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 USAA010411Floor Support · corrodedPIT - FOUND FLOOR SUPPORT BEAM CORRODED 160 INCHES, STATION 500D TO STATION 380 FLOOR SUPPORT BEAM 26L. CORROSION LEVEL 1, TASK C53-208-01. REMOVED CORROSION, REPAIRED SUPPORT BEAM, REPLACED SECTION PER TYPICAL REPAIR 53-20-04. (M)Mar 22, 2001 · N587US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010408Link · corrodedPIT - FOUND LINK WITH 3 INCH DIAMETER FRETTING, RIGHT WING INBOARD DOG BONE LINK LUG ON AFT SIDE OF SPAR. BLENDED AREA, DAMAGE TREATED AND PRIMED. (M)Mar 20, 2001 · N587US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010407Bracket · crackedPIT - FOUND BRACKET CRACKED .375 INCH, 14 INCHES INBOARD OF ENGINE PYLON LEFT WING REAR SPAR. REPAIRED PER 2024-T3 DWG NR 69-43586-7 SH 26 ZONE B6 PER SRM 57-20-10 PAGE 10. (M)Mar 20, 2001 · N587US · Boeing 737301 · Wing Miscellaneous StructureSDR USAA010297Skin · crackedTPA - FOUND SKIN CRACKED .25 INCH, LOWER LOBE FUSELAGE SKIN DIRECTLY AFT COOLING FAN CUTOUT. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M)Mar 20, 2001 · N588US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01083Door · not closedBWI - FLT 1568 - ON CLIMB-OUT FROM DCA, AT APPROXIMATELY 4,500 FEET, THE FLIGHT ATTENDANT ADVISED CREW OF A LOUD AIR NOISE COMING FROM THE FORWARD ENTRY DOOR. SIMULATANEOUSLY, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. FLIGHT DIVERTED TO BWI AND LANDED Mar 20, 2001 · N300AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA010259Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH LONG CRACK, RIGHT SIDE, STATION 727D AT STRINGER 23 RT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201. (M)Mar 12, 2001 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA010260Spar · damagedPIT - FOUND REAR SPAR WITH PLY SEPARATION .5 INCH BY .5 INCH, BOTTOM INBOARD SPAR END. REMOVED SPLINTER PLY THEN COMPLETED 2 WET LAY UP THEN RESEALED EDGES PER EA 70365 AND SRM 51-70-17. (M)Mar 8, 2001 · N587US · Boeing 737301 · Wing SparSDR USAASB01071Power Supply · failedGSO - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Mar 2, 2001 · N576US · Boeing 737301 · Emergency LightingSDR USAASB01069Charger · inoperativeDCA - MAINTENANCE FOUND THE THIRD BULLNOSE EMERGENCY LIGHT IN THE CABIN INOPERATIVE. MAINTENANCE REPAIRED THE GROUND ON PIN 16 OF PLUG D2962 AT STATION 462. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY (P/N 2012-1) AT STATION 62Mar 1, 2001 · N352US · Boeing 737301 · Emergency LightingSDR USAASB01065Switch · faultyCLT - FLT 1625 - EN ROUTE FROM CLT-JAX, AS CREW RETRACTED THE FLAPS/SLATS, THE NR 6 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND OVERHEAD PANELS AND WOULD NOT EXTINGUISH. THE CREW VISUALLY LOOKED AT THE SLATS ON THE WINGS AND APPEARED TO BFeb 27, 2001 · N575US · Boeing 737301 · Leading Edge Slat Position Indicating SystemSDR USAA010405Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED, .5 INCH BY 1 INCH IS LARGEST, 1 INCH, .75 INCH, AND .25 INCH STATION 996.5 LBL 50 RBL 50. PER TYPICAL REPAIR 53-15-01B. (M)Feb 26, 2001 · N587US · Boeing 737301 · Fuselage Main, Floor BeamSDR SWAA010575Charger · inoperativeDURING SCHEDULED RON CHECK, FOUND 2 BULLNOSE EMERGENCY EXIT LIGHTS INOP AT LEFT AFT CABIN. REMOVED AND REPLACED BATTERY CHARGER PER MM.Feb 26, 2001 · N660SW · Boeing 737301 · Emergency LightingSDR USAASB01060Controller · faultyCLT - FLT 1262 - ON CLIMB-OUT FROM PBI, EN ROUTE TO PHL, PRESSURIZATION WAS UNCONTROLLABLE WITH THE RIGHT PACK AS THE LEFT PACK WAS ON MEL. