Boeing 727-232
Service difficulty reports · 6,539
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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 = '727232' 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 = '727232' 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 DL72S961606Transverse Beam · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. REPAIRED PER ERA 303225-14AD.SDR DL72S960446Angle · crackedFOUND DURING E-1 LETTER CHECK, NR 7 SLAT ANGLE CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR DL72S960445Angle · crackedFOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK IN COVE ANGLE NR 1 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PG 5A.SDR DL72S960440Switch · defectiveWITH NR 1 AND NR 2 ENGINES RUNNING, STARTED NR 3 ENG AND THEN NR 2 FLAMED OUT. RESET FUEL SHUTOFF VALVE CIRCUIT BREAKER AND STARTED ENG, CONTRACT MTC CKD FUEL S/O VLV OPERATION. CKD ENG FOR FUEL LEAKS. CKD INTAKE/EXHAUST. ALL OK. STARTED ENG SEVERAL TIMESSDR DL72S960436Light · inoperativeFOUND EMERGENCY EXIT LIGHT INOP AT AFT LT DOOR IN EMERGENCY. REPLACED LIGHT ASSY.SDR DL72S960616Skin · damagedDURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGE TO OUTBOARD CORNER OF SKIN, APPROX 10 INCHES. REPAIRED PER SRM 57-50-3, FIG 5.SDR DL72S960442Rib · crackedDURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB JUST O/B OF THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0.SDR DL72S960441Rib · crackedDURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB AT THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0.SDR DL72S960437Web · crackedTWO LIGHTENING HOLES IN RT VERT WEB OF AFT AIR STAIR TORQUE BOX WERE FOUND WITH CRACKS ROUTED PAST LIMITS. FOUND AT D-2 LTR CHECK AND REPAIRED PER MM 53-11-0.SDR CAL960206Engine · failedIAH - FLT 1926 - THE NR 3 ENGINE THROTTLE BEGAN TO VIBRATE AT 1,200 FEET DURING CLIMB-OUT OF IAH. A STRONG VIBRATION WAS REPORTED IN REAR CABIN. THE NR 3 ENGINE POWER WAS REDUCED, BUT THE VIBRATION CONTINUED. A LOUD BANG ACCOMPANIED BY NR 3 ENGINE SHUTDOWN SDR DL72S960431P/D Valve · leakingDESCENDING INTO ROC, NR 2 ENG FAILED/FLAME-OUT. ATTEMPTED RESTART NOT SUCCESSFUL. PRIOR TO DESCENT NR 2 FUEL FLOW 1,000 LBS HIGHER THAN OTHERS AND IT USED 1,000 LBS MORE DURING FLT. FOUND FUEL LEAK AT P AND D VLV. REPLACED PACKING, RAN ENGINE AND LEAK CHECSDR DL72S960429Angle · crackedNR 3 L/E SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S960428Angle · crackedNR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S960427Angle · corrodedCORROSION AT UPSTOP ANGLE FWD OF FWD HINGE ACCESS PNL 3348L. REPAIRED BEAM PER M/M 53-30-1.SDR DL72L960434Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN, DOUBLER AND TRIPLER WERE FOUND CRACKED IN THE UPPER FWD CORNER OF THE R-1 DOOR CUTOUT. THE CRACK IS 0.5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. IN ACCORDANCE WITH FAA 8110-3 FORM, A TIME-LIMITED RSDR DL72L960418Mount Bracket · crackedFOUND DURING D-1 