Boeing 737-301

Service difficulty reports · 4,797

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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 = '737301'
  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 USAA04337Skin · damagedFOUND PROBLEM WITH PREVIOUS REPAIR AT BS 470, STRINGER 8L TO 9L. REPAIRED PER SRM 53-00-01 FIGURE 201. (M)Jun 22, 2004 · N575US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA04336Spar · damagedPIT - FOUND PROBLEM WITH PREVIOUS REPAIR ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB AT REAR SPAR LOWER SURFACE. REPAIRED PER SRM FIUTE 204 DETAIL NR 1. (M)Jun 22, 2004 · N575US · Boeing 737301 · Horizontal Stabilizer, Spar/RibSDR USAA040304Skin · delaminatedPIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTERNAL DOUBLER AND NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M)Jun 15, 2004 · N575US · Boeing 737301 · Wing, Plate/SkinSDR USAA040305Skin · delaminatedPIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DAMAGE. INSTALLED FILLER/CORE MATERIAL, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)Jun 15, 2004 · N575US · Boeing 737301 · Wing, Plate/SkinSDR USAA040288Beam · crackedPIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M)Jun 11, 2004 · N355US · Boeing 737301 · Vertical StabilizerSDR USAA040287Floorbeam · corrodedPIT - FOUND BEAM CORRODED THREE 1 INCH DIAMETER AREAS, BS 947 LBL 30 TO LBL 46. REMOVED CORROSION, TREATED AND PRIMED, PERFORMED TYP REPAIR 53-15-01B, SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Jun 10, 2004 · N355US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA040290Lug · wornPIT - FOUND BEAR LUG WORN, BEARING LUG BORE WORN INSIDE DIAMETER SURFACE .75 INCH. ROTO PEENED BORE ID PER TYPE REPAIR 54-50-09 REV C. (M)Jun 8, 2004 · N334US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA040281Stiffener · corrodedPIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BOEING DWG 65C28106. (M)Jun 8, 2004 · N575US · Boeing 737301 · Fuselage Main, BulkheadSDR USA2004F00071Wire · brokenMAINTNANCE REPORTED THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED A BROKEN WIRE. OPERATIONAL CHECK GOOD.Jun 8, 2004 · N563AU · Boeing 737301 · Light System WiringSDR USA2004F00080Shuttle Valve · faultyENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING NOT AS MUCH EFFORT WAS REQUIRED. AC WAS FOUND IN SAFE CONDITION FOR MAINT FERRY FLIGHT. Jun 5, 2004 · N563AU · Boeing 737301 · Hydraulic System, MainSDR USA2004F00078Control System · malfunctionedENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING, NOT AS MUCH EFFORT WAS REQUIRED. AIRCRAFT WAS FOUND IN SAFE CONDITION FOR MAINTENANCE FJun 5, 2004 · N563AU · Boeing 737301 · Elevator Control SystemSDR USAA040278Stiffener · corrodedFOUND RADIAL STIFFENER CORRODED 1 INCH, STATION 1016, AFT PRESS BULKHEAD CENTER RADIAL AT BL 0 . MANUFACTURED AND INSTALLED REPAIR ANGLES TO REPLACED SECTION PER EO 5302V112A. (M)Jun 4, 2004 · N589US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040279Bulkhead · corrodedPIT - FOUND WEB CORRODED .25 INCH AREA, STATION 1016, AFT PRESSURE BULKHEAD WEB AT BL 0 UNDER STIFFENER. REMOVED FASTENERS BURNISHED AREA, TREATED, PRIMED, RE-INSTALLED FASTENERS PER EO 5302V112A. (M)Jun 4, 2004 · N589US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA040303Skin · dentedPIT - FOUND SKIN DENTED WITH DELAMINATION TWO AREAS 2 INCHES BY 1.5 INCH AND 1 INCH BY 1.375 INCH AREA, LEFT ELEVATOR LOWER SURFACE BETWEEN 176/200. REMOVED DISBONDED SKIN AND CORE, REPLACED CORE MATERIAL AND NEW DOUBLERS PER SRM 55-20-01 AND EA 78563. (M)Jun 3, 2004 · N575US · Boeing 737301 · Elevator, Plate/SkinSDR AWXA200400581Flashlight · inoperativeEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CABIN FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.May 30, 2004 · N326AW · Boeing 737301 · Emergency EquipmentSDR USAA040280Splice · crackedPIT - FOUND STRINGER SPLICE CRACKED 1 INCH, STRINGER 4 LEFT, FRAME STATION 907 IN CENTER FLANGE