Boeing 737-247

Service difficulty reports · 1,009

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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 = '737247'
  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 DL73S040268Floor Support · fatiguedA CRACKED WAS NOTED IN THE BBL 0.07 LONGITUDINAL FLOOR SUPPORT AT BS 715. CRACKED REMOVED AND FLOOR SUPPORT REPAIRED PER ERA 386095-14AD.Mar 25, 2004 · N239WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73S040267Attach Fitting · corrodedCORROSION WAS NOTED ON THE LUGS OF THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR HINGE AND HOUSING FITTING. CORROSION REMOVED AND FITTINGS REWORKED IAW ERA 386232-14.Mar 25, 2004 · N239WA · Boeing 737247 · Horizontal Stabilizer, Attach FittingsSDR DL73S040266Skin · corrodedCORROSION WAS FOUND ON THE KEEL BEAM LOWER SKIN PANEL. LOWER SKIN PANEL WAS REPLACED PER ERA 386233-14.Mar 25, 2004 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040246Proximity Sensor · failedDISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR.Mar 18, 2004 · N242WA · Boeing 737247 · Leading Edge Slat Position Indicating SystemSDR DL73S040205Skin · damagedSCRIBE MARKS WERE NOTED BETWEEN BS 360 AND BS 540 ALONG S26L LAP JOINT IN THE LOWER SKIN. LAP JOINT WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386161-14.Mar 1, 2004 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040204Skin · damagedSCRIBE MARKS WERE NOTED BETWEEN BS 360 TO BS 540 AT THE S26R LAP JOINT. LAP WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386165-14.Mar 1, 2004 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040203Skin · dentedA TIME LIMITED REPAIR WAS REMOVED FROM BS 1025 NEAR S25R, NEARBY ADDITIONAL DAMAGE WAS NOTED (EG, DENTS AND GOUGES). DENTS AND GOUGES WERE CUTOUT AND A PERMANENT REPAIR INSTALLED PER ERA 386109-14.Mar 1, 2004 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040198Connector · shortedFLT ATTENDANT REPORTED EGG ODOR WHICH DEVELOPED INTO AN ELECTRICAL BURNING ODOR. ENGINES WERE OFF AND APU RUNNING WITH PACKS ON. FOUND ODOR EMINATING FROM AFT GALLEY COFFEE DISPENSER. REPLACED AND OPERATED BOTH DISPENSERS. FOUND NR 2 DISPENSER CONNECTOR SHFeb 28, 2004 · N238WA · Boeing 737247 · Equipment/Furnishings WiringSDR DL73S040177Bulkhead · canningTHE GORE WEB OF THE AFT PRESSURE DOME AT FS 1016 WAS FOUND WITH AN OIL CAN CONDITION BETWEEN STRINGER 2R & 3R NEAR THE OUTER -Y- CHORD OF THE DOME. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088605-14.Feb 19, 2004 · N380DL · Boeing 737247 · Fuselage Main, BulkheadSDR DL73S040175Attach Fitting · corrodedCORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORKED PER ERA 386225-14.Feb 19, 2004 · N239WA · Boeing 737247 · Empennage Flight Control Surfaces, Attach FittingsSDR DL73S040173Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A .25 INCH CRACK AT THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING (R2 DOOR). THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER. THE CUTOUT WAS REPAIRED WITH EXTERNAL STEEL REPAIR DOUBLER PER ERFeb 18, 2004 · N380DL · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040162Light · burnedWHILE WORKING MCO ON ANTI SKID LIGHTS STAYING ON DIM. FOUND WINDSHEAR AND ALTITUDE ALERT LIGHT ASSEMBLIES WITH ELECTRICAL BURNS AND ODOR. REPLACED ASSEMBLIES.Feb 17, 2004 · N376DL · Boeing 737247 · Flight Compartment LightingSDR DL73S040124Control Valve · inoperativeACFT WOULD NOT PRESSURIZE, AT FL190 CABIN ALT WARNING HORN SOUNDED. FOUND LEFT A/C PACK CONTROL VALVE FLUCTUATING. REPLACED SAME. ACFT PRESSURIZES NORMALLY.Feb 1, 2004 · N378DL · Boeing 737247 · Cabin Pressure Control SystemSDR DL73S040109Fitting · corrodedTHE BS 685 MLG SIDE STRUT SUPPORT FITTINGS ON BOTH THE LT & RT WERE FOUND WITH CORROSION IN THE LUG BORES. REMOVAL OF THE CORROSION RESULTED IN DECREASING THE LUG STRENGTH TO AN UNACCEPTABLE LEVEL. THE FITTING ON BOTH SIDES OF THE AIRCRAFT WERE REMOVED AND NJan 28, 2004 · N243WA · Boeing 737247 · Fuselage, Landing Gear Attach FittingsSDR DL73S040103Fitting · corrodedDURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLEVIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES REWORKED PER ERA 3860Jan 28, 2004 · N242WA · Boeing 737247 · Empennage Flight Control Surfaces, Attach FittingsSDR DL73S040101Fitting · corrodedDURING INSPECTION AND REWORK OF THE HORIZONTAL STABILIZER LUGS, SEVERAL LUGS WERE REWORKED BEYOND PUBLISHED LIMITS. CORROSION REMOVED AND LUGS REWORKED IAW ERA 386090-14AD.Jan 28, 2004 · N238WA · Boeing 737247 · Horizontal Stabilizer StructureSDR DL73S040100Skin · damagedSCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S10L LAP SPLICE BETWEEN BS 259 AND 291. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386027-14.Jan 28, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040099Frame · damagedBS 951 FRAME SUSTAINED DAMAGE IN THE RADIUS AT WL 203. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386060-14.Jan 28, 2004 · N238WA · Boeing 737247 · Fuselage Main, FrameSDR DL73S040098Keelbeam · corrodedCORROSION WAS NOTED AT BS 606 ON THE LWR SURFACE OF THE RIGHT KEELBEAM INBOARD FLANGE. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386066-14.Jan 28, 2004 · N238WA · Boeing 737247 · Fuselage Main, KeelSDR DL73S040097Beam · damagedDAMAGE INCURRED TO THE VERTICAL FLANGE OF THE LOWER CHORD AT RBL 63, IN THE BS 639 STUB BEAM. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386099-14.Jan 28, 2004 · N238WA · Boeing 737247 · Fuselage Main, StructureSDR DL73S040096Skin · damagedA GOUGE WAS NOTED ON THE UPPER SKIN LAP SPLICE AT S26R AT BS 440. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386070-14.Jan 28, 2004 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040095Skin · crackedDURING CROWN INSPECTION FOUR FASTENERS HOLES WERE NOTED WITH CRACK INDICATIONS. DISCREPANCIES WERE REPAIRED PER ERA 386057-14AD.Jan 28, 2004 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040085Skin · damagedSCRIBE MARKS WERE NOTED IN THE LWR SKIN AT LAP SPLICE LOCATED AT S14L BETWEEN BS 345 TO BS 360. SCRIBE MARKS REMOVED AND AREA REPAIRED PER ERA 088065-14.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040084Skin · corrodedCORROSION WAS NOTED IN THE FUSELAGE SKIN AT S27L BETWEEN BS 947.50 TO 967. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386110-14.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040083Beam · crackedA CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 386098-14.Jan 26, 2004 · N242WA · Boeing 737247 · Fuselage Main, StructureSDR DL73S040076Skin · damagedTHE LOWER SKIN OF THE STRINGER 10R LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 330-360. THE SCRIBED SECTION OF SKIN WAS CUT AND REMOVED. THE AREA WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386026-14.Jan 23, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040075Skin · damagedTHE LOWER SKIN OF THE STRINGER 14L LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360-540. THE LAP JOINT AND SCRIBE WERE COMPLETELY CUT OUT TO REMOVE ALL DAMAGE. THE AREA WAS RESTORED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040070Bulkhead · corrodedCORROSION WAS NOTED ON THE BS 1016 PRESSURE BULKHEAD, AT BL 0 AND AFFECTED BOTH THE WEB AND CHANNEL STIFFENERS. CORROSION WAS REMOVED AND DAMAGE REPAIRED PER ERA 385929-14.Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, BulkheadSDR DL73S040069Skin · damagedSCRIBE MARKS WERE FOUND AT THE LAP JOINT LOCATED AT S10R, BETWEEN BS 259 TO BS 290. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386028-14.Jan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040068Skin · damagedSCRIBE MARKS FOUND ON THE LOWER SKIN OF THE LAP SPLICE AT S10L, BETWEEN BS 908 TO 1016. A NEW SKIN PANEL IS TO BE INSTALLED. HOWEVER, THE NEW PANEL WAS NOTED TO HAVE DISCREPANCIES. THE SUBJECT SKIN PANEL WAS REWORKED AT BS 908, S-14L PER ERA 386020-14, IN OJan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040067Skin · damagedSCRIBE MARKS FOUND IN THE LOWER SKIN OF THE LAP SPLICE AT S10L BETWEEN BS 908 AND 1016. THE SKIN PANEL WAS BEING REPLACED. THE NEW PANEL WAS NOTED AS HAVING SEVERAL DISCREPANCIES FROM THE MANUFACTURER. DISCREPANCIES WERE NOTED ALONG THE S20L LAP AND WERE REJan 22, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040073Skin · damagedTHE LOWER FUSELAGE SKIN OF THE STRINGER 14L SKIN LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE LINE WERE REMOVED WITH A CUTOUT. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BJan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040072Skin · damagedTHE LOWER SKIN OF THE STRINGER 14R SKIN LAP JOINT WAS FOUND WITH A SCRIBE ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE WERE CUT OUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087866-14.Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040071Skin · damagedTHE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360 TO FS 540. THE SKIN LAP JOINT WAS CUT OUT TO REMOVE THE LAP AND THE SCRIBE MARK. THE AREA WAS THEN REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS Jan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040065Skin · damagedTHE LOWER SKIN PANEL AT THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 345 TO FS 360. THE LOWER SKIN WAS CUT BELOW THE SCRIBE AND THE DAMAGED SECTION REMOVED. THE CUT AND LAP JOINT WERE REPAIRED WITH 2 EXTERNAL ALJan 21, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040063Lap Joint · scratchedTHE LOWER SKIN OF THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE PANEL LENGTH FROM FS 540 - FS 727. THE LAP JOINT WAS DISASSEMBLED, INSPECTED, ALL DAMAGE MACHINED AWAY, RE-INSPECTED AND RE-ASSEMBLED. THE REPAIR WAS ACCOMPLISHED Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040062Skin · scratchedTHE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE LAP JOINT WAS UNFASTENED, SEPARATED, ALL DAMAGE REMOVED THROUGH MACHINING, AND THOROUGHLY INSPECTED TO ENSURE NO CRACKS OR Jan 20, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040054Lap Joint · scratchedINSPECTION OF THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT BETWEEN FS 727 & 908 REVEALED A SCRIBE LINE ALONG THE LENGTH OF THE PANEL. THE ENTIRE LAP JOINT ALONG THE PANEL LENGTH WAS CUT AND REMOVED AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAIJan 16, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040046Floorbeam · crackedDURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 665, BS 669 AND BS 673. DAMAGE WAS REPAIRED AS PER ERA 385959-14AD.Jan 16, 2004 · N236WA · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73S040043Skin · crackedDURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 559 & 579. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUJan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040041Skin · dentedDENTS WERE NOTED IN THE FUSELAGE SKIN AROUND L2 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386075-14.Jan 15, 2004 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040040Skin · damagedDENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14.Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040039Frame · damagedA DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REPAIRED PER ERA 386004-14.Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, FrameSDR DL73S040038Floorbeam · crackedDURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH. UPPER CHORD WAS CUT OFF AND A NEW SECTION SPLICED IN PER ERA 385945-14.Jan 15, 2004 · N236WA · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73S040033Spar · damagedRIGHT ELEVATOR REAR SPAR FOUND DAMAGED AT OUTBOARD END. REPAIR ACCOMPLISHED FROM ELEV STA 88 TO OUTBOARD END PER ER/A 426886-14.Jan 13, 2004 · N382DL · Boeing 737247 · Elevator, Spar/RibSDR DL73S040029Solenoid · failedDURING TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE AS PER THE CHECKLIST FLAP WERE RETRACTED TO 0 AND NO T/O WARNING HORN WAS NOTICED. REPLACED GEAR HANDLE INTERLOCK SOLENOID.Jan 12, 2004 · N380DL · Boeing 737247 · Landing Gear SelectorSDR DL73S040022Frame · crackedCRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRACKS INDICATIONS WERE REMOVED AND REPAIR INSTALLED PER ERA 385971-14.Jan 9, 2004 · N236WA · Boeing 737247 · Fuselage Main, FrameSDR DL73S040021Skin · dentedTHE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14.Jan 9, 2004 · N236WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S040020Skin · crackedTHE FUSELAGE SKIN IN THE KEEL AREA BETWEEN FS 661 & 727 WAS FOUND WITH CRACKS AT SEVERAL OF THE ACCESS CUTOUTS IN THE PANEL. THE CRACKING IS TYPICAL OF BAC S/B 737-53-1104. THE SKIN PANEL WAS REMOVED AND A MODIFIED PANEL MANUFACTURED AND INSTALLED. THE REPAJan 8, 2004 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73S031115Wire Harness · shortedON APPROACH, THE LEFT GEN TRIPPED. RT BUS ATTEMPTED TO PICK UP AND TRIPPED ALSO. DOWN TO STBY POWER. CREW DECLARED EMERGENCY. FOUND LT GENERATOR CABLE SHORTED. REPLACED GENERATOR FEEDER HARNESS.Dec 20, 2003 · N243WA · Boeing 737247 · Electrical Power System Wiring
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