 53-30-04. (M)Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010236Frame · crackedCLT - FOUND FRAME CRACKED 2 INCHES, FS 767 AT STRINGER 13L. INSTALLED REPAIR DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, FrameSDR USAA010235Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FRAME 807 STRINGER 13L. REMOVED DAMAGE AND INSTALLED DOUBLERS PART 1 AND 2 IAW SRM 53-10-4. (M)Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, FrameSDR USAA010234Skin · crackedCLT - FOUND SKIN DOUBLER CRACKED 8 INCHES BY 11 INCHES, 727 PLUS 16 S 27R. INSTALLED DOUBLER PER SRM 53-30-03. (M)Feb 19, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR CA010308012Actuator · leaking(CAN) AT APPROXIMATELY 20 MINUTES OUT, THE A SYSTEM HYDRAULIC LIGHT ILLUMINATED. THE HYDRAULIC FLUID GAUGE WAS CHECKED AND FOUND TO BE EMPTY. THE USE OF ALTERNATE FLAP AND GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT WFeb 19, 2001 · Boeing 737201 · Drag Control ActuatorSDR USAA010199Skin · crackedBOS - FOUND SKIN CRACKED 1.5 INCH, STATION 765, STRINGER 18L. CUT OUT DAMAGE AND INSTALLED 11 INCHES BY 6.75 INCHES SOLID RIVITS DOUBLER PER SRM 53-30-3 FIG 6. (M)Feb 16, 2001 · N255AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010254Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 616 STRINGER 3 LEFT. MODIFIED PART NR INSTALLED. (M)Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010253Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616 STRINGER 1. MODIFIED PART NR INSTALLED. (M)Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010252Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .5 INCH, BS 967 AT STRINGER 7L. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4 FIG 8. (M)Feb 15, 2001 · N249US · Boeing 737201 · Fuselage Main, StructureSDR USAA010247Floorbeam · corrodedCLT - FOUND FLOOR FRAME CORRODED 4 SQUARE INCHES, STATION 987.5 LBL 14, RBL 15, RBL 24. REPLACED T-CAP FROM LEFT AND RIGHT EXTREMITIES PER TYP REP 53-60-01. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Feb 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010246Floorbeam · corrodedCLT - FOUND FLOOR FRAME CORRODED 12 SQUARE INCHES, BS 947.5 LBL 30 - RBL 49. FABRICATED T-CAP AND SPLICE PARTS PER 53-10-9. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Feb 15, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA0102000Skin · crackedBOS - FOUND SKIN CRACKED 1.375 INCH CRACK, BETWEEN STATION 747 AND 767 ABOVE STRINGER 18R. INSTALLED DOUBLER AT STATION 747 AND 767 ON STRINGER 18R AND 19R PER SRM 53-30-3. (M)Feb 14, 2001 · N253AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010255Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 15L BS 520-540. REPLACED STRINGER SECTION IAW SRM 53-10-3. (M)Feb 14, 2001 · N249US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010249Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, STATION 663 RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER DRW 65C37732, EA 68973. (M)Feb 14, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010157Angle · crackedCLT - FOUND CREASEBEAM ANGLE .5 INCH, BS 630, RBL 45. FABRICATED NEW ANGLE PER SRM 51-10-1 AND DWG 65 47973. (M)Feb 13, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010156Crease Beam · crackedCLT - FOUND CREASEBEAM WEB CRACKED 1 INCH, AFT OUTBOARD CORNER AT STATION 638. SPLICED IN NEW SECTION PER SRM 51-10-1 AND 51-40-4. (M)Feb 13, 2001 · N249US · Boeing 737201 · Fuselage Main, StructureSDR USAA010136Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, FS 785 AT STRINGER 19L. INSTALLED DOUBLER PER EA 69066. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010135Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 685 STRINGER 4L. REPLACED TIE CLIP PER EO 5393G227. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010134Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727G, STRINGER 8R. REPLACED TIE CLIP PER EO 5393G227. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010133Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 616, STRINGER 2L. INSTALLED NEW TIE CLIP PE EO 5393G227. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010132Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STATION 616, STRINGER 6L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010155Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, STATION 178, WL 207 AND 195 RIGHT SIDE. SPLICED IN NEW SIDE CORD PER EO 5300V157. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAA010154Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, TWO PLACES, STATION 178, WL 207, AND WL 195, LEFT SIDE. SPLICED IN NEW SIDE CHORD PER EO 5300V157. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAA010152Torque Box · crackedCLT - FOUND TORQUE BOX WEB CRACKED .5 INCH, BS 947 JUST BELOW STRINGER 11L. REMOVED AND REPLACED DOUBLER AND FILLER PER TR 53-30-07 REV A. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, StructureSDR USAA01043Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 707, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-1 AND 51-30-2. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010142Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 706, STRINGER 6L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010141Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 639, STRINGER 3L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010140Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 616, STRINGER 2R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010139Clip · crackedCLT - FOUND CLIP CRACKED .125 INCH, STATION 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous Structure
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