Boeing 737-232

Service difficulty reports · 1,700

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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 = '737232'
  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 DL73K000606Battery Pack · inoperativeTWO AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.Mar 30, 2000 · N320DL · Boeing 737232 · Emergency LightingSDR DL73K000595Unknown · odorFLT 2452 MCO-EWR, HAD ELECTRICAL ODOR AROUND THE FWD F/A JUMPSEAT. CREW DIVERTED TO RIC. TROUBLESHOOTING WITH CONTRACT MTC AND NOTHING FOUND. SENT MECH FROM CVG DUE TO ATL FLT DELAYED DUE TO MECHANICAL. DAL MECH ALSO FOUND NOTHING WRONG WITH ACFT.Mar 29, 2000 · N302DL · Boeing 737232 · Air Distribution SystemSDR DL73K000586Wire · pinchedON L/O, FOUND AISLE EMERGENCY EXIT LIGHTS INOP FWD OF WING. REPAIRED WIRING.Mar 27, 2000 · N316DL · Boeing 737232 · Light System WiringSDR DL73K000557Doubler · wornAN EXISTING DOUBLER WAS WORN ALONG IT'S AFT EDGE LOCATED AT THE FORWARD EDGE OF THE C1 DOOR. THE DOUBLER WAS REMOVED AND REPLACED PER ERA 334214-14. THE DAMAGE WAS FOUND AT HMV.Mar 22, 2000 · N302DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000539Spar · corrodedCORROSION WAS FOUND ON THE FRONT AND REAR SPAR OF THE HORIZONTAL STABILIZER CENTER SECTION ATTACH FITTING. CORROSION WAS FOUND ON THE FORWARD AND AFT FACES AND IN THE BORE. THE DAMAGE WAS REMOVED, TREATED AND PAINTED PER ERA 334168-14 AT HMV.Mar 20, 2000 · N302DL · Boeing 737232 · Horizontal Stabilizer, Spar/RibSDR DL73K000538Fitting · corrodedCORROSION WAS FOUND ON THE REAR SPAR ATTACH LUGS OF THE HORIZONTAL STABILIZER. THE CORROSION WAS TO THE FORWARD AND AFT FACES OF THE FITTING AND INSIDE THE LOWER BORE. THE CORROSION WAS REMOVED, TREATED AND PAINTED PER ERA 334170-14AT HMV.Mar 20, 2000 · N302DL · Boeing 737232 · Horizontal Stabilizer, Attach FittingsSDR DL73K000529Valve · malfunctionedAIRCRAFT FAILED TO PRESSURIZE AFTER T/O FROM PBI. OUTFLOW VLVS INDICATED FULL CLOSED. F/A REPORTED THERE WAS LOUD WIND NOISE AROUND L1 DOOR. DOOR INDICATED CLOSED AND LOCKED. DIVERTED TO MCO. PRESSURIZED AC TO 7 PSID. CHECKED ALL DOOR SEALS- CABIN, CARGOMar 17, 2000 · N319DL · Boeing 737232 · Cabin Pressure Control SystemSDR DL73K000526Fitting · corrodedCORROSION WAS FOUND ON THE FORWARD AND AFT FACE OF BOTH THE INNER LUGS OF THE VERTICAL STABILIZER ATTACH FITTING. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PAINTER PER ERA 334169-14. THE DAMAGE WAS FOUND AT HMV.Mar 17, 2000 · N302DL · Boeing 737232 · Vertical StabilizerSDR DL73K000525Fitting · corrodedCORROSION WAS FOUND ON ALL EIGHT OF THE AFT SPAR ATTACH LUGS ON THE BODY ATTACHMENT POINT FOR THE VERTICAL STABILIZER AT APPROXIMATELY FS 1080. CORROSION WAS REMOVED AND THE AREA TREATED AND PAINTED PER ERA 334185-14 AT HMV.Mar 17, 2000 · N302DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR DL73K000518Doubler · wornWEAR WAS FOUND ON THE LAP JOINT LOWER INTERNAL BONDED DOUBLER AT APPROXIMATELY FS 310 AND STR 10L JUST BELOW THE L1 DOOR UPPER HINGE CUTOUT. THE WEAR WAS .25 IN DIAMETER AND A MAXIMUM OF .011 DEEP. THE AREA WAS BLENDED AND TREATED PER ERA 