OF STRINGER SPLICE. REMOVED AND REPLACED PART PER OM-26 AND J3-58-53513-C-001. (M)May 29, 2004 · N589US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040297Skin · delaminatedPIT - FOUND SKIN AND CORE DELAMINATED 4 INCHES BY 4 INCHES, NR 5 SLAT OUTBOARD END TRAILING EDGE SECTION. INSTALLED NEW CORE PER SRM 51-20-10. (M)May 27, 2004 · N589US · Boeing 737301 · Leading Edge DevicesSDR USAA040298Skin · delaminatedPIT - FOUND SURFACE TO CORE DELAMINATION 3 INCHES BY 2.5 INCH AREA, NR 4 SLAT TOP SURFACE INBOARD TRAILING EDGE. INSTALLED NEW CORE AND EXT DOUBLER PER SRM 51-70-10. (M)May 26, 2004 · N589US · Boeing 737301 · Leading Edge DevicesSDR USAA040301Skin · delaminatedPIT - FOUND SKIN TO CORE BOND WITH 1 INCH DIAMETER AND .75 INCH DIAMETER, LEFT WING NR 2 SLAT TOP SURFACE INBOARD AND OUTBOARD T/E CORNERS. REMOVED EXT SKIN AND DAMAGED CORE, INSTALLED NEW PER SRM 51-70-10. (M)May 26, 2004 · N589US · Boeing 737301 · Leading Edge DevicesSDR USA2004F00095Check Valve · contaminatedON APPROACH, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED AND THAT THE RT MLG WOULD NOT EXTEND. TOWER CONFIRMED THAT THE RT MLG WAS NOT DOWN. CAPTAIN EXTENDED THE RT MLG MANUALLY USING THE ALTERNATE GEAR EXTENSION PROCEDURES. GEAR FELL AND LOCKEMay 24, 2004 · N352US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAASB04063Wire · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 5, 6, 7, 8 AND 10 INOPERATIVE. MAINTENANCE FOUND WIRES SHORTED AT SEAT ROW 9, LEFT SIDE. REPAIRED WIRES. ALSO, REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)May 21, 2004 · N574US · Boeing 737301 · Light System WiringSDR USAA040230Lap Joint · corroded.2500 INCH DIA. AREA OF CORROSION ON LAP JOINT AT STA 1016 BL 0. REMOVED RIVET AND CLEANED CORROSION AROUND RIVET HOLE AND REINSTALLED RIVET IAW SRM, FIG 1.May 16, 2004 · N352US · Boeing 737301 · Fuselage Main, StructureSDR USAA040231Stiffener · corrodedSTIFFENER (1 INCH X 1 INCH AREA) CORROSION; NO LEVEL/TASK NO LEVEL/TASK STA 1016 AT BL 0. CLEANED CORROSION AND TREATED AND PRIMED IAW SRM 53-00-01 FIG 101.May 16, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USA2004F00048Circuit Card · malfunctionedAFTER TAKEOFF, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED OPERATION OF NOSE LANDING GEAR DOWN LOCK SENSOR ANMay 13, 2004 · N591US · Boeing 737301 · Landing Gear Position and WarningSDR USA2004F00036Charger · failedMAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD.May 13, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR SWAA041327Battery · inoperativeDURING SPV, FOUND R2 DOOR EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.May 10, 2004 · N659SW · Boeing 737301 · Emergency LightingSDR SWAA041326Battery · inoperativeDURING SPV, FOUND EMERGENCY EXIT LIGHTS RT MID CABIN, INOP. REMOVED AND REPLACED BATTERY PACK PER MM.May 10, 2004 · N659SW · Boeing 737301 · Emergency LightingSDR SWAA041325Bulkhead · corrodedDURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, RBL 2 TO LBL 2, CORRODED. REPAIRED PRESSURE WEB PER ER.May 10, 2004 · N659SW · Boeing 737301 · Fuselage Main, BulkheadSDR USA2004F00037Battery Pack · dischargedMAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD.May 8, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR USAA040191Skin · crackedPIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DOUBLER, TRIPLER AND FILLERS PER EA 78356. (M)May 7, 2004 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040189Skin · crackedCLT - FOUND SKIN CRACKED 1.8125 INCH CRACK STATION 727D, STRINGER 24R. DOUBLER INSTALLED PER SRM 53-00-01, DETAIL X1, FIG 229. (M)May 5, 2004 · N589US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040232Frame · crackedFRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004.May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, FrameSDR USAA040200Stringer · crackedSTRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02.May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040182Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE