Boeing 737-201

Service difficulty reports · 2,471

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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"

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SDR USAA960404Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CORROSION ON STRINGER, FORWARD OF AFT PRESSURE BULKHEAD STRINGER 26R BS 1016. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)Apr 25, 1996 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960403Skin · crackedGSO - DURING 'WALK-AROUND', VISUAL INSPECTION FOUND 1.2 INCH CRACK IN FUSELAGE SKIN BS 767 AT STR 18 RIGHT. INSTALLED DOUBLER, REPAIRED SRM 53-30-3, FIGURE 6. (X)Apr 23, 1996 · N247US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960382Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 69 INCH CORROSION STRINGER 27L, BS 947 TO 1016. INSTALLED STRINGER/DOUBLERS. REPAIRED PER SRM 53-10-3, DETAIL VI. (M)Apr 13, 1996 · N251AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960394Bulkhead · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK 1156 BULKHEAD. STOP DRILLED BOTH ENDS OF CRACK, MANUFACTURED, HEAT TREATED, AND INSTALLED REPAIR. REPAIRED PER EO 5391G3569. (X)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960393Bulkhead Ftg · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 1156 OUTBOARD OF LEFT OUTBOARD PIVOT FITTING BULKHEAD. INSTALLED DOUBLER, REPAIRED PER EO 5391G569. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960392Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 3 INCH CORROSION BS 1006 TO BS 996 STRINGER 26L. INSTALLED REPLACEMENT STRINGER SECTION, REPAIRED PER SRM 53-10-3. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960391Seat Track · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION SEAT TRACK BS 344 TO BS 349 LBL 22. CUT SEAT TRACK AND SPLICED IN NEW, REPAIRED PER SRM 53-10-5. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960381Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT WEB, BS 350 STRINGER 16L. FABRICATED AND INSTALLED REPLACEMENT WEB. REPAIRED PER BOEING DRAWING 65-17685. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960380Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 294 AND STRINGER 7 LEFT. REMOVED CRACK SECTION OF STRINGER WEB, FABRICATED NEW SECTION AND INSTALLED PER SRM. REPAIRED PER BOEING DRAWING 65-17684 AND SRM 53-10-1 AND 51-30-2 PAGE 5. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960379Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 350 AT STRINGER 17L FRAME. REMOVED DAMAGED AREA FABRICATED REPAIR AND REPAIRED PER SRM 20-30-06 SRM 51-40-4. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, FrameSDR USAA960378Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK EXTERIOR SKIN AND BEAR STRAP BS 328 WL 210 RIGHT SIDE LOWER AFT CORNER OF DOOR CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 26. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960377Strigner · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK WEB OF BUILD UP STRINGER BS 294, STRINGER 7L. FABRICATED AND INSTALLED WEB PER BAC PRINT NR 65-27684 SRM 51-30-2, PAGE 5 AND SRM 53-10-1 NOTED. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960376Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 CRACK STRINGER TIE CLIP STATION 360, STRINGER 4L. FABRICATED AND INSTALLED NEW TIE CLIP, REPAIRED PER SRM 57-10-1. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960375Stab Strap · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (BOTTOM OF FLOOR BEAM) BS 312, RBL 45. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-9. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960374Stab Strap · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (FLOOR BEAM BOTTOM) BS 344, RBL 32. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-9. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960373Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK DOOR FRAME SKIN BS 349, STRINGER 15L. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960372Angle · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TWO FASTENERS AT BS 727, STRINGER 18 IN FRAME CHORD ANGLE. REPLACED SECTION OF CHORD ANGLE, REPAIRED PER EO 5394G068. (M)Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960371Angle · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK FRAME CHORD ANGLE STATION FRAME 727, BETWEEN STRINGER 16R AND STRINGER 17R. REMOVED DAMAGED AREA MANUFACTURED HEAT TREATED AND INSTALLED REPAIR. REPAIRED PER SRM 51-40-4 FIG 1 SRM 20-30-06. (Apr 12, 1996 · N260AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 97ZZZX264Bearing · failedABQ - FLT 322 - BLOCK TURN BACK. CREW REPORTED APPARENT RT MLG DAMAGE. MAINT FOUND THE NR 4 MAIN WHEEL, BRAKE AND AXLE ASSEMBLY DAMAGED. REPLACED THE LOWER STRUT ASSEMBLY, THE NR 4 BRAKE ASSEMBLY, THE NR 3 AND NR 4 TIRE ASSEMBLIES, WHEEL BEARING, WHEEL BEARMar 29, 1996 · N214AU · Boeing 737201 · Wheel/Ski/FloatSDR 96ZZZX1691Landing Gear · damagedABQ - BLOCK TURN-BACK. FLIGHT CREW REPORTED APPARENT RT MLG DAMAGE. MAINTENANCE FOUND NR 4 MAIN WHEEL, BRAKE, AND AXLE ASSYS DAMAGED. REPLACED THE LOWER STRUT ASSY, NR 4 BRAKE ASSY, NR 3 AND NR 4 TIRE ASSYS, WHEEL BEARING, WHEEL BEARING THRUST WASHER AND NUMar 29, 1996 · N214AU · Boeing 737201 · Main Landing GearSDR USAASB96057Flap Indicator · failedCLT - FLT 1632 - AFTER TAKEOFF, CREW RECEIVED FLAP ASYMMETRY LIGHT UPON RETRACTION OF FLAPS. NO UNCOMMANDED ROLL WAS EXPERIENCED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP INDICATOR. (M)Mar 28, 1996 · N265AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAA960334Stringer · corrosionROA - DURING CX-4 CHECK VISUAL INSPECTION FOUND 2 INCH BY 20 INCH CORROSION STRINGER 27 LEFT FROM BS 947 TO BS 967 DUE TO LAV SPILLS. REMOVED DAMAGED SECTION OF STRINGER. FABRICATED NEW STRINGER, DOUBLERS, SPLICES AND SHIMMS, INSTALLED SAME. REPAIRED PER SRMar 24, 1996 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960369Stringer · crackedINT - DURING 'DROP-IN' CHECK VISUAL PCI INSPECTION, FOUND 2.2 INCH CRACK, STATION 706 STRINGER 18A RIGHT. INSTALLED REPAIR, REPAIRED PER EA 41018. (M)Mar 22, 1996 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960333Skin · crackedROA - DURING 'CX-4' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AND BEAR STRAP FORWARD SERVICE DOOR CUT OUT (LOWER AFT CORNER) STA 328. REPAIRED DOUBLER, PN 65C27287-13, REPAIR DOCUMENT T.R. 53-10-19, REV A. (X)Mar 21, 1996 · N256AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96050Connector · deformedCLT - FLT 1850 - AFTER TAKEOFF FROM CLT, CREW RECEIVED NR 1 FUEL HEAT LIGHT AND NR 1 OIL TEMPERATURE ROSE INTO THE YELLOW ARC. CREW REDUCED POWER TO ENGINE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND PIN IN FUEL HEAT VALVEMar 20, 1996 · N229US · Boeing 737201 · Fuel HeaterSDR USAASB96049Ac Generator · loose wireCMH - FL 868 - AFTER DEPARTURE FROM CMH, NR 2 AND NR 3 TRANSFORMER RECEIVER UNITS FAILED. FLIGHT RETURNED TO CMH AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE ENGINE GENERATOR FEED HARNESS WIRE. WIRE 'S' WAS LOOSE AT THE NR 2 GENERATOR. SEMar 20, 1996 · N244US · Boeing 737201 · AC Generation SystemSDR USAASB96048Engine · failedGSO - FL 8028 - AT APPROXIMATELY 600 FEET AGL AFTER TAKEOFF FROM GSO, THE LEFT ENGINE EXPLODED. TOWER ADVISED CREW THAT ENGINE WAS TRAILING SMOKE AND FIRE. FLIGHT RETURNED TO GSO AND GROUND EMERGENCY CREWS EXTINGUISHED THE ENGINE FIRE. NO FIRE WARNINGS RECEMar 19, 1996 · N224US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA960322Skin · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK SKIN BS 970 STRINGER 21L. DOUBLER INSTALLED PER SRM 53-30-3, REPAIRED PER SRM 53-30-3. (M)Mar 18, 1996 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960321Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER APPROXIMATELY 10 INCHES BY .5 INCH STRINGER 29L STATION 947 TO 957. REPLACED APPROXIMATELY 22.5 INCHES OF STRINGER. REPAIRED PER SRM 53-10-3. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960320Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 767 STRINGER 19 RT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-3. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960319Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 767 STRINGER 19 R FUSELAGE SKIN. INSTALLED REPAIR, REPAIRED PER SRM 53-30-3. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960318Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 WL 210 AT SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960317Angle · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK STATION 727 UPPER COMPRESSION CHORD ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-03. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960316Bulkhead Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960315Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, 2 INCH CRACK, 1 INCH CRACK AND .5 INCH CRACK AT 178 BULKHEAD WEB AT LOWER LEFT RADAR DISH MOUNT. INSTALLED DOUBLER REPAIR, REPAIRED PER TR 53-10-11. (M)Mar 16, 1996 · N263AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960311Stringer · corrosionROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION S-27L BS 980 TO 992 STRINGER. REMOVED DAMAGED STRINGER, INSTALLED NEW STRINGER AND STRINGER SPLICE. REPAIRED PER SRM 53-10-3. (M)Mar 14, 1996 · N248US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960310Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK FUSELAGE SKIN STRINGER 18L BS 767. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-01. (M)Mar 14, 1996 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96046Light · failedFLT NR 492 - PHL - FOUND OVERWING EXIT LIGHT INOP AT LEFT AISLE SEAT EXIT. MAINTENANCE REPLACED LIGHT ASSEMBLY. (M)Mar 11, 1996 · N233US · Boeing 737201 · Emergency LightingSDR USAA960307Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK SKIN, STRINGER 19 LEFT BS 807. INSTALLED DOUBLER, REPAIRED EPR SRM 53-30-3. (M)Mar 11, 1996 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96044Connectors · disconnectedFLT NR 770 - ROA - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE INDICATED CLOSED IN AUTO, STANDBY, AND MANUAL. RETURNED TO FIELD. MAINTENANCE FOUND AC AND DC CANNON PLUGS DISCONNECTED FROM THE OUTFLOW VALVE. SECURED PLUGS, OPS CHECK NORMAL.Mar 8, 1996 · N254AU · Boeing 737201 · Cabin Pressure Control SystemSDR USAASB96043Connector · failedFLT NR 311 - PHL - DURING TAKEOFF ROLL, LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO FIELD. REPLACED CONNECTOR D886. OPS CHECKS SATISFACTORY. (M)Mar 7, 1996 · N251AU · Boeing 737201 · Overheat DetectionSDR USAASB96042Csd · overservicedFLT NR 2278 - LGA - AT FL 150 LOST RIGHT CSD. THE FLIGHT RETURNED TO FIELD AT LGA. THE APU WAS ON MEL. NR 2 CSD DISCONNECTED FOR HIGH OIL PRESSURE. MAINTENANCE FOUND NR 2 CSD OVER SERVICED WITH OIL. DRAINED OIL LEVEL TO NORMAL. REMOVED AND REPLACED CSD FMar 7, 1996 · N256AU · Boeing 737201 · Alternator-Generator DriveSDR 96ZZZX1461Corner · crackedDEN - DURING AN A-3 CHECK, MAINTENANCE REPORTED A CRACK IN THE FORWARD SERVICE DOOR (R-1). CRACK WAS APPROXIMATELY 1.25 INCHES IN LENGTH AND WAS LOCATED IN THE LOWER FORWARD CORNER. REPAIRED CRACK PER SB 737-52-1070.Mar 6, 1996 · N205AU · Boeing 737201 · Service DoorsSDR USAASB96034Windshield · delaminatedFLT NR 1129 - CRW - AFTER DEPARTING PIT AND CLIMBING TO FLT LEVEL 350, THE FIRST OFFICERS WINDSHIELD BEGAN TO BUBBLE/DELAMINATE. CAPTAIN DECIDED TO DIVERT TO CRW BECAUSE HE COULD NOT TELL IF ONLY THE OUTER PANE WAS INVOLVED. MAINTENANCE REPLACED FIRST OFFICEFeb 24, 1996 · N247US · Boeing 737201 · Flight Compartment WindowsSDR USAA960289Chord · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION Z-ANGLE STATION 270 AT BL 0. REMOVED CORROSION AND INSTALLED DOUBLER, REPAIRED PER TR 53-20-04. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960287Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 328 AT NR 3 STOP FOR FORWARD CABIN SERVICE DOOR FRAME. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3 PAGE 1. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA960283Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727 B 2 INCH AND STRINGER 17. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960282Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 3 STOP CUT OUT (AFT FRAME) AT FORWARD CABIN SERVICE DOOR. STOP DRILLED CRACK, REPAIRED PER SRM 52-00-2 PAGE 4, FIG 1 AND SRM 51-40-3 PAGE 1. (M)Feb 24, 1996 · N243US · Boeing 737201 · Service DoorsSDR USAA960281Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 20 INCH CORRODED AREA RIGHT Z-ANGLE AT AFT SERVICE DOOR STATION 940 TO STATION 1010. REMOVED CORROSION ON ALODINE AND PRIMED. COMPLETED REPAIR PER SRM 51-10-6. LEVEL 1 CORROSION. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960280Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK FUSELAGE BULKHEAD STATION 178, WL 200, RBL 6 INCHES. INSTALLED REPAIRED DOUBLER, REPAIRED PER TR 53-10-11. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
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