Boeing 737-232
Service difficulty reports · 1,700
Newest first. General aviation reporting is voluntary.
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 = '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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL73K002474Regulator · failedA/C FAILED TO PRESSURIZE_,AUTO STBY MANUAL CORR.ACT.FND PRESS LOW OFF NR 1 ENG ,REP NR 1 ENG PILOT PRESS REG PRESS A/C IN ALL POS .CK GOODSDR DL73K002455Floor Support · crackedCRACKS WERE FOUND IN THE WEB, DOUBLER AND UPPER CHORD OF THE LBL 24 LONGITUDINAL FLOOR SUPPORT AT FS 675. THE CRACKS WERE REMOVED AND THE DAMAGE REPAIRED PER ERA 396570-14AD AT HMV.SDR DL73K002450Keelbeam · crackedFUSELAGE / STRG. 18A SHEAR BEAM / FS 727 / LT & RT SIDES : CRACK REPAIRS THE WEB SECTION OF THE STRINGER 18A SHEAR BEAMS WERE FOUND CRACKED AT FS 727. THE RH BEAM CRACK IS 3 INCH LONG AND THE LT BEAM CRACK IS 1.5 INCH. THE CRACKS ARE SISDR DL73K002320Skin · crackedFUSELAGE / SKIN / AFT ENTRY DOOR OPENING / LWR HINGE CUTOUT:CRACK REPAIR THE LOWER HINGE CUTOUT OF THE AFT ENTRY DOOR OPENING SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. SDR DL73K002275Wire · shortedNR 2 ENG OIL TEMP IN YELLOW BAND. FOUND NR 2 FUEL HEAT VALVE C/B POPPED. FOUND WIRE 058-20 INSIDE FIREWALL CANNON PLUG SHORTED TO GROUND. REPAIRED SAME.SDR DL73K002264Fitting · corrodedTHE VERTICAL STABILIZER ATTACHMENT LUGS WERE FOUND CORRODED AT HMV. ERA 396368-14 REMOVES CORROSION FROM THE BORES AND FACES OF THE LUGS AND REINSTALLS THE BUSHING AND SLEEVES.SDR DL73K002260Door Frame · corrodedTHE FORWARD FRAME OF THE C2 DOOR OPENING WAS FOUND CORRODED ON THE AFT SURFACE UNDERNEATH THE DOOR LATCH FITTING. THE CORROSION WAS CUT OUT AND REPAIRED PER ERA 396463-14AD AT HMV.SDR DL73K002259Fitting · corrodedCORROSION WAS FOUND ON THE HORIZONTAL STABILIZER CLEVIS LUGS IN THE BORES AND FACES. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396374-14 AT HMV.SDR DL73K002258Fitting · corrodedCORROSION WAS REMOVED FROM THE HORIZONTAL STABILIZER ATTACH LUGS FROM THE BORE AND FACE. ERA 396375-14 REPAIRED THE AREA AT HMV.SDR DL73K002250Module · wornDISCOVERED SEVERAL CHAFED AND BROKEN WIRES IN A BUNDLE PASSING UNDER THE A/C POWER CONTROL BOX MOUNTED BEHIND THE PILOT''S OVERHEAD INST PANEL. REPAIRED ASSOCIATED WIRING AND REPLACED THE A/C POWER CONTROL PANEL. NO FAULTS WERE DETECTED IN FLT DISC FOUND WHSDR DL73K002245Switch · failedAFTER T/O CREW HAD SLAT INTRANSIT LIGHTS ON NR 2 AND NR 6 SLAT AFTER RETRACTION. REPLACED NR 2 SLAT ROD END SWITCH AND SLAT INDICATION BOX, ALL INDICATIONS NOW NORMAL.SDR DL73K002218Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK NEAR FS 520 AND STRINGER 16L. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM 53-30-3, FIG 1 AND ER/A 379238-14.SDR DL73K002206Wire · chafedON CLIMBOUT, NR 2 ENG OIL TEMP WENT TO 137 DEGREES. AFTER CYCLING FUEL HEAT VALVE TEMP WENT INTO THE RED. SHUT DOWN ENGINE. FOUND CONNECTOR PLUG WIRE ON FUEL HEAT VALVE CHAFED. REPLACED CONNECTOR PLUG.SDR DL73K002205Light · overheatedSTRONG RUBBER BURNING SMELL CAME FROM VENTS AROUND AFT ENTRY LIGHT IN REAR GALLEY AT CRZ FL290. SMELL COMING FROM AFT OVERHEAD ENTRY LIGHT. SMELL GONE WITH AFT ENTRY LIGHT OFF. PULLED AND SECURED CB B8 ON P18-3 PNL. FWD AND AFT ENTRY LIGHTS NOW INOP. FWD SDR DL73K002198Terminal · looseLEFT AISLE EMERGENCY LIGHTS (AFT 3 LAMPS) INOP. FOUND GROUND TERMINAL LOOSE. TIGHTENED SAME AND OPERATION NORMAL.SDR DL73K002190Skin · crackedDURING SHOP VISIT THE C-2 DOOR OUTER SKIN WAS FOUND DAMAGED. A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR HANDLE LATCH CUTOUT. REPAIRED PER ER/A 396879-14.SDR DL73K002189Connector · shortedAT DEPARTURE ELECTRICAL SMELL IN GALLEY. FOUND NR 2 COFFEEMAKER CANNON PLUG ARCING. TIED BACK BOTH C/P AND COLLARED C/B. CANNON PLUGS LATER REPLACED. NO FURTHER TROUBLE.SDR DL73K002157Line · rupturedSYSTEM A PRESSURE WENT TO ZERO AND BOTH PUMP LIGHTS ON, WHEN GEAR SELECTED DOWN. GEAR WAS MANUALLY EXTENDED. FOUND RUPTURED HYD LINE ON NR 2 ENG PYLON TO FIREWALL.SDR DL73K002153Floorbeam · crackedTHE BL 0.07 FLOORBEAM WAS FOUND CRACKED FROM FS 700 TO FS 717 IN THE WEB. THE DAMAGE WAS REMOVED AND REPAIRED PER B737 S/B 57-1210 AT HMV.SDR DL73K002151Floorbeam · crackedCRACKS WERE FOUND IN THE BL 0 FLOORBEAM WEB AND CHORD BETWEEN FS 650 AND FS 675. THE DAMAGE WAS REMOVED AND REPAIRED SIMILIARL TO THAT OF S/B 737-57-1210 PER ERA 396377-14 AT HMV.SDR DL73K002122Skin · puncturedTHE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT RESULTING IN TEARING AND GOUGING OF THE SKIN. THE DAMAGE WAS REMOVED WITH AN APPROX 20 X 7 INCH CUTOUT BETWEEN FS 896 AND 925 BETWEEN STRINGERS 19R AND 20R. THE SKIN BUTT SPLICE STRAP AT FS 907 WAS ALSO DAMAGESDR DL73K002113Power Supply · inoperativeON MTC CK FOUND R2 OVER DOOR EMERGENCY LIGHT AND AFT EXIT LOCATOR EMERGENCY LIGHT NOT ILLUMINATING ON TEST. REPLACED POWER SUPPLY.SDR DL73K002106Frame · crackedA CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT FS 616 FRAMES AT THE OVERWING FRAME TO BEAM JOINT STUB. ERA 396361-14 AUTHORIZES A REPAIR SIMILIAR TO THAT OF SB 737-53-1182 AT HMV.SDR DL73K002102Oxygen Mask · leakingF/O O2 MASK FAILED, CAUSING TOTAL DEPLETION OF CREW 02 SYSTEM. REPLACED F/O O2 MASK AND CREW OXYGEN BOTTLE.SDR DL73K002088Frame · wornTHE FS 440 FRAME HAS A WORN AREA AT THE FORWARD LOWER CORNER OF THE C1 DOORWAY. THE WEAR IS LOCATED ON THE VERTICAL WEB OF THE Z-FRAME. THE DAMAGE WAS BLENDED SMOOTH AND A REPAIR DOUBLER WAS INSTALLED PER ERA 396283-14 AT HMV.SDR DL73K002066Floorbeam · crackedCRACK INDICATIONS WERE FOUND ON THE BL 0.07 LONGITUDINAL FLOORBEAM BETWEEN FS 700 AND FS 717. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B737 S/B 57-1210 PER ERA 396272-14 AT HMV.SDR DL73K002065Floorbeam · corrodedTHE FS 294 FLOORBEAM WAS CORRODED ON THE UPPER CAP AT LBL 10 AND RBL 49. REPAIRED PER ERA 396233-14AD AT HMV.SDR DL73K002062Frame · crackedTHE FS 400 RT SIDE FRAME WAS FOUND CRACKED IN THE SKIN ATTACH FLANGE IN THE BEND RADIUS ADJACENT TO THE FIRST FASTENER ABOVE STR 14R. THE DAMAGE WAS TRIMMED OUT AND A REPAIR INSTALLED PER ERA 396241-14 AT HMV.SDR DL73K002057Attach Fitting · corrodedTHE RT AND LT HORIZONTAL STABILIZER ATTACH FITTINGS WERE FOUND CORRODED. MATERIAL WAS REMOVED FROM THE FACES AND THE BORES WERE OVERSIZED TO REMOVE CORROSION. THE DAMAGE WAS FOUND AT HMV.SDR DL73K002056Fitting · corrodedTHE RT HORIZONTAL STABILIZER CLEVIS LUG WAS FOUND CORRODED THE BORES WERE OVERSIZED AND SOME LOCAL BLENDED WAS APPLIED TO THE FACES PER ERA 396224-14 AT HMV.SDR DL73K002055Fitting · corrodedCORROSION WAS FOUND ON MULTIPLE LUGS ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE ATTACH LUGS. ALL CORROSION WAS REMOVED AND REPAIRED PER ERA 396259-14 AT HMV.SDR DL73K002053Frame · corrodedCORROSION WAS FOUND ON THE INBOARD CHORD OF THE FS 500B FRAME AT STR 25R. THE DAMAGE WAS REMOVED AND A FACTORY SPLICE EXTENDED TO REPAIR THE DAMAGE. THE DAMAGE WAS FOUND AT HMV.SDR DL73K002050Pcu · malfunctionedON T/O ROLL 125 KNOTS FELT A UNCOMMANDED YAW TO THE RIGHT, FELT LIKE SOMEONE KICKED THE RUDDER PEDAL. REPLACED RUDDER PCU PER M/M.SDR DL73K002017Actuator · intermittentAFTER STARTING NR 1ENG (NORMAL START) DURING TAXI OUT NR 1 ENG FLAMED OUT. ON RESTART ATTEMPT AT GATE, NO FUEL FLOW INDICATION AFTER START LEVER RAISED TO IDLE. REPLACED BAD FUEL SOV ACTUATOR AND GATE ASSY PER MM. RAN NR 1 ENG, ALL PARAMETERS GOOD.SDR DL73K002013Engine · inoperativeOIL FILTER BYPASS LIGHT ON AFTER TAKEOFF. NR 1 ENG SHUT DOWN. RETURNED TO MCI. OIL PRESSURE WAS NORMAL WHILE ENGINE RUNNING. ENGINE WINDMILLED ABOUT 30 MIN. METAL FOUND IN MAIN FILTER AND GEARBOX CHIP DETECTOR. REPLACED NR 1 ENGINE PER CARD DECK 3T213.SDR DL73K001970Unknown · odorPILOTS DETECTED A MELTING PLASTIC SMELL AT CRUISE (FL 330.7M) SMELL WAS INTERMITTENT AND FLT CREW WAS UNABLE TO DETERMINE THE SOURCE. EXECUTED PRECAUTIONARY, DIVERT TO ATL. FUMES/SMELL DID NOT REOCCUR AFTER INITIAL DESCENT INTO ATL. INSP PACK INLETS, INSP BSDR DL73K001955Line · damagedENGINE HYD PUMP NR 2 PRESSURE LIGHT ON SYSTEM. REPLACED NR 2 ENGINE HYD PUMP AND HYD PRESS LINE. REPLACED FILTERS AND INSP A SYSTEM RETURN MODULE, ALL NORMAL. FLUSHED LINES, NO