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 97ZZZM223Anti-Ice Tube · failedTPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTTLE AND THE LIGHT ILLUMINATED AGAIN. CAPT DECIDED TO RETURN TO FIELD AT TPA. NO EMERGENCY WAS DECLJan 15, 1997 · N228US · Boeing 737201 · Engine Anti-Icing SystemSDR 97ZZZM213Power Supply · inoperativeCLE - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. REFERENCE USAASB97014.Jan 15, 1997 · N255AU · Boeing 737201 · Emergency LightingSDR F3LA97012Web · corrodedPAE - FOUND CORROSION IN NOSE WHEEL WELL UPPER HORIZONTAL WEB AROUND RT ACCESS PANEL CUTOUT BS 236 TO 252, LBL 2 TO 16, WL 190. FOUND CORROSION ON NOSE WHEEL WELL UPPER HORIZ WEB AND STIFFENERS TO BE OUT OF LIMITS, FABRICATED DOUBLERS FROM .080 7075 T6. INSTJan 11, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA97011Doubler · corrodedPAE - FOUND CORROSION ON OUTFLOW VALVE INTERNAL DOUBLER BS 983 RBL 20 WL 183. FOUND DOUBLER TO BE OUT OF LIMITS. REMOVED OUTFLOW VALVE AND DOUBLER, FABRICATED NEW DOUBLER, BACK DRILLED HOLES, DEBURRED, ALODINED, PRIMED AND INSTALLED. REINSTALLED OUT FLOW VAJan 10, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB97032Battery Pack · dischargedCMH - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M571. OPS CHECK GOOD. (M)Jan 9, 1997 · N232US · Boeing 737201 · Emergency LightingSDR USAA970012Skin · crackedROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 3 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. REMOVE CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Jan 9, 1997 · N243US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970011Stringer · corrosionROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BS 965 TO 969. REMOVED CORROSION AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. (M)Jan 9, 1997 · N243US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970008Bulkhead · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACKED PRESSURE BULKHEAD STATION 178 WL 202, RBL 7 INCH. INSTALLED REPAIR DOUBLER, REPAIRED PER TR 53-10-11. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA970007Bulkhead · crackedINT - DURING Q-6 CHECK EDDY CURRENT, FOUND 2 INCH LONG CRACK PRESSURE BULKHEAD STATION 178, WL 198 RBL 7. INSTALLED REPAIR DOUBLER, REPAIRED PER TR 53-10-11. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA970006Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 56 INCH CORRODED AREA AT STRINGER 27L, BS 939 - BS 995. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER EA 41963. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970005Bulkhead Fitting · corrodedINT - DURING Q-6 VISUAL INSPECTION, FOUND 3.9 INCH BY .5 INCH BONDED DOUBLER/BULKHEAD FITTING CORRODED AT BS 663.75 AT STRINGER 17R. REMOVED CORROSION AND INSTALLED REPAIR PER EA 41979. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA970004Skin · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .1875 INCH CRACK AFT SERVICE DOOR UPPER HINGE CUTOUT IN FLANGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21 A. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970003Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.25 INCH LONG CRACK IN FUSELAGE SKIN AT EDGE OF EQUIPMENT COOLING EXHAUST OUTLET STATION 376, LBL 2 INCH. STOP DRILLED CRACK, INSTALLED EXTERIOR DOUBLER, REPLACED INTERIOR DOUBLER. REPAIRED PR 51-10-1 SRM, ANDJan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970002Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 12 INCH STATION 902 TO STATION 914, STRINGER 26L. INSTALLED REPAIR SPLICE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C 53-107-02, CORROSION LEVEL 2. (M)Jan 8, 1997 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA97010Shear Tie · corrodedPAE - FOUND CORROSION (C53-028-01) ON UPPER SURFACE OF SHEAR TIE IN FORWARD CARGO BAY AT BS 420 LBL 9 WL 148. BLENDED OUT CORROSION ON UPPER SURFACE OF SHEAR TIE IN FORWARD CARGO BAY AT BS 420 LBL 9 WL 148. REMOVED 2 INCHES BY 1 INCH BY .005 INCH WITH ORIGINJan 8, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA97009Skin · dentedFOUND FORWARD CARGO DOOR OUTER SKIN IS DENTED AND GOUGED ALONG ENTIRE LENGTH OF LOWER SKIN. REMOVED DAMAGED AREAS, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 52-00-3, 51-40-3 ON FORWARD CARGO DOOR OUTER LOWER SKIN. (M)Jan 7, 1997 · N207AU · Boeing 737201 · Cargo/Baggage DoorsSDR F3LA97008Frame · crackedPAE - FOUND FORWARD CARGO DOOR FORWARD SIDE FRAME AROUND LATCH CAM IS CRACKED. REMOVED AND REPLACED FORWARD