334203-14. THE DAMMar 16, 2000 · N302DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000515Duct · failedAFTER TAKEOFF PVD WITH BLEEDS OFF, RE-CONFIGURED PNEU PANEL. FELT SURGE OF AIR IN A/C AND MUFFLED NOISE HEARD. FLT ATTN INFORMED CREW OF SMOKE AND FUMES IN CABIN. DECLARED EMERGENCY AND DIVERTED INTO BOS. FOUND BLOWN DUCTS IN AIR CONDITIONING DISTRIBUTION Mar 14, 2000 · N313DL · Boeing 737232 · Air Distribution SystemSDR DL73K000504Skin · crackedTHE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT WAS FOUND WITH A 1 INCH TYPICAL CRACK THROUGH THE SKIN, BONDED, DOUBLER, AND BEAR STRAP. THE CRACK WAS ROUTED OUT OF ALL MEMBERS AND REPAIRED WITH THREE ALUMINUM DOUBLERS PER ER/A 369515-14, REV A.Mar 10, 2000 · N309DL · Boeing 737232 · Passenger/Crew DoorsSDR DL73K000333Skin · crackedA 2 INCH LONG CRACK WAS FOUND IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP OF THE AFT ENTRY DOOR (L2) CUTOUT AT THE UPPER AFT CORNER. THE CRACK WAS ROUTED OUT OF THE SKIN ASSY AND REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 369290-14, REV C.Feb 18, 2000 · N328DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000328Skin · crackedA CRACK WAS FOUND IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP OF THE AFT ENTRY DOOR (L2) CUTOUT AT THE UPPER FWD CORNER. THE CRACK WAS ROUTED OUT OF ALL THREE MEMBERS AND REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 369342-14, REV A.Feb 17, 2000 · N328DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000313Skin · crackedTHE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR (L2) CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.3 X 2.4 CUTOUT AND REPAIRED WITH 3 EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 24 AND ER/A 369Feb 15, 2000 · N305DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000301Line · crackedON ARRIVAL PBI B-LOW QUANTITY LIGHT ILLUMINATED WITH LOSS OF HYD FLUID. INSTALLED INTRIM LINE BETWEEN NR 1 B-PUMP AND FILTER HOUSING. REF IPC 29-14-0-5E ITEM 156 (P/N 293201291).Feb 13, 2000 · N312DL · Boeing 737232 · Hydraulic System, MainSDR DL73K000255Fitting · corrodedTHE LT & RT MAIN LANDING GEARS SIDE STRUT SUPPORT FITTING LUGS AT FS 685 WERE FOUND WITH CORROSION IN THE LUG BORES AND ON THE LUG FACES. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES AND MACHINING THE LUG FACES. REPAIR BUSHINGS WERE INSTALLED Feb 3, 2000 · N311DL · Boeing 737232 · Fuselage, Landing Gear Attach FittingsSDR DL73K000244Skin · crackedA TYPICAL CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER OF THE LOWER HINGE CUTOUT OF THE AFT ENTRY DOOR (L2) CUTOUT. THE UNDERLYING BEARSTRAP WAS INSPECTED AND FOUND TO BE CRACK FREE. THE CRACK WAS ROUTED OUT OF THE SKIN ASSY WITH A .75 INCH CUTOUT AND REPAFeb 2, 2000 · N303DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000243Skin · crackedA TYPICAL CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER OF THE LOWER HINGE CUTOUT OF THE AFT ENTRY DOOR (L2) CUTOUT. THE CRACK WAS ROUTED OUT WITH A .75 INCH CUTOUT. THE UNDERLYING BEARSTRAP WAS INSPECTED AND FOUND UNDAMAGED. THE SKIN ASSY WAS REPAIRED WITFeb 1, 2000 