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACFeb 25, 2001 · N575US · Boeing 737301 · Cabin Pressure ControllerSDR DL733010328Oven · malfunctionedFWD OVEN HAD AN ELECTRICAL /BURNT SMELL. GALLEY PWR WAS REMOVED, CONDITION IMPROVED. REPLACED FWD GALLEY OVEN AND BOTH CONTROLLERS. OVEN DPN 255701023, S/N 98-12-0066, CONTROL DPN 255701024, S/N OFF 8601-0701 & 8612-1728.Feb 24, 2001 · N948WP · Boeing 737301 · Buffet/GalleysSDR USAASB01052Battery Pack · dischargedGSO - MAINTENANCE FOUND SOME EMERGENCY LIGHTS IN THE CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Feb 17, 2001 · N584US · Boeing 737301 · Emergency LightingSDR SWAA010485Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, LBL 32. REPAIRED BEADED WEB PER TR T1-353-046.Feb 16, 2001 · N660SW · Boeing 737301 · Fuselage Main, StructureSDR SWAA010484Gusset · crackedDURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR CRACKED AT AFT LOWER CORNER GUSSET. REPAIRED GUSSET PER BAC DWG.Feb 16, 2001 · N660SW · Boeing 737301 · Service DoorsSDR USAA010206Fitting · crackedPIT - FOUND FITTING CRACKED AND CORRODED .25 INCH BY .075 INCH PLUS DEEP, RIGHT HORIZONTAL STABILIZER FITTING FORWARD TOP SPAR LUG HORIZ SIDE. CORROSION LEVEL 1. MACHINED FITTING AND INSTALLED NEW BUSHINGS PER SRM 55-10-10, J3-90-09000-173. (M)Feb 15, 2001 · N352US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA010205Fitting · corrodedPIT - FOUND FITTING BUSHING DAMAGE, RIGHT HORIZONTAL STAB FORWARD CENTER SECTION, TOP AFT CLEVIS FITTING. CORROSION LEVEL 1. MACHINED FORWARD FACE OF LUG REMOVED .014 INCH PER SRM 55-10-10, MFG NEW BUSHING PER SRM 55-10-10. (M)Feb 15, 2001 · N352US · Boeing 737301 · Horizontal Stabilizer StructureSDR SWAA010452Frame · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED VERTICAL CHORD PER SRM.Feb 13, 2001 · N660SW · Boeing 737301 · Fuselage Main, FrameSDR SWAA010451Lens · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REPLACED LENS PER MM.Feb 13, 2001 · N660SW · Boeing 737301 · Emergency LightingSDR SWAA010420Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT FWD SVC DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM.Feb 11, 2001 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01046Indicator · failedBUF - FLT 638 - DURING DESCENT INTO BUF, CREW EXTENDED FLAPS TO 5 DEGREES AND THEN TO 10 DEGREES BUT RECEIVED A FLAP LIGHT. FLAPS WOULD NOT EXTEND BEYOND 5 DEGREES. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED AT BUF WITHOUT FURTHER INCIDENT. MAINTENFeb 10, 2001 · N585US · Boeing 737301 · Leading Edge Slat Position Indicating SystemSDR SWAA010414Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND .75 INCH EXTERNAL FUSELAGE SKIN CRACK AT AFT SIDE OF EQUIPMENT EXHUAST CUTOUT. REPAIRED SKIN DOUBLER PER SWA ACO.Feb 10, 2001 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA010388Shear Tie · corrodedDURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 360. REPAIRED SHEAR TIE PER SRM.Feb 7, 2001 · N660SW · Boeing 737301 · Fuselage Main, StructureSDR SWAA010387Beam · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2.5 