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 USAA960279Hinge Fitting · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT WING AT WS 537.8 LOWER FLANGE OF AILERON HINGE FITTING. FABRICATED AND INSTALLED FLANGE REPAIR PER EA 40893. (M)Feb 24, 1996 · N243US · Boeing 737201 · Wing, Control Surface Attach FittingsSDR USAA960278Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED NUT PLATE HOLES AT FLOOR BEAM STATION 460-500 ABOVE STRINGER 27 R. REPLACED ANGLE, REPAIRED PER SRM 53-10-5 FIG 6. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960277Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 4 STOP CUTOUT (AFT FRAME) AT FORWARD CABIN SERVICE DOOR. STOP DRILLED CRACK, REPAIRED AND INSTALLED. 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 USAA960276Clip · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA AT STRINGER TIE CLIP BS 540 STRINGER 26 L. REPLACED STRINGER TIE CLIP, REPAIRED PER SRM 53-10-1. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960275Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION INTERCOSTAL, STATION 270 TO STATION 294 LBL 10 INCHES. INSTALLED NEW PREFAB INTERCOSTAL, REPAIRED PER BOEING DRAWING 65-45634. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960274Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN 1156 BULKHEAD STRINGER 2 L AND STRINGER 3 L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960273Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK ON SKIN BS 380 BETWEEN STRINGER 28 L AND BL 0. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04 AND EA 25454. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960134Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 639 STUB BEAM WEB LBL 48 WL 206.5. INSTALLED WEB, REPAIRED PER BOEING DRAWING 65C25211. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960116Frame · crackedINT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK ON CIRCUMFERENTIAL FRAME WEB STATION 328 4 INCHES BELOW STRINGER 20R. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA960106Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN CIRCUMFERENTIAL FRAME STATION 360 4 INCHES BELOW STRINGER 19 R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)Feb 24, 1996 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAASB96032Light · inoperativeFLT 2674 - LGA - EMERGENCY EXIT LIGHT AT FORWARD SERVICE DOOR INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK OVER FORWARD GALLEY SERVICE DOOR. EMERGENCY LIGHTS OPS CHECK GOOD. (M)Feb 20, 1996 · N239US · Boeing 737201 · Emergency LightingSDR F3LA96008Warning Horn · soundedFLT NR 546 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE LANDING GEAR WARNING HORN SOUNDED WITH THROTTLES RETARDED TO IDLE AND FLAPS UP. WARNING HORN DID NOT SOUND AT FLAP SETTINGS 1 OR 5 WITH THROTTLES RETARDED TO IDLE. LANDING GEAR WAS UP IN BOTH CASES. Feb 14, 1996 · N217US · Boeing 737201 · Landing Gear Position and WarningSDR USAASB96030Overheat Det · malfunctionedFLT 771 - PIT - DIVERTED TO PIT DUE TO RIGHT WING AND BODY OVERHEAT. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. WENT OUT SHORTLY AFTER RIGHT ENGINE BLEED VALVE WAS CLOSED ACCORDING TO FLIGHT MANUAL PROCEDURE. MAINTENANCE CHECKED WIRING RESISTANCEFeb 12, 1996 · N262AU · Boeing 737201 · Overheat DetectionSDR USAA960191Skin · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SKIN BS 347 AT STRINGER 17L. INSTALLED DOUBLERS. REPAIRED PER EO 5391G-694. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960190Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK TIE CLIP, STRINGER 3R, BS 727. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960189Tie Clip · crackedINT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS BS 767 AT STRINGER 5L AND STRINGER 10L, STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960188Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 685 STRINGER 3 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960187Tie Clip · crackedINT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS, BS 727B AT STRINGER 2L AND STRINGER 7L, STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960186Tie Clip · crackedINT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 10 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-3535214. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960185Tie Clip · crackedINT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 6 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960184Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 747 STRINGER 5 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960183Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 578 AT STRINGER 3 LEFT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960182Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN 2 STRINGER TIE CLIPS BS 616 AT STRINGER 2L AND STRINGER 4L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960181Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 639 STRINGERS 4L, 6L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960180Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 685, STRINGER 2L AND STRINGER 5L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960179Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 706, STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960178Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 727 A STRINGERS 3L, STRINGER 4L, STRINGER 5L. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960177Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 7L AND STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960176Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10L. REPAIRED PER EO 5353G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960175Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 5 LEFT. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960173Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 578 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960172Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 639 STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960171Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP BS 727A STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960170Tie Clip · crackedINT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 727 B S-1, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M)Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 96ZZZX570Control Module · failedMSP - FLT 417 - UPON ARRIVAL, FLIGHT CREW REPORTED AN ACRID ODOR AND SMOKE IN THE CABIN. ODOR AND SMOKE CLEARED WHEN LEFT PACK WAS TURNED OFF. MAINTENANCE REPLACED THE CABIN TEMPERATURE MODULE AND SYSTEM CHECKED OKAY.Jan 29, 1996 · N212US · Boeing 737201 · Cabin Temperature ControllerSDR 96ZZZX569Valve · malfunctionedDEN - FLT 233 - UPON ARRIVAL, FLIGHT CREW REPORTED THE LEFT PACK TEMPERATURE CONTROL WENT TO FULL HOT IN AUTOMATIC MODE CAUSING SMOKE IN THE CABIN. SMOKE DISSIPATED WHEN CONTROL WAS REPOSITIONED TO MANUAL. REPLACED THE LEFT PACK VALVE, AND SYSTEM CHECKED OKAJan 28, 1996 · N212US · Boeing 737201 · Cabin Temperature Control SystemSDR USAA960161Shear Beam · crackedINT - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AT SHEAR BEAM STRINGER 18A, STATION 706. INSTALLED REPAIR ANGLES AND DOUBLERS. REPAIRED PER EO 5393G256 PART 3 SECTION IV. (M)Jan 27, 1996 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960160Skin · crackedROA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND HINGE CUTOUT AFT ENTRY DOOR SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-03 FIG 34. (M)Jan 27, 1996 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960159Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 17 INCH STR 27L CORRODED AT STATION 947 STRINGER 27L. REPAIRED STRINGER STR SPLICE, REPAIRED PER SRM 53-10-3, PG 3. (M)Jan 27, 1996 · N223US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB96020Gasper Fan · failedCHS - EN ROUTE MCO-IAD - CREW NOTED ELECTRICAL IN SMELL IN CABIN. FLIGHT DIVERTED TO CHS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE GASPER FAN. (M)Jan 26, 1996 · N224US · Boeing 737201 · Air Distribution FanSDR USAASB96018Aux Power Unit · failedFLT NR 1184 - BWI - ON FINAL APPROACH APU FIRE WARNING MOMENTARILY WENT OFF. FIRED FIRE BOTTLE. MAINTENANCE REPLACED THE APU. (M)Jan 22, 1996 · N234US · Boeing 737201 · Airborne Auxiliary Power Unit (APU) SystemSDR USAASB96012Pressurization · lostFLT NR 818 - PIT - FLIGHT DIVERTED DUE TO LOSS OF PRESSURIZATION. (M)Jan 19, 1996 · N242US · Boeing 737201 · Cabin Pressure Control SystemSDR USAA960097Stringer · corrosionINT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND TWO LOCATIONS 2 INCHES BY 4 INCHES CORRODED AND 2 INCHES BY 8 INCHES CORRODED AT STRINGER 27L, BS 927 TO 967. INSTALLED STRINGER AND DOUBLERS. REPAIRED PER SRM 53-10-3, FIG 1. (M)Jan 17, 1996 · N249US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB96005Accy Unit · failedFLT NR 1530 - PHL - GREEN 'NOSE GREEN' REMAINED ON ENTIRE LIGHT. RED 'NOSE GEAR' LIGHT NEVER CAME ON IN FLIGHT. FLEW BY TOWER. MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT. ALL INDICATIONS NORMAL. (M)Jan 9, 1996 · N257AU · Boeing 737201 · Landing Gear Position and WarningSDR USAA960012Skin · dentedCLT - INSPECTION VISUALLY FOUND A DENT 8 INCHES BY 4 INCHES IMPACT DAMAGE LOCATED AT BS 480 BETWEEN STRINGER 25R AND STRINGER 26R OF FUSELAGE SKIN. INSTALLED DOUBLER PER USA EA NR 40585. (M)Jan 8, 1996 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960014Shear Beam · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM WEB AT BS 706. INSTALLED DOUBLER. REPAIRED PER EO 5393G259 REV 'A' 11/01/95. (M)Jan 4, 1996 · N228US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960013Shear Beam · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND ONE .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM AT BS 727. INSTALLED DOUBLER. REPAIRED PER EO 5393G256 REV 'A' 11/01/95. (M)Jan 4, 1996 · N228US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960195Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 27L, BS 786.5 TO BS 1016. INSTALLED STRINGER SPLICES, REPAIRED PER SRM 53-10-3. (M)Jan 3, 1996 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951428Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SHEET METAL AT LOWER CORNER MED. INSTALLED INTERIM REPAIR PER EA 31854 AND TBC. REPAIRED PER EA 31854SB 737-53-1083. (M)Dec 30, 1995 · N237US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB95032Retract Mech · malfunctionedFLT NR 1177 - BWI - RETURN TO FIELD, UNABLE TO RETRACT LANDING GEAR. GEAR HANDLE WOULD NOT GO TO UP, DID NOT ATTEMPT TO OVERRIDE. (M)Dec 25, 1995 · N243US · Boeing 737201 · Landing Gear Retraction/Extension System
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