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K000220Coffeemaker · malfunctionedDURING TAXI IN, NOTICED ELECTRICAL FUMES. FUMES SEEMED TO BE COMING FROM CB PANEL BEHIND F/O SEAT. ALSO, NOTICED BT LEAD. FLIGHT ATTENDANT FOUND R1 GALLEY COFFEEMAKER OVERHEATING. REPLACED SAME, PERFORMED OPS AND CHECK ALL OK. INSPECTED ALL CB PANELS AND Jan 30, 2000 · N310DA · Boeing 737232 · Buffet/GalleysSDR DL73K000217Wire · chafedREPAIRED SHORTED WIRE W448-001-20 PER WD 26-12-01. REPLACED LOOP CONNECTOR D858. ALL OPERATIONAL CHECKS NORMAL. LEFT WING BODY OVERHEAT.Jan 29, 2000 · N328DL · Boeing 737232 · Overheat DetectionSDR DL73K992800Seal · separatedNR 1 ENG HAD MULTIPLE COMPRESSOR STALLS AT FL310 AS THROTTLES RETARDED FROM CLIMB EPR TO CRUISE EPR OF 1.96. COMPRESSOR STALLS STOPPED AS THROTTLES WERE PULLED TO IDLE THE ENG WAS NOT SHUTDOWN AND OPERATED NORMALLY AT IDLE. REPLACED C2 FAN FOR SEAL LIBERATIODec 20, 1999 · N302DL · Boeing 737232 · Turbine Engine Compressor SectionSDR DL73K992779Fire Loop · malfunctionedATTEMPTED APU START PRIOR TO LANDING, HAD INDICATION OF APU FIRE (LIGHTS AND BELLS). FIRE HANDLE PULLED, BOTTLE DISCHARGED AND LIGHT EXTINGUISHED. INSPECTED APU AREA AND EXHAUST, SUSPECT FALSE INDICATION. REPLACED LOOP.Dec 16, 1999 · N309DL · Boeing 737232 · Fire DetectionSDR DL73K992743Beam · crackAFT CARGO DOOR / NR 2 STOP BEAM / OUTER CHORD: AD 98-11-04, R1 CRACK FOUND IN TYPICAL POSITION ON NR 2 STOP BEAM OUTER CHORD AS ADDRESSED IN SUBJECT AD (I.E. LOCATED AT FWD END OF BEAM ADJACENT TO STOP FITTING). AUTHORIZED ANGLE REPAIR.Dec 11, 1999 · N322DL · Boeing 737232 · Cargo/Baggage DoorsSDR DL73K992714Fire Detector · malfunctionedAPU FIRE INDICATION AFTER START AT 12,000 FT. PULLED FIRE HANDLE AND THE LIGHT REMAINED ON. AFTER FIRING THE BOTTLE THE FIRE HANDLE LIGHT WENT OUT IN ABOUT 2 SEC. APU HAD BEEN RUNNING FOR ABOUT 1 MIN WHEN THE FIRE INDICATION CAME ON. TROUBLESHOOT SYSTEM, NDec 11, 1999 · N309DL · Boeing 737232 · Fire DetectionSDR DL73K992698Fitting · corrodedTHE STRUT ATTACH LUG OF THE RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LUG BORE AND ON THE LUG FACES. THE BORE WAS OVERSIZED AND THE LUG FACES MACHINED TO REMOVE THE CORROSION. A REPAIR BUSHING WAS INSTALLED ADec 8, 1999 · N332DL · Boeing 737232 · Fuselage, Landing Gear Attach FittingsSDR DL73K992655Turbine Wheel · damagedAT APPROX 400 FT AGL, LOUD BANG, NR 1 ENGINE FAILED 700 DEGREES EGT, WINDMILLING N1 AND N2 WAS BLOF T/O DUE TO GROSS WT. FOUND 3RD STAGE OF LPT DAMAGED. REPLACED ENGINE.Dec 6, 1999 · N329DL · Boeing 737232 · Turbine SectionSDR DL73K992651Light · inoperativeEMERGENCY EXIT LIGHTING INOP ROWS 1 THRU 3. REPLACED PWR SUPPLY AND FOUND WIRES SHORTED AT ROW 4 D, E, F. REPAIRED SAME, OPS CKS NORMAL.Dec 4, 1999 · N302DL · Boeing 737232 · Emergency LightingSDR DL73K992644Panel · looseLOUD NOISE COMING FROM RT REAR OF AIRCRAFT, FELT VIBRATION ON PEDALS DURING CRUISE AT FL 150 AND 240. NO AIRCRAFT CONTROL PROBLEMS NOTICED. NO SIGNIFICANT PRESSURIZATION PROBLEMS NOTICED. INSPECTED A/C PER MM 5-51-281. FOUND DEBRIS ON AFT PRESS RELIEF VALVDec 3, 1999 · N312DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992555Bleed