LETTER CHECK, .375 INCH CRACK AT NR 6 L/E FLAP ACTUATOR MOUNT BOX UPPER O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.SDR DL72L960417Skin · crackedA 1.5 INCH CRACK AT MAIN ENTRY DOOR CUTOUT, OUTER SKIN AT UPPER HINGE CUTOUT. FOUND AT A-2 LTR CHECK. REPAIRED PER MM 53-30-0 PG 11.SDR DL72K960489Frame · crackedFOUND ON MV1 CHK L-2 DOOR S/N 1097 HAS .50 INCH CRACK AT FWD FRAME UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40-2, FIG 4.SDR DL72S960402Angle · crackedFOUND DURING A-1 LETTER CHECK, ANGLE CRACKED NR 7 SLAT O/B TRACK SUPPORT BOX I/B ANGLE. ANGLE CRACKED NR 6 SLAT I/B TRACK SUPPORT BOX I/B ANGLE. REPLACED ANGLES PER M/M 57-20-21 PG 813.SDR DL72S960399Frame · crackedFOUND DURING A-1 LETTER CHECK, .5 INCH CRACK IN LT MLG UPLOCK FRAME O/B FLANGE AT STA 910 UPPER END OF RADIUS BLOCK. REPAIRED PER MM 53-11-0.SDR DL72S960398Rib · crackedA .5 INCH CRACK PAST PREVIOUS STOP DRILL, LOWER O/B SIDE OF NR 4 SLAT NOSE RIB AT ACTUATOR ATTACH. A .375 INCH CRACK UPPER O/B SIDE OF NR 4 L/E SLAT NOSE RIB AT ACTUATOR ATTACH. REPAIRED PER MM 57-54-0.SDR DL72S960397Bracket · crackedA .4375 INCH CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BRACKET I/B UPPER CORNER. REPAIRED PER MM 57-20-21 PAR 12.SDR DL72S960396Skin · crackedA 1 INCH CRACK AT CENTER ENGINE INLET HOUSING OUTER SKIN BELOW PANEL 9523. REPAIRED PER MM 54-30-0.SDR DL72L960414Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 870 AND STR 9R. THE CUT OUT MEASURES 5 INCHES BY 3 INCHES, IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3A, A DOUBLER AND TRIPLER WERE INSTALLED.SDR DL72L960401Bracket · crackedFOUND DURING D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER MM 57-20-21.SDR DL72L960400Web · crackedFOUND DURING D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER MM 53-11-0 PG 828.SDR DL72K960443Rib · crackedUPON ROUTINE INSPECTION, THE I/B ACTUATOR RIB WAS FOUND TO BE DAMAGED. REPAIR WAS ACCOMPLISHED PER THE 727 M/M 57-54-0 FIG 804, FOR NR 8 L/E SLAT.SDR DL72S960552Rib · crackedDURING INSPECTION, NR 4 L/E SLAT INTERNAL SUPPORT RIB NR 5 AND NR 17 WERE FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S960551Skin · crackedDURING INSPECTION, NR 4 L/E SLAT UPPER SKIN WAS FOUND CRACKED SEVERAL PLACES UNDER THE WING FENCE. REPAIRED SKIN PER MM 57-54-0.SDR DL72S960389Rib · crackedDURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0.SDR DL72S960385Skin · crackedDURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813.SDR DL72L960405Bracket · crackedFOUND ON D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-0-21 PG 811.SDR DL72L960404Web · crackedFOUND ON D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0 PG 828.SDR DL72L960390Skin · crackedDURING INSPECTION, LEFT WING O/B AILERON WAS FOUND WITH LOWER OUTBOARD SKIN CRACKED. REPAIRED PER MM 57-51-0 PG 801.SDR DL72S960370Hprsov · malfunctionedON DECENT AT ABOUT 9K, STRONG DUSTY ELEC SMELL IN AFT ENTRY AREA. THE WING AND ENGINE HEAT