CARGO DOOR FORWARD SIDE FRAME AROUND LATCH CAM PER SRM 51-30-2 AND 51-30-8. (M)Jan 7, 1997 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA97007Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 294 LBL 12 TO RBL 34 WL 208. REMOVED AND REPLACED UPPER CHORD OF FLOORBEAM BS 294 WL 208 FROM RBL 60 TO LBL 60 IN IAW SRM 53-10-9, SRM 53-10-1. (M)Jan 7, 1997 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97006Seat Tracks · corrodedPAE - FOUND CORROSION (53-107-02) ON SEAT TRACK BS 328 TO 360, RBL 22 WL 208. REMOVED CORRODED SEAT TRACK AT BS 328 TO 360 RBL 22 WL 208 AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-30-2, MM 51-21-1 AND 51-21-171. (M)Jan 7, 1997 · N207AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA97002Bulkhead Web · crackedPAE - AT BS 178 BULKHAD, NDI SHOWED 12 CRACK INDICATIONS AT VARIOUS LOCATIONS BETWEEN WL 184 TO WL 234, RBL 17.5 TO LBL 17.5. BLIND FASTENERS INSTALLED IN PREVIOUS REPAIR AT WL 234, RBL 12 AND LBL 12. REMOVED CENTER WEB, FABRICATED, ALODINED, PRIMED AND INSTJan 7, 1997 · N207AU · Boeing 737201 · Fuselage Main, BulkheadSDR F3LA97004Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 344, RBL 10, WL 208. REMOVED .028 INCH OF MATERIAL 4 INCHES BY 2 INCHES FROM ORIGINAL THICKNESS OF .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. FABRICATED AND REPLACED IAW SRM 53-10-09 INSTALLED Jan 6, 1997 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA97003Floorbeam · corrodedPAE - FOUND CORROSION (C53-202-04) ON AFT SIDE OF FLOOR BEAM (PREVIOUS REPAIR) BS 986, LBL 5 TO RBL 5, WL 208. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS ON AFT SIDE OF FLOOR BEAM, REPAIRED PE SRM 53-10-9. (M)Jan 6, 1997 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAASB97006Connector · looseCLE - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT ROWS 1, 2 AND 3 INOP. MAINTENANCE REPLACED PIN NR 1 AT CANNON PLUG D9004P. OPERATIONAL CHECK GOOD. (M)Jan 4, 1997 · N257AU · Boeing 737201 · Emergency LightingSDR USAASB97004Transmitter · failedBWI - FLT 570 - INBOUND TO BWI, THE NR 2 ENGINE OIL PRESSURE INDICATOR DROPPED TO 27 PSI, WHICH IS IN THE RED RANGE. CREW GOT NO OIL LIGHT AND THE OIL PRESSURE LIGHT WOULD NOT PRESS TO TEST. CREW SHUT DOWN THE NR 2 ENGINE AND DECLARED AN EMERGENCY. FLIGHT LJan 3, 1997 · N241US · Boeing 737201 · Engine Oil PressureSDR 97ZZZX313Wire · failedELP - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY AISLE PATH LIGHTING AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OKAY.Jan 3, 1997 · N217US · Boeing 737201 · Light System WiringSDR USAASB97001Light · failedSYR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE MAIN ENTRANCE DOOR WOULD NOT ILLUMINATE OR RECHARGE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY ABOVE THE MAIN ENTRANCE DOOR. OPS CHECK GOOD. (M)Jan 1, 1997 · N264AU · Boeing 737201 · Emergency LightingSDR USAA970046Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK FORWARD SERVICE DOOR OUTER SKIN UPPER HINGE CUTOUT. EXT DOUBLER INSTALLED PER SRM 52-00-3. (M)Jan 1, 1997 · N252AU · Boeing 737201 · Service DoorsSDR F3LA96075Dome · mis repairedPAE - REPAIR ON BS 1016 PRESSURE DOME DOES NOT CONFORM TO THE SRM. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON PRESSURE DOME BS 1016, LBL 19, WL 244 PER SRM 53-10-4 FIGURE 3. (M)Dec 31, 1996 · N207AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960806Stringer · corrodedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 13 INCHES OF CORROSION, STRINGER 27 LEFT, BETWEEN STATION 1003 AND 1016. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1. (M)Dec 30, 1996 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA96074Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 1006 LBL 10 TO LBL 36 WL 208. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR PART IAW SRM 53-10-1, 53-10-6 AND 53-10-9 AT BS 1006 LBL 10 TO LBL 36 WL 208. (M)Dec 30, 1996 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA96073Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 947 RBL 40-47 WL 208 AND RBL 5-15. FOUND TO BE OUT OF LIMITS. REPLACED TOP CHORD AT STATION 947 LBL 35 TO RBL 61 WL 208 IAW SRM 53-10-9 AND EWO 96-0931. (M)Dec 30, 1996 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA96072Forging · crackedPAE - FOUND CRACK IN FORGING AT BS 727 BL 0, WL 208, 1.5 INCH LONG. REMOVED AND REPLACED FORGING AT BS 727 BL 0, WL 208 IAW SRM 51-10-1 AND SRM 51-30-2. (M)Dec 30, 1996 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA96071Frame · crackedPAE - FORWARD GALLEY DOOR AFT SIDE FRAME IS CRCKED, 3 INCHES TO 5 INCH CRACKS FOUND. REMOVED AND REPLACED FORWARD GALLEY DOOR AFT SIDE FRAME PER SRM 51-30-2. (M)Dec 30, 1996 · N207AU · Boeing 737201 · Galley DoorsSDR F3LA96070Angle · crackedPAE - INBOARD LOWER RIB ANGLE CRACKED ON AFT END AT L/W AILERON NR 3 HINGE FITTING. REMOVED AND REPLACED INBOARD AND OUTBOARD LOWER RIB ANGLE ON L/W AILERON NR 3 HINGE FITTING IAW OHM 20-50-1. (M)Dec 30, 1996 · N207AU · Boeing 737201 · Wing Miscellaneous StructureSDR USAASB97031Battery Pack · dischargedBWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M)Dec 27, 1996 · N264AU · Boeing 737201 · Emergency LightingSDR F3LA96069Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 967 RBL 50, LBL 25, WL 208. FOUND CORROSION ON FLOORBEAM TO BE OUT OF LIMITS. REPLACED FLOORBEAM PER EWO 96-0930 AND SRM 53-10-9. (M)Dec 26, 1996 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAASB96268Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR INTERIOR AND EXTERIOR EXIT LIGHTS INOP. ALSO, THE MAIN ENTRANCE DOOR UPPER EMERGENCY LIGHT WAS FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR UPPER EMEDec 25, 1996 · N232US · Boeing 737201 · Emergency LightingSDR USAA960805Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.1250 INCH CRACK STRINGER 17 L, BS 760 FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960804Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, INSPECTION FOUND .75 INCH CRACK AT FUSELAGE SKIN STRINGER 17L, BS 740. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960803Stringer · corrosionROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27L, BS 1000 TO 1016. SPLICED IN STRINGER, REPAIRED PER CD 25G00984A, SRM 53-10-3 FIG 1. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960802Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 3 INCH CRACK STRINGER 16 BS 727A PLUS 8 L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960801Stringer · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK STRINGER 18A, SHEAR BEAM BS 727 LEFT. INSTALLED REPAIR KIT 65C29228-3, REPAIRED PER EO 5393G256/EA 59193. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960800Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .3125 INCH CRACK FORWARD ENTRY DOOR CUT OUT FORWARD UPPER HINGE CUT OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1 AND TR 53-30-11. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960799Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, FOUND 2.5 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17 R BS 328) FUSELAGE SKIN, TEAR STRAP AND BEAR STRAP. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA96068Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED CORROSION ON TOP CHORD OF FLOORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED 3 INCH BY 3 INCH BY .024 INCH ORIGINAL THICKNESS .080 INCH. FOUND TO BE OUT OF LIMITS IDec 23, 1996 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR F3LA96067Floorbeam · corrodedPAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 328, RBL 10 TO RBL 41, WL 208. REMOVED CORROSION IN AN AREA OF 3 INCH BY 18 INCH WITH A DEPTH OF .028 INCH AND AN ORIGINAL THICKNESS OF .080 INCH, FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLDec 23, 1996 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960798Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS .175 INCH LONG BS 440, BETWEEN STRINGER 23R AND STRINGER 24R SKIN. TRIMMED OUT DAMAGE, INSTALLED FILLERS AND REPAIRED DOUBLER, REPAIRED PER EA NR 41810. (M)Dec 21, 1996 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960797Skin · crackedINT - DURIGN Q-6 CHECK EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK LOWER AFT CORNER RT FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED TRIPLER REPAIR PLUS 3.7 LB WEIGHT CHANGE. REPAIRED PER SRM 53-30-3. (M)Dec 21, 1996 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960796Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 296, RBL 55 WL 208 FRAME. STOP DRILLED AND INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3 FIG 1. (M)Dec 21, 1996 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA960795Skin · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK AFT SERVICE DOOR CUTOUT AT UPPER HINGE CUTOUT FORWARD END SKIN. INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M)Dec 21, 1996 · N248US · Boeing 737201 · Fuselage Main, Plate/Skin
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