Boeing 737-228
Service difficulty reports · 371
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 = '737228' 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 = '737228' 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 PIDA20050080Pan · corrodedDRIP PANS AT BS 1016 HAVE CORROSION FROM LBL 45 TO RBL 45. REPLACED LEFT AND RIGHT DRIP PANS PER SRM 51-10-1 AND SRM 51-30-0.SDR PIDA20050074Stringer · corrodedCORROSION ON STRINGER 27 LT JUST AFT OF BS 967 FRAME. SPLICED IN NEW SECTION OF STRINGER P/N 65-51628-29 FROM BS 917 TO BS 1016 PER SRM 53-10-3.SDR PIDA20050072Stringer · corrodedCORROSION ON STRINGER 27 LT AT THE AFT END AT BS 360. REPAIRED PER SRM 53-10-3.SDR PIDA20050096Fitting · crackedAFT ANGLE FOR AFT APU DOOR HINGE CRACKED. REPLACED FITTING AND ATTACH ANGLES PER DWG 65-54838.SDR PIDA20050094Intercostal · corrodedDIAGONAL INTERCOSTAL AND OVERLAPING WEB HAVE CORROSION FROM BS 1006 TO BS 1016 AT LBL 4. REPLACED CORRODED SHIM OF INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050093Intercostal · corrodedINTERCOSTAL WEB AND STRAP HAVE CORROSION AT ATTACH FASTENER AT BS 1006 FLOORBEAM AT LBL 26. REPLACED WEB AND STRAP PER DWG 65-46812 AND SRM 51-10-1 AND SRM 51-10-2.SDR PIDA20050098Support Bracket · corrodedBLEED AIR DUCT SUPPORT BRACKET AND ATTACH ANGLES AT BS 1016 AT LBL 12 HAVE CORROSION. REPLACED DUCT SUPPORT BRACKET AND ANGLES PER SRM 51-10-1.SDR PIDA20050081Channel · corrodedHAT CHANNEL FROM BS 1026 TO BS 1030 AT BL 0 IS CORRODED. REPLACED CHANNEL PER DWG 65-46816 AND SRM 51-10-1 AND SRM 51-30-0.SDR PIDA20050101Intercostal · corrodedINTERCOSTAL FROM BS 1016 TO BS 1040 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050097Mount · crackedSHELF THAT RADAR T/R RACK MOUNTS TO HAS A CRACK IN BOTH AFT CORNERS. REPAIRED MOUNT ANGLES PER SRM 51-40-3.SDR PIDA20050100Intercostal · crackedINTERCOSTAL FROM BS 500A TO BS 500B AT STR 26 RT IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41757 AND SRM 51-10-1.SDR PIDA20050102Web · corrodedWEB IN RIGHT SIDE OF FWD CARGO BIN IS CORRODED FROM BS 500B TO BS 520. REPLACED CORRODED WEB PER DWG 69-41757-504 AND SRM 51-10-1.SDR PIDA20050106Strap · crackedSONIC VIBRATION STRAP AT LBL 11 AT BS 330 IS CRACKED. REPAIRED STRAP PER SRM 53-10-9.SDR PIDA20050103Angle · corrodedTRANSITION ANGLE IN FWD CARGO BIN IS CORRODED FROM BS 500A TO BS 520. REPLACED TRANSITION ANGLE PER SRM 51-10-1.SDR PIDA20050084Seat Track · corrodedSEAT TRACK AT RBL 42 HAS CORROSION ON O/B FLANGE AT BS 280. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1.SDR PIDA20050083Seat Track · corrodedSEAT TRACK AT RBL 15 HAS CORROSION ON FLANGES FROM BS 269 TO BS 294. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1.SDR PIDA20050082Seat Track · corrodedSEAT TRACK AT RBL 52 HAS CORROSION ON FLANGES FROM BS 328 TO BS 360. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1 AND SRM 51-10-2.SDR PIDA20050091Intercostal · corrodedINTERCOSTAL AT LBL 11 BETWEEN BS 294 AND BS 312 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050086Intercostal · corrodedINTERCOSTAL FROM RBL 16 TO RBL 31 AT BS 298 HAS CORROSION ON TOP SURFACE. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050099Angle · corrodedZ-ANGLE AT R-1 DOOR HAS CORROSION AT FASTENER HOLES. REPLACED Z-ANGLE PER SRM 51-10-1.SDR PIDA20050107Intercostal · corrodedINTERCOSTAL AT LBL 11 IS CORRODED AT THE NUT PLATE HOLES FROM BS 328 TO BS 344. REPLACED INTERCOSTAL SHIM PER SRM 51-10-1.SDR PIDA20050088Intercostal · corrodedINTERCOSTAL AT RBL 11 BETWEEN BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050087Intercostal · corrodedINTERCOSTAL AT LBL 11 FROM BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050075Floorbeam · corrodedBS 294 FLOORBEAM HAS CORROSION FROM LBL 28 TO RBL 45 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9.SDR PIDA20050090Intercostal · corrodedINTERCOSTAL AT BS 320 BETWEEN RBL 30 AND RBL 56 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1.SDR PIDA20050089`Intercostal · corrodedINTERCOSTAL AT BS 320 BETWEEN RBL 11 AND RBL 29 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1.SDR PIDA20050073Stringer Clip · corrodedCORROSION ON STRINGER 27 LT ATTACH CLIP AT BS 540 FRAME. REPAIRED PER DRAWING 65-49564 AND SRM 51-10-1.SDR PIDA20050104Floorbeam · corrodedFLOORBEAM IN AFT CARGO BIN AT RBL 5 HAS CORROSION AROUND NUT PLATE HOLE AT BS 787. REPAIRED DAMAGED AREA OF UPPER LEG PER SRM 51-40-3.SDR PIDA20050105Clip · corrodedFLOORBEAM ATTACH CLIP AT BS 867 AT LBL 8 IN AFT CARGO BIN IS CORRODED. REPLACED ATTACH CLIP PER SRM 51-10-1.SDR PIDA20050077Floorbeam · corrodedBS 328 FLOORBEAM HAS CORROSION FROM LBL 15 TO RBL 57 AT FASTENER HOLES. SPLICED IN NEW SECTION OF FLOORBEAM T-CAP FROM LBL 35 TO RIGHT O/B END PER SRM 53-10-9.SDR PIDA20050076Floorbeam · corrodedBS 312 FLOORBEAM HAS CORROSION FROM LBL 20 TO RBL 20 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9.SDR PIDA20050018Wire · damagedYAW DAMPER DISENGAGED DURING FLIGHT AND WILL NOT RE-ENGAGE. PLACED YAW DAMPER ON MEL 22-3-16. REPAIRED BROKEN WIRE PER SWPM 20-30-13. OPS CHECK GOOD PER MM 22-12-01SDR 252TR0037Coupler · damagedYAW DAMPER IS INOP. PLACED ON MEL 22-3. REPLACED YAW DAMPER COUPLER PER MM 22-11-141. OPS AND BITE CHECK OK.SDR 237TR0010Computer · malfunctionedTHE A-AUTO PILOT WILL NOT ENGAGE IN CWS OR CMD. PLACED A-AUTO PILOT ON MEL 22-1. 03/17/2005: REPLACED A-SYSTEM AFCS PER MM 22-11-331. OPS CHECKS GOOD.SDR 237TR0009Indicator · inoperativeNR 1 FLIGHT DIRECTOR INOP. PLACED ON MEL 34-12. 03/14/2005: REPLACED NR 1 ADI AND OPS CHECKED PER MM 22-11-01.SDR PIDA250021ASupport Angle · corrodedCORROSION AROUND THE FORWARD LAVATORY DUMP VALVE, I/B SIDE. REPLACED CORRODED SUPPORT ANGLE PER BAC DWG 65-55757 AND SRM 51-10-2.SDR 252TR0036Wire · brokenBOTH EMERGENCY EXIT LIGHTS IN G-2 GALLEY AREA AT FORWARD ENTRY DOOR AISLE INOP. REPAIRED BROKEN WIRES UNDER GALLEY PER SWPM 20-00. OPS CHECKS OK.SDR 252TR0035Panel · crackedLEFT ENGINE O/B COWL EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975.SDR 252TR0034Panel · crackedRIGHT ENGINE I/B COWLING EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975.SDR 252TR0033Fairing · crackedRIGHT ENGINE O/B THRUST REVERSER FAIRING CRACKED AT THE I/B AFT END. WELDED PER BAC SPEC 5975.SDR 252TR0032Attach Bracket · crackedRIGHT RAM AIR DUCT FORWARD UPPER O/B ATTACH BRACKET CRACKED. REPLACED ATTACH BRACKET PER SRM 51-10-2 AND 51-40-03.SDR 252TR0031Intercostal · crackedINTERCOSTAL ATTACH ANGLE CRACKED UNDER RIGHT TRANSITION ANGLE AT BS 947. REPLACED ATTACH ANGLE PER SRM 51-10-2.SDR 252TR0029Skin · corrodedCORROSION AROUND THE FORWARD LAVATORY DUMP VALVE, I/B SIDE. REPLACED CORRODED SUPPORT ANGLE PER BAC DWG 65-55757 AND SRM 51-10-2.SDR 252TR0028Skin · corrodedCORROSION IN LOWER SKIN AT STR 27 LT BETWEEN BS 500A AND BS 500B AND DAMAGE IN KEEL BEAM RUN-OUT AREA. REPAIRED PER EA 53-031.SDR 234TR0027Computer · malfunctionedNUMBER 2 ADI HAS FLIGHT DIRECTOR FLAG. REPLACED NR 2 FLIGHT CONTROL COMPUTER. OPS CHECKS GOOD PER MM 22-11-01.SDR 251TR0012Battery Pack · inoperativeEMERGENCY EXIT LIGHTS OUTSIDE OF L1 DOOR AND ABOVE L2 DOOR INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD PER MM 33-51-81.SDR 237TR0008Switch · malfunctionedFLIGHT DIRECTOR BAR GOES AWAY WHEN TOGA IS PRESSED. PLACED ON MEL 22-17. 12/08/2004: REPLACED SWITCH IN RIGHT HAND THROTTLE. FLIGHT DIRECTOR OPS CHECKS GOOD PER MM 22-11-01.SDR 234TR0024Skin · damagedREMOVED FUSELAGE SKIN FROM BS 1016 TO 1033 FROM STR 26 RT TO 26 LT FOR ACCESS TO BS 1016 BULKHEAD REPAIRS. REPAIRED FUSELAGE SKIN PER SB 737-53A1075. REPAIRS TO THE BS 1016 BULKHEAD THAT REQUIRED REMOVAL OF FUSELAGE SKIN ARE REPORTED ON UNIQUE CONTROL NR 234SDR 234TR0026Stringer · corrodedCORROSION ON STR 28 LT FROM BS 985 TO BS 1016. REPAIRED DAMAGED SECTION PER SRM 53-10-3.SDR 234TR0025Stringer · corrodedCORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED DAMAGED SECTION PER SRM 51-10-1 AND SRM 51-40-04.
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