BETWEEN STATION 986.5 AND 100.6 PER SRM 52-10-02. (M)May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA040181Support Fitting · crackedPIT - FOUND MLG SUPPORT FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUPPORT FITTING PER EA 78221. (M)May 3, 2004 · N585US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA040179Web · crackedPIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PER SRM 51-10-2. (M)May 3, 2004 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040180Support Fitting · crackedPIT - FOUND MLG SUPPORT FITTING CRACKED .25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT MLG SUPPORT FITTING PER EA 78221. (M)May 3, 2004 · N585US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA040122Skin · crackedCLT - FOUND SKIN CRACKED 3.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT, STATION 344.47, WL 207.5. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 202. (M)Apr 22, 2004 · N588US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040141Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727D S-23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)Apr 17, 2004 · N558AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200400368Indicator · faultyON TAKEOFF, NR 2 ENGINE OIL PRESSURE NEVER WENT ABOVE 21 PSI IN YELLOW RANGE, REJECTED TAKEOFF BETWEEN 100-110 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND INDICATOR IAW BMM 79-32-01 & 79-32-02, OPERATIONAL CHECK WAS GOOD. FApr 14, 2004 · N325AW · Boeing 737301 · Engine Oil Indicating SystemSDR USA2004F00025Outflow Valve · failedON CLIMB OUT, ENROUTE, THE AUTO MODE OF THE PRESSURIZATION CONTROLLER FAILED AT FL230. THE AUTO FAIL LIGHT ILLUMINATED AND THE CABIN PRESSURE WARNING HORN ACTIVATED AS CABIN ALTITUDE REACHED 12,000 FEET. THE OUTFLOW VALVE WAS NOTED AS BEING CLOSED. FLIGHT DApr 10, 2004 · N591US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR USAA040160Stringer Splice · crackedPIT - FOUND STRINGER SPLICE WITH TWO .125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)Apr 9, 2004 · N585US · Boeing 737301 · Fuselage Miscellaneous StructureSDR SWAA041019Skin · delaminatedDURING SCHEDULED RON, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED RT WING OUTBOARD T/E AFT FLAP PER SRM.Apr 8, 2004 · N660SW · Boeing 737301 · Trailing Edge FlapsSDR USAA040116Skin · crackedCLT - FOUND SKIN CRACKED .700 INCH, 3 INCHES AFT OF FS 727D ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)Apr 7, 2004 · N563AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA041007Bracket · brokenDURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM.Apr 7, 2004 · N659SW · Boeing 737301 · Escape SlideSDR USAA040096Bulkhead · corrodedFOUND AFT PRESSURE BULKHEAD CORRODED 2 FEET BY 2 INCH AREA, FROM LBL .5 TO RBL 5 INCHES IN FRONT OF CHANNEL STIFFENER. INSTALLED FILLERS, DOUBLERS AND STIFFENERS PER BAC DWG 65C28106, SRM 51-40-02, 53-80-08, EA 781171. (M)Apr 1, 2004 · N576US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA040098Stringer · crackedPIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, FROM AFT EDGE TO INBOARD FASTENER LEFT 18A SHELF. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M)Apr 1, 2004 · N576US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040099Stringer · crackedPIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, AFT END OF RIGHT 18A SHELF INTO FIRST FASTENER. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M)Apr 1, 2004 · N576US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040101Skin · crackedFOUND SKIN CRACKED .375 INCH, TOP HINGE CUTOUT AFT SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-60-01. (M)Apr 1, 2004 · N574US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA040955Battery · inoperativeDURING SCHEDULED RON, FOUND LT CENTER AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.Mar 31, 2004 · N659SW · Boeing 737301 · Emergency Lighting
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