Line · leakingSOLID WING BODY OVERHEAT LIGHT PASSING 1,500 FT, AFTER TAKEOFF. AFTER COMPLETING PROCEDURES, LIGHT REMAINED ON. RETURNED TO DEPARTURE AIRPORT AND LANDED. A/C GROSS WEIGHT UPON LANDING 112,000 LBS. FOUND BLEED LEAK FWD OF APU BLEED VALVE. REPLACED GASKETSNov 20, 1999 · N325DL · Boeing 737232 · APU Bleed Air SystemSDR DL73K992427Compressor · bird srtikeON APPROACH BOS CREW REPORTED POSSIBLE BIRD STRIKE. INSPECTION FOUND DAMAGE TO NR 2 ENGINE FAN BLADES. DRESSED BLADES TO LIMITS OF 5 FLIGHTS FLY BACK LIMITS. RAN ENGINE TO TAKEOFF POWER. ALL PARAMETERS AND OPERATION NORMAL.Nov 2, 1999 · N313DL · Boeing 737232 · Turbine Engine Compressor SectionSDR DL73K992396Stringer · crackedTHE STRINGER 18A WEB WAS FOUND WITH A CRACKED FASTENER HOLE AT FS 727 ON THE LT AND RT SIDES OF THE AIRCRAFT. THE CRACKS ARE TYPICAL OF THOSE NOTED IN BAC S/B 737-53-1066. THE CRACKS WERE REPAIRED WITH A NEW GUSSET CHANNEL SIMILAR TO THE S/B AND INSTALLED PEOct 27, 1999 · N322DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR DL73K992381Air Dist · odorELECTRICAL ODOR EMINATING FROM FWD CABIN (ROW 4 TO FWD GALLEY) SIMILAR TO VERY POTENT MATCH SMELL. INSPECTED ACFT ELECT SYS, GALLEY PWR, OVERHEAD AND SIDEWALL LIGHTS, ALL OK. RAN NR 1 AND NR 2 ENGINES, LOADED ELECT SYSYEMS NTF. RAN LT AND RT PACKS, NO ODOR Oct 26, 1999 · N318DL · Boeing 737232 · Air Distribution SystemSDR DL73K992329Power Supply · inopAT DEPARTURE TIME, EMERGENCY LIGHTS ROWS 1 THRU 16 WOULD NOT TURN OFF. REPLACED POWER SUPPLY AND BATTERY LIGHTS OPERATION NORMAL.Oct 22, 1999 · N311DL · Boeing 737232 · Emergency LightingSDR DL73S992312Skin · crackedTHE LOWER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A .7 TYPICAL CRACK THROUGH THE SKIN AND BONDED DOUBLER. THE BEAR STRAP WAS UNDAMAGED. THE CRACK WAS ROUTED OUT OF THE SKIN AND DOUBLER AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER AND TRIPLER POct 20, 1999 · N323DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S992310Skin · crackedA .8 LONG CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER AT THE LOWER FORWARD CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND BONDED DOUBLER (BEAR STRAP WAS UNDAMAGED) AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PEROct 20, 1999 · N323DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992301Battery · dischargedON L/O, FOUND AFT SECTION EMERGENCY LIGHTS INOP ROWS 17 TO 20 INCLUDING RT SIDE GALLEY. FOUND BATTERY AT MODULE M9222 INOP. REPLACED BATTERY, EMERGENCY LIGHTS OPN CKS NORMAL.Oct 19, 1999 · N326DL · Boeing 737232 · Emergency LightingSDR DL73K992299Skin · crackedA .125 INCH CRACK AT FUSE SKIN AT L-1 WINDOW UPPER O/B CORNER. INSTALLED DOUBLER PER SRM 53-30-3 REPAIR II FIG 11.Oct 19, 1999 · N309DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992298Skin · crackedA 2.25 INCH CRACK IN FUSE SKIN STA 727B STR 18 RT. INSTALLED DOUBLER PER SRM 53-30-3 F1.Oct 19, 1999 · N309DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992297Skin · crackedA 2.25 INCH CRACK IN FUSE SKIN STA 767 ABOVE STR 19 RT. INSTALLED DOUBLER PER SRM 53-30-3 F1.Oct 19, 1999 · N309DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992217Skin · crackedFUSELAGE, SKIN ASSY, L1 DOOR CUTOUT, CRACK REPAIR. A CRACK WAS FOUND IN THE SKIN, DOUBLER, AND BEAR STRAP AT THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS REPAIRED WITHIN INTERIM STRAP REPAIR PER THE Oct 2, 1999 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73K992170Yaw Damper · malfunctionedUNCOMMANDED ROLL/YAW AT 31000 FT, 77 MACH AUTOPILOT ENGAGED, A/C ROLLED HARD LEFT. REQUIRED 40-50 DEGREE AILERON TO TO RIGHT TO COUNTER COMMAND ROLL. POM COMPLIED WITH YAW DAMPER DISENGAGED. A/C RETURNED TO NORMAL FLIGHT. REPLACED YAW DAMPER COUPLER AND RUDSep 28, 1999 · N310DA · Boeing 737232 · Autopilot SystemSDR DL73K992023Fuse · blownE-PATH LIGHTS INOP ROW 10 TO 18. REPLACED FUSE IN PWR SUPPLY.Sep 11, 1999 · N314DA · Boeing 737232 · Emergency LightingSDR DL73K991943Power Supply · inopON TAXI OUT, UNABLE TO EXTINGUISH EMERG FLOOR PATH LIGHTING SYS RT SIDE OF A/C. REPLACED AFT RT EMERGENCY LIGHT PWR PACK AND BATTERY IN FWD GALLEY CEILING. SYS OPERATION NORMAL.Sep 1, 1999 · N322DL · Boeing 737232 · Emergency LightingSDR DL73K991937Bulkhead Web · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH A .75 CRACK AT LBL 6.7 WL 208 AND ANOTHER .75 CRACK AT BL 0 WL 190. THERE WAS AN EXISTING DOUBLER REPAIR INSTALLED TO REPAIR OTHER PREVIOUS CRACK CUTOUTS. THE EXISTING DOUBLER WAS REMOVED, THE WEB INSPECTED, THE NEW CRAug 29, 1999 · N307DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73K991915Fan · failedAT DEPARTURE - WHEN FLT CREW SWITCHED ON GASPER FAN GOT ELECTRICAL SMELL IN COCKPIT AND CABIN. REMOVED BAGS FROM FWD B/B AND PULLED AFT WALL TO CONFIRM GASPER FAN AT FAULT. REPLACED GASPER FAN, OP CHECKS GOOD.Aug 27, 1999 · N324DL · Boeing 737232 · Air Distribution FanSDR DL73K991899Sensor · inopNR 1 LEADING EDGE DEVICE INDICATED FULL EXTENDED AFTER FLAPSWERE PUT UP. REPLACED NR 1 LEADING EDGE FLAP DOWN SENSOR.Aug 25, 1999 · N322DL · Boeing 737232 · Leading Edge Slat Position Indicating SystemSDR DL73K991870Heat Valve · failedNOTICED NR 1 FUEL HEAT VALVE OPEN. COULD NOT CLOSE. OIL TEMP ROSE TO 140 DEG AND STAYED. AFTER 15 MIN NR 1 ENGINE WAS SHUTDOWN. REPLACED NR 1 ENG FUEL HEAT VALVE PER M/M 73-14-11. CHECKED OPERATION OF FUEL HEAT VALVE PER M/M 73-14-0. OPERATION CHECK NORMAAug 21, 1999 · N320DL · Boeing 737232 · Fuel HeaterSDR DL73K991841Outflow Valve · failedAT LEVEL OFF AT 37,000 ALTITUDE WARNING HORN SOUNDED AND CABIN ALTITUDE CLIMBING TO 10,000. DESCENDED TO MAINTAIN 10,000 CABIN ALTITUDE AND SELECTED MANUAL AC & DC WORKED OK NO FAIL LIGHT. FOUND FWD OUTFLOW VALVE STUCK OPEN. REPLACED VALVE. ALSO, OVHD PAug 17, 1999 · N309DL · Boeing 737232 · Pressure Regulator/Outflow ValveSDR DL73K991837Bulkhead Web · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS OF THE AFT PRESSURE BULKHEAD WEB, A CRACK INDICATION WAS NOTED NEAR STRINGER 6R. INTERNAL HFEC INSPECTION CONFIRMED TWO CRACKED FASTENER HOLES AT THE WEB TO CAP INTERFACE AT STRINGER 6R. THE CRACKED AREA OF WEB WAS CUTOUTAug 14, 1999 · N329DL · Boeing 737232 · Fuselage Main, Bulkhead
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