Boeing 737-347
Service difficulty reports · 359
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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 = '737347' 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 = '737347' 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 DL733021124Frame · crackedA CRACK WAS FOUND IN THE OUTER CHORD OF THE FS 727 FRAME AT STR 14L. THE .8 INCH CRACK WAS CUT OUT AND THE FRAME WAS REPAIRED WITH A .090 7075-T6 ANGLE. THE DAMAGE WAS FOUND ATHMV.SDR DL733021102Fitting · corrodedCORROSION WAS FOUND ON THE AFT FACE OF THE NR 3 LUG AND THE FORWARD FACE OF THE NR 6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUG. THE BUSHINGS WERE REPLACED WITH THICKER FLANGESSDR DL733021087Fitting · corrodedCORROSION WAS FOUND ON THE RT INBOARD LUG BORE ON THE HORIZONTAL STABILIZER CENTER SECTION UPPER FITTING. THE BORE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL733021065Beam · wornWORN AREAS WERE FOUND IN THE CROWN BEAM LUG BORES ON THE NR 1 AND NR 2 PYLONS. THE WORN AREAS WERE REMOVED BY OVERSIZING THE LUG BORES ON THE NR 1 AND NR 2 PYLON. OVERSIZED BUSHINGS WERE INSTALLED IN THE BORES. THE DAMAGE WAS FOUND AT HMV.SDR DL733021056Skin · delaminatedWING SPOILERS WAS FOUND WITH EXCESSIVE DELAMINATION. REPAIR PER ER/A 417560-14 AND NORDAM EWO E0038848.SDR DL733021059Skin · delaminatedRT WING INBOARD MID FLAP WEDGE IS DISBONDED. REPAIR PER ER/A 417696-14.SDR DL733021057Wedge · damagedDAMAGE TO LT WING INBOARD MID FLAP WEDGE. REPAIR PER ER/A 417684-14.SDR DL733020892Smoke Detector · faultyLAV SMOKE AMBER LIGHT AND CHIME CAME ON DURING CRUISE FLIGHT. ALL LAVS CHECKED WITH NO SIGN OF SMOKE, FUMES, EXCESSIVE HEAT. CIRCUIT BREAKER PULLED TO SILENCE CHIME. FOUND AFT RT DETECTOR INOP. REPLACED DETECTOR, OPS CHECKS GOOD.SDR DL733020877Engine · overtempON TAKEOFF (NORMAL POWER) CLIMBOUT BOTH ENGINE INDICATIONS SHOWED RED LIGHT ILLUMINATED ON DIGITAL READOUT AT 970 DEGREES (C) PLUS ON BOTH ENGINES AT LEAST 5 SECONDS. N1 INDICATES AT ABOUT 96.6. PULLED BACK THROTTLES, RED LIGHT EXTINGUISHED. REMOVED AND REPSDR DL733020874Transmitter · malfunctionedDURING FLAP EXTENSION RIGHT FLAP IND REMAINED NEAR ZERO AND LEFT INDICATED NEAR ONE DEGREE. L/E INDICATIONS NORMAL. FOLLOWED QRH PROCEDURES AND LANDED AT 170 KIAS. REPLACED RIGHT T/E FLAP POSITION TRANSMITTER, OPS NORMAL.SDR DL733020870Skin · crackedDURING INSPECTION PER OPN 57512 SKIN CRACK WAS FOUND AT STATION 727E+15 AND STRINGER 23L. CORRECTIVE ACTION: REPAIRED PER ER/A 383585-14.SDR DL733020869Skin · crackedDURING INSPECTION PER OPN 57512 CRACK WAS FOUND IN THE SKIN AT STATION 727D+15 AND STR-22R. CORRECTIVE ACTION: REPAIRED PER ER/A 383586-14.SDR DL733020812Hydraulic Line · rupturedLOSS OF B-SYSTEM PRESSURE IN FLIGHT. REPLACED B-PUMP HYD SUPPLY LINE IN RT WHEEL WELL . ALSO REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAIN FILTER SYSTEM, OPS AND LEAKS CHECKS NORMAL.SDR DL733020630Skin · dentedTWO LARGE DENTS WERE FOUND IN FUSELAGE SKIN BETWEEN STA 907 AND 957 AND S-20R AND 25R. THERE WAS ALSO AN EXISTING REPAIR IN THE AREA. THE DAMAGED SKIN AREA WAS TRIMMED AWAY AND EXISTING REPAIR REMOVED. A NEW SECTION OF SKIN WAS SPLICED IN AT FS 957 FORWARD SDR DL733020631Skin · damagedA NEW SECTION OF SKIN WAS SPLICED IN FROM FS 907 TO 957 AND S-20R TO 25R PER ER/A 383228-14. A SECTION OF THE LOWER SKIN WAS FOUND TO BE ROUTED OUT IN THE LAP SPLICE AREA AT APPROXIMATELY FS 935 AND S-25R. AFTER INSTALLATION OF THE NEW UPPER SKIN, THE LOWER SDR DL733020608Proximity Sensor · faultyFWD CARGO DOOR LIGHT CAME ON DURING T/O AT 130 KTS. CONTINUED T/O AND RETURNED TO AIRPORT. CARGO DOOR IND LIGHT INTERMITTENT. REPLACED FWD CARGO DOOR SENSOR PER M