Boeing 737-201

Service difficulty reports · 2,471

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  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 F3LA97134Bulb · failedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROWS 14 A, B, C, 16 A, B, C, 17 A, B, C, AND 18 A, B, C, INOPERATIVE. MAINTENANCE REPLACED BULBS IN AFFECTED ROWS AND SYSTEM CHECKED OKAY. (X)Jun 1, 1997 · N212US · Boeing 737201 · Emergency LightingSDR USAASB97143Battery Pack · dischargedGSO - MAINTENANCE FOUND THE AFT SERVICE DOOR AND THE AFT ENTRY DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)May 29, 1997 · N234US · Boeing 737201 · Emergency LightingSDR USAASB97141Oil Quantity Ind · failedGSO - FL1267 - ON CLIMB-OUT FOR GSO AT APPROXIMATELY 6,000 FEET, THE NR 1 ENGINE OIL QTY GAUGE SLOWLY DROPPED TO ZERO. CREW CALLED GSO TOWER AND DECIDED TO RETURN TO FIELD. AS THE FLIGHT GOT CLOSER TO GSO, THE NR 1 ENGINE OIL QTY GAUGE STARTED TO CLIMB BACK TMay 26, 1997 · N263AU · Boeing 737201 · Engine Oil QuantitySDR USAA970215Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AT LOWER FORWARD CORNER OF DOOR CUTOUT AFT ENTRY DOOR BS 964. INSTALLED EXT SKIN REPAIR AND REPAIRED PER EA 42446. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970214Skin · dentedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENTS 2.5 INCH BY 3 INCH AND 1.5 INCH BY 1.5 INCH STATION 807 BETWEEN STRINGER 19L AND 20L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970213Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FORWARD CARGO FRAME BS 500 BL '0'. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-3 FIG 1. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, FrameSDR USAA970212Beam · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BL '0' BL 660 WL 208 BEAM. INSTALLED REPAIR ANGLES, REPAIRED PER BOEING DRAWING NR 65C34537. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970211Skin · crackedINT - DURING Q-2 CHECK CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 380 BETWEEN STRINGER 28L AND BL '0' SKIN. INSTALLED DOUBLER DOUBLER, REPAIRED PER TR 53-30-04. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970210Stringer · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AFT CARGO BS 907 STRINGER 26R. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 SRM 53-10-4 FIG 10. CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970209Stringer · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 907, STRINGER 24L. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970208Skin · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 4 INCHES APPROX BS 927 BETWEEN STRINGER 24L AND 25L SKIN. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 53-30-3. CORROSION TASK NR 53-208-01, CORROSION LEVEL 2. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970207Frame · corrodedINT - DURING Q2-CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AFT CARGO LOWER LEG OF FRAME BS 767 STRINGER 26R-25R. INSTALLED FRAME REPAIR CONSISTING OF SHEAR TIE, FILLER SUPPORT ANGLE AND RADIUS FILLER, REPAIRED PER SRM 53-10-4 FIG 6. CORROSMay 24, 1997 · N226US · Boeing 737201 · Fuselage Main, FrameSDR USAA970206Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH CRACK FORWARD LOWER CORNER AFT ENTRY DOOR SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER EA 42446. (M)May 24, 1997 · N226US · Boeing 737201 · Passenger/Crew DoorsSDR USAA970205Stringer · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 12 INCHES STATION 962 , STRINGER 27L. INSTALLED DOUBLER (SPLICE), REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)May 24, 1997 · N226US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB97136Lights · malfunctionedDCA - FLT 1727 - FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH, SEVERAL BATTERY PACKS AND CLEANED THE EMERGENCY EXIT SWITCHES. SYSTEMS OPS CHECK GOOD. (M)May 22, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97135O-Ring · leakingMCO - FLT 682 - EN ROUTE TO CLT AT FL270, CAPTAIN REPORTED LOST OIL PRESSURE AND OIL QTY ON THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED. THE NR 1 ENGINE WAS SHUTDOWN AND 35 PSI AND THE FLIGHT DIVERTED MCO. THE FLT LANDED WITHOUT INCIDENT AND TAXIED TO GATE. May 22, 1997 · N252AU · Boeing 737201 · Turbine Engine Oil SystemSDR USAASB97133Battery · dischargedCLT - FLT 7900 - DURING TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, THE LOW LEVEL EMERGENCY EXIT LIGHTS FROM SEAT ROW 7 AND BACK ILLUMINATED. AFTER LANDING, THE AFT MOST LIGHTS WENT OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS AT SEMay 21, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAA970203Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT OUTER AREA OF STRINGER WHERE MATES W/SKIN 15 INCHES LONG BY 1 INCH WIDE, SOME AREAS COMPLETELY THROUGH STRINGER, STATION 360-375 STRINGER 25L. INSTALLED NEW SEGMENT OF STRINGER, REPAIRED PER SRM 53-May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970202Doubler · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND BELL CRANK CUTOUT DOUBLERS CRACKED STATION 677, RBL 25 AND LBL 25 STATION 677, RBL 25 AND LBL 25. INSTALLED NEW REINFORCEMENTS IN AREA, ACCOMPLISHED EO 5791G632, PART 3B. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970201Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 639 STRINGER 16L FRAME. INSTALLED REPAIR PER DRAWING 65C31658. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, FrameSDR USAA970200Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH AND .25 INCH CRACK LOWER HINGE CUT OUT UPPER AND LOWER CORNERS (FWD ENTRY DOOR) SKIN. INSTALLED DOUBLERS, REPAIRED PER TR 52-10-05. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970199Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUTOUT SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42403. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970198Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 919, STRINGER 25L. SPLICED STRINGER, REPAIRED PER SRM 53-10-3. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970197Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970196Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKS 4 INCHES AND 2 INCHES AT STRINGER 18R STATION 727 A PLUS 16 INCHES AND STRINGER 18R STATION 727 A PLUS 3 INCHES SKIN. INSTALLED ONE DOUBLER FOR BOTH CRACKS PER SRM 53-30-03 FIG 6. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970195Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT UPPER CORNER OF CAPTAINS NR 1 WINDOW FRAME FLIGHT COMPARTMENT SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 11. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97131Battery Pack · dischargedCLT - MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATION CHECK GOOD. (M)May 15, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97130Socket · failedCLE - MAINTENANCE FOUND THE AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR AND SOCKET ASSEMBLY DUE TO CORROSION. OPERATIONAL CHECK GOOD. (M)May 14, 1997 · N260AU · Boeing 737201 · Emergency LightingSDR USAASB97129Csd Drain Plug · brokenSAV - FL403 - THE NR 1 ENG CSD LOW PRESS LIGHT BEGAN TO BLANK AND THE FREQ WAS FLUCTUATING ERRATICALLY. ABNORMAL CHECKLIST WAS FOLLOWED, THE NR 1 ENG CSD WAS DISCONNECTED. THE APU WAS ON MEL AND WITH ONLY ONE POWER SOURCE, THE FLT DIVERTED TO SAV. FLT LANDEMay 12, 1997 · N244US · Boeing 737201 · Alternator-Generator DriveSDR USAASB97127Qty Ind · failedCHA - FL1229 - AFTER T/O, LT FUEL QTY IND PEGGED PAST FULL IND. PRESSED TEST BUTTON AND FUEL QTY DROPPED TO 3,000 LBS, THEN FLUCTUATED UP AND DOWN. FLT CONTINUED ON UNTIL EAST OF CHA, WHEN THE RT FUEL QTY IND APPEARED TO FAIL (SHOWED A STEADY AMOUNT WITH NO May 10, 1997 · N262AU · Boeing 737201 · Fuel Quantity IndicatorSDR USAA970190Stub Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 7 INCH CRACK STATION 639 LBL 50 INCH STUB BEAM. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING 65C25211. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970189Stub Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 695 LBL 64 INCH STUB BEAM. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING 65-465-44. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970188Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 1 RIGHT COCKPIT WINDOW FRAME SKIN. FABRICATED DOUBLER AND INSTALLED, REPAIRED PER SRM 53-30-3 FIG 11. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970187Crease Beam · crackINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 637 RBL 69 CREASE BEAM. INSTALLED SPLICE, REPAIRED PER SRM 51-40-4. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970186Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .100 INCH LONG UPPER HINGE CUTOUT, AFT SERVICE DOOR SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970185Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH BY .031 INCH CORROSION STATION 1006 STRINGER 25L. CUT OUT DAMAGED STRINGER, FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-3 FIG 1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970184Skin · dentedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DENT 3.5 INCH BY 1.5 INCH SKIN STATION 380 STRINGER 19R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)May 8, 1997 · N239US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97124Fuel Pump · failedCLT - FL1173, ON CLIMB-OUT AT APPROX 1,200 FT, THE NR 1 ENG LOST THRUST. THE LOW OIL PRESS LIGHT CAME ON WITH NO OTHER INDICATIONS. CAPTAIN PERFORMED SINGLE ENGINE FAILURE CHECKLIST AND SHUTDOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TMay 7, 1997 · N225US · Boeing 737201 · Engine Fuel PumpSDR USAASB97123O-Ring · failedIND - AT FL280 EN ROUTE FROM CLT TO ORD, SYSTEM 'A' HYDRAULICS FAILED. QTY AND PRESSURE WENT TO ZERO. CREW ACCOMPLISHED ABNORMAL PROCEDURES AND DIVERTED TO IND. NO EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATEMay 6, 1997 · N248US · Boeing 737201 · Drag Control ActuatorSDR USAASB97120Heat Manifold · failedBWI - FL250, ON CLIMB-OUT OF BWI, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN BROUGHT POWER BACK TO IDLE AND LGIHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT BWO WITH NR 1 ENGINE AT IDLE. CAPTAIN DID DECLARE AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHMay 2, 1997 · N244US · Boeing 737201 · Fuel HeaterSDR USAASB97118Air Vent · not connectedORF - FL8032, AFTER TAKEOFF, AIRCRAFT DID NOT PRESSURIZE AND APPEARED TO HAVE A LOUD WIND NOISE COMING FROM THE CAPTAINS WINDSHIELD. AS PRECAUTIONARY, THE FLIGHT RETURNED TO FIELD AT ORF. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDEApr 29, 1997 · N249US · Boeing 737201 · Air Distribution SystemSDR USAASB97117Windshield · crackedORF - FL1926, FLIGHT WAS CLIMBING OUT OF PHL THROUGH FL290 WHEN THE CAPTAINS WINDSHIELD BEGAN TO CRACK. CAPTAIN DECIDED TO DIVERT INTO ORF. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIApr 29, 1997 · N249US · Boeing 737201 · Flight Compartment WindowsSDR 97ZZZM673Heat Controller · failedORF - FL1926, FLIGHT WAS CLIMBING OUT OF PHL THROUGH FL290 WHEN THE CAPTAINS WINDSHIELD BEGAN TO CRACK. CAPTAIN DECIDED TO DIVERT INTO ORF. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIApr 29, 1997 · N249US · Boeing 737201 · Windshield/Door Rain/Ice RemovalSDR USAASB97110Battery Pack · dischargedCLE - DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY PER MM. OPERATIONAL CHECK NORMAL. BATTERY PACK - P/N 61-0478-9. Apr 23, 1997 · N253AU · Boeing 737201 · Emergency LightingSDR 97ZZZX2013Power Supply · inoperativeCLE - DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY PER MM. OPERATIONAL CHECK NORMAL. BATTERY PACK - P/N 61-0478-9. Apr 23, 1997 · N253AU · Boeing 737201 · Emergency LightingSDR USAASB97102O-Ring · failedALB - FLT 291 - DESCENDING THROUGH 10,000 FEET AT IDLE POWER, CREW NOTICED THE LOW OIL PRESSURE LIGHT FOR THE NR 1 ENGINE ILLUMINATED. THEY CONFIRMED LOW OIL PRESSURE LIGHT WITH QUANTITY GAUGE AND OIL PRESSURE GAUGE. AT THAT TIME, CREW SHUT DOWN THE NR 1 ENGApr 12, 1997 · N260AU · Boeing 737201 · Turbine Engine Oil SystemSDR USAASB97125Wire · brokenCMH - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 11 INOP. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT SOCKET. OPS CHECK GOOD. (M)Apr 8, 1997 · N242US · Boeing 737201 · Light System WiringSDR USAASB97094Garlock Seal · failedBWI - FLT 1243 - FLIGHT HAD JUST LEVELED OFF AT 28,000 FEET WHEN CREW NOTICED THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE TOWARDS ZERO. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUT-DOWN OCCURRED Apr 4, 1997 · N226US · Boeing 737201 · Turbine Engine Accessory DriveSDR USAASB97089Light · failedPHL - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Mar 23, 1997 · N260AU · Boeing 737201 · Emergency LightingSDR USAA970115Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4.5 INCH CRACK STATION 1156 BETWEEN STATION 2L AND 3L SKIN. INSTALLED DOUBLER, REPAIRED PER SB 737-53-1095 AND EA 42156. (M)Mar 21, 1997 · N249US · Boeing 737201 · Fuselage Main, Plate/Skin
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