OFF. DEACTIVATED GALLEY POWER AND LAV FLUSH MOTORS AS PRECAUTION. INSPECTED AND OPERATED SYSTEMS, UNABLE TO DUPLICATE. SUBSEQUENT OCCURENCE ISOLATED PROBLEM TO HIGHSDR DL72S960369Air Distr · odorDURING FINAL APPROACH, FLT ATTN NOTICED BURNING SMELL LIKE FIREWORKS, AROUND LT AFT LAV AREA. MTC POWERED A/C, TURNED ON ALL GALLEY AND LAV EQUIPMENT AND WAS UNABLE TO REPRODUCE ANY NOTICEABLE SMELL.SDR DL72S960367Bell Crank · wornPILOT REPORTS, AT 230 KTS A LOUD VIBRATION WAS HEARD FROM THE F/O WINDOW AREA DURING CLIMBOUT AND AT 220 KTS DURING DECEL THE VIBRATION STOPPED. REPLACED THE RIGHT HAND OUTBOARD AILERON TRIM TAB BELL CRANK, WHICH WAS FOUND TO HAVE OBLONGED MOUNT HOLES. RIG CSDR DL72S960364Oven · failedALL 3 FWD FACING OVENS IN AFT GALLEY WERE SMOKING AND EMITTING AN ELECTRICAL/CHEMICAL ODOR. THEY WERE NOT USEABLE.SDR DL72S960351Valve · stickingAT 18,000 FT CABIN CLIMB 1000 FPM, STANDBY AND MANUAL NO HELP. MADE EMERGENCY DESCENT TO 11,000 FT. FOUND RT PACK VALVE STICKING CLOSED. REPLACED SAME, OPS CKS. REMOVED BOTH WATER SEP BAGS, NO OBSTRUCTIONS FOUND. REINSTALLED PRESSURIZATION, CHECK NORMAL.SDR DL72K960345Skin · crackedDURING SHOP VISIT, INNER TAI SKIN CRACKED BETWEEN RIBS NR 11 AND NR 12 AT AFT RIVET TAIL. REPAIRED PER MM 57-54-0 FIG 803A, FOR NR 2 L/E SLAT.SDR DL72S960340Cadc · failedAFTER TAKEOFF, TCAS DISPLAYED ALL FAILED AND MAIN TCAS SCREEN SHOWED NR 1 XPONDER DATA BUS AND ALT DATA. CENTER ADVISED THEY RECEIVED SQUAWK, BUT NO ALT READOUT. AT FL 310 LEVEL OFF AND CRUISE MACH .80, A/C BEGAN MILD DUTCH ROLL. ROLL CEASED WHEN SPEED SLOWSDR DL72K960338Skin · crackedDURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED TAI SKIN. REPAIRED SKIN PER MM 57-54-0 FIG 803.SDR DL72K960337Rib · crackedDURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED RIB. REPAIRED PER MM 57-54-0.SDR DL72L960344Skin · gougedDAMAGE WAS FOUND ON THE UPPER TORQUE BOX SKIN DUE TO AN UNCONTAINED ENGINE FAILURE. THE DAMAGED SKIN SECTIONS WERE REMANUFACTURED AND REPLACED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 12 FEB 96.SDR DL72L960332Stiffener · crackedFOUND DURING B-1 LETTER CHECK - 1 INCH CRACK LWR END SPAR STIFFENER AT NR 6 L/E SLAT I/B TRACK I/B ANGLE. REPLACED PER MM 57-20-21.SDR DL72L960331Angle · crackedFOUND DURING B-1 LETTER CHECK - .50 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTATCH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72L960330Angle · crackedATTACH ANGLE BROKEN NR 1 L.E. FLAP ACTUATOR BOX. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21.SDR DL72S960352Te Wedge · dentedNR 5 L/E SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER SRM 57-43-02.SDR DL72K960342Floorbeam · corrodedFOUND ON MV1 CHECK, CORROSION SEVERAL PLACES FLOORBEAM STA 344. REPAIRED PER SRM 53-10-8 FIG 11.SDR DL72S960316Light · inoperativeAIRSTAIR COMPARTMENT EMERGENCY LIGHT IS INOP DURING TEST. REPLACED LIGHT ASSY, CHECKS GOOD.
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