CONTAMINATION FOUND. RAN ENGINES, CHECKS NORMAL.SDR DL73K001949Power Supply · inoperativeAT DEPARTURE FWD SECTION OF EMERGENCY LIGHTS WAS FOUND TO BE INOP. REPLACED DEFECTIVE POWER SUPPLY AND BATTERY.SDR DL73K001934Skin · crackedA 4 INCH CRACK IN FUSE SKIN STA 947.6 STR 26R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 16.SDR DL73K001911Light · inoperativeDURING MAINT TEST FOUND AFT SECTION AILSE ESCAPE LIGHTS INOP. REPAIRED SHORT TO GROUND IN FLOOR TRACK WIRING AT ROW 14. REPLACED M9221 LT PACK DUE TO BLOWN FUSE.SDR DL73K001897Coffeemaker · shortedFLT ATT REPORTED STRONG ELECTRICAL SMELL IN AFT GAL. TURNED OFF AFT GALLEY PWR IN COCKPIT SMELL WENT AWAY. FOUND SHORTED AFT NR 1 COFFEE DISPENSER. REPLACED SAME, CKS OK.SDR DL73K001893Skin · damagedTIME LIMITED REPAIR REMOVED AT THE AFT ENGRY DOOR LOWER HINGE CUTOUT AND NEW REPAIR INSTALLED WITH SOLID FASTENERS. ER/A 301124-14 REV C.SDR DL73K001896Skin · crackedTHE FUSELAGE SKIN AND BONDED DOUBLER WAS FOUND WITH A TYPICAL CRACK IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1 X 1.5 INCH CUTOUT. THE CUTOUT WAS LOCALLY REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STEEL TRISDR DL73K001895Skin · damagedSKIN AT AFT GALLEY DOOR LWR HINGE CUTOUT CRACKED. DAMAGE IS TRIMMED OUT AND REPAIRED. ER/A 300224-14 REV.ASDR DL73K001884Skin · crackedA 4 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN NEAR FS 520 AND STRINGER 16L. THE SKIN WAS CUT OUT TO REMOVE THE CRACK. THE CUT OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 378705-14.SDR DL73K001865Floorbeam · corrodedSTA 328 FLOORBEAM - PREVIOUS REPAIR CORROSION ON SURFACE TASK NR C53-107-02 OPN 58101AD NRC 416. FLOORBEAM REPAIRED PER SRM 53-10-9 FIG 9.SDR DL73K001850Valve · stuckNR 1 ENG ANTI-ICE COWL VALVE FAILED TO OPEN IN FLIGHT. REPLACED NR 1 ENG ANTI-ICE VALVE. GROUND OPS NML. LK CHECK GOOD.SDR DL73K001848Window · shortedAIRTURN BACK DUE TO UNIDENTIFIED ODOR IN COCKPIT. FOUND TERMINAL AND WIRE ON R2 SLIDING WINDOW OVERHEATED. REPLACED TERMINALS, WINDOW AND CONTROLLER. LEAKS CHECK AND OPERATIONAL CHECK GOOD. NO ODOR PRESENT.SDR DL73K001847Valve · stuckACRID ODOR IN COCKPIT DURING DESCENT, COULD NOT IDENTIFY SOURCE BUT VERIFIED BY ALL CREW MEMBERS DID NOT AFFECT CABIN AIR. ON GROUND AT GATE F/A REPORTS ODOR IN AFT GALLEY. FOUND 35 DEGREE VALVE ON LT PACK STICKING OPEN. REMOVED AND REPLACED 35 DEGREE VALVSDR DL73K001917Floorbeam · corrodedSTA 328 FLOORBEAM PREVIOUS REPAIR CORROSION ON SURFACE, TASK NR C53-107-02. REMOVED FASTENERS. TRIMMED BEAM AND PICKED UP HOLES. TREATED AND PAINTED PER SRM 53-10-9 PG 21. OK TO INSTALL. BEGAN INSTALLING REPAIR PER SRM 53-10-9 FIG 9. INSTALLED REPAIR PER
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