CRACK AT NLG ACTUATOR SUPPORT WEB, BS 232, BL 0, WL 184. REPAIRED WEB PER SRM.Feb 7, 2001 · N660SW · Boeing 737301 · Fuselage Miscellaneous StructureSDR SWAA010386Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACKS AT WL 187.5, LBL 1 & RBL 1. REPAIRED BULKHEAD WEB PER SRM.Feb 6, 2001 · N660SW · Boeing 737301 · Fuselage Main, BulkheadSDR SWAA010385Frame · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, RBL 1. REPAIRED FRAME PER SRM.Feb 6, 2001 · N660SW · Boeing 737301 · Fuselage Main, FrameSDR SWAA010383Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 870, STR 23R. REPAIRED SKIN PER SRM.Feb 6, 2001 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA0001261O-Ring · crackedPHX - AIR TURNBACK - 1/31/01 - AFTER DEPARTURE FROM PHX THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND THE AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND A UNION ON THE NR 5 INBOARD GROUND SPOILER ACTUATOR LEAKING, CRACKED. THEFeb 6, 2001 · N324AW · Boeing 737301 · Drag Control ActuatorSDR SWAA010358Frame · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT SVC DOOR CUTOUT, BS 294, WL 208. REPAIRED FRAME PER SRM.Feb 5, 2001 · N660SW · Boeing 737301 · Fuselage Main, FrameSDR SWAA010357Crease Beam · crackedDURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CRACKED AT LT SIDE, BS 616 TO BS 639. REPAIRED CREASE BEAM WEB PER SRM.Feb 4, 2001 · N660SW · Boeing 737301 · Fuselage Main, StructureSDR SWAA010341Stringer Clip · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 663, STRS 10R & 10L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.Feb 2, 2001 · N660SW · Boeing 737301 · Fuselage Miscellaneous StructureSDR SWAA010337Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 4.75, WL 202. REPAIRED BULKHEAD WEB PER SRM.Feb 2, 2001 · N660SW · Boeing 737301 · Fuselage Main, BulkheadSDR SWAA010327Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 3 BS 178 BULKHEAD WEB CRACKS AT WL 234, LBL 12, LBL 10 & RBL 10. REPAIRED BULKHEAD WEB PER SRM.Feb 1, 2001 · N660SW · Boeing 737301 · Fuselage Main, BulkheadSDR USAA010169Floorbeam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .014 INCH, FLOOR DECK SUPPORT 1250 LBBL AFT STATION 767. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-06B. (M)Jan 23, 2001 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010168Floorbeam · corrodedPIT - FOUND SUPPORT BEAM CORRODED 1 INCH BY 4 INCHES BY .011 INCH, FLOOR DECK SUPPORT 300 LBBL AFT STATION 767. CORROSION LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REP 53-10-06B. (M)Jan 23, 2001 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010167Floorbeam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .016 INCH, FLOOR DECK SUPPORT 810 RBBL AFT OF STATION 767. CORROSION LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-068. (M)Jan 23, 2001 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010166Floorbeam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 5 INCHES BY .011 INCH, FLOOR DECK SUPPORT 810 LBBL AFT OF STATION 767. CORROSION LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-068. (M)Jan 23, 2001 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010165Floorbeam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES BY .017 INCH, DECK STRUCTURE 810 LBBL AFT STATION 727D. CORROSION LEVEL 1, TASK NR C53-202-01. INSTALLED DOUBLER PER TYP REPAIR 53-10-20. (M)Jan 23, 2001 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAASB01014Regulator · failedBWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEED PRESSURE WENT TO 30 PSI WHILE THE LEFT STAYED AT 0. CABIN ALTITUDE CLIMBED TO OVER 10,000 FEET AND SET OFF THE CABIN ALTITUDE WARNING HORJan 21, 2001 · N339US · Boeing 737301 · Pneumatic Distribution SystemSDR USAASB01013Adc · faultyTPA - FLT 9230 - AFTER T/O, AT APPROX 500 FT, THE WINDSHEAR WARNING WITH AUDIO SOUNDED ALONG WITH STICK SHAKER ACTIVATION. AIRSPEED DROPPED TO 110 KNOTS ON THE CAPTS SIDE. WINDSHEAR RECOVERY PROCEDURES WERE PERFORMED. AIRSPEED FLUCTUATED FROM 110 TO 125 KNOJan 20, 2001 · N588US · Boeing 737301 · Air Data ComputerSDR USAASB01012Warning System · malfunctionedORF - FLT 12 - AFTER TAKEOFF FROM MCO, CREW RECEIVED A RIGHT MLG RED LIGHT WHEN PLACING THE GEAR HANDLE TO THE UP POSITION AS WELL AS THE OFF POSITION. AFTER RECYCLING GEAR TO THE DOWN POSITION, INDICATIONS WERE NORMAL AS THREE GEAR GREEN LIGHTS ILLUMINATED. Jan 19, 2001 · N346US · Boeing 737301 · Landing Gear Position and WarningSDR USAASB01009Wire Harness · out of positionLGA - MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHTING AT SEAT 16C INOPERATIVE. MAINTENANCE REPOSITIONED WIRING HARNESS FOR SEAT ROW 16ABC EMERGENCY EXIT PATH LIGHTING. OPS CHECK GOOD. (M)Jan 18, 2001 · N300AU · Boeing 737301 · Light System WiringSDR USAASB01010Wire · disconnectedPIT - FLT 276 - AFTER TAKEOFF FROM AVP, EN ROUTE TO PIT, THE LANDING GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. LANDING GEAR HANDLE WAS MOVED TO THE DOWN POSITION, FLAPS WERE RETRACTED AND THE GEAR Jan 18, 2001 · N337US · Boeing 737301 · Landing Gear System WiringSDR USAASB01007Pump · failedPIT - FLT 9228 - DURING CRUISE, EN ROUTE FROM YUL-YYZ, THE NR 2 ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. DECISION WAS MADE FOR FLIGHT TO DIVERT TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DELCARED. MAINTENANCE REMOVED AND REPLACED TJan 15, 2001 · N592US · Boeing 737301 · Hydraulic Pump (Electric/Engine), MainSDR USAA010022Skin · crackedCLT - FOUND SKIN CRACKED, STATION 200, LBL 5. INSTALLED EXTERIOR DOUBLER PER EA 68798. (M)Jan 15, 2001 · N355US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAASB01005Door · not closedPHL - FLT 1228 - ON CLIMB-OUT FROM PHL, EN ROUTE TO CLT, CAPTAIN REPORTED THAT THE AIRCRAFT CABIN PRESSURE CONTINUED TO CLIMB ALONG WITH OUTSIDE PRESSURE. MIX VALVE APPEARS TO BE WORKING FINE. HOWEVER, FLIGHT ATTENDANT REPORTED THAT THE SEAL FOR THE AFT RIGHJan 13, 2001 · N351US · Boeing 737301 · Service DoorsSDR USAASB01002Indicator · failedPIT - FLT 1950 - ON DESCENT TO PIT, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. AS CREW POSITIONED FLAPS TO ONE DEGREE FLAPS, THE LEFT FLAP INDICATOR STOPPED AT ONE QUARTER DEGREE WHILE THE RIGHT FLAP INDICTOR STOPED AT JUST LESS THAN ONE DEGREE. CREW ACCOMPLIJan 2, 2001 · N351US · Boeing 737301 · Leading Edge Slat Position Indicating SystemSDR AWXA0001173Charger · failedRIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER; LIGHT CHECKS GOODJan 2, 2001 · N326AW · Boeing 737301 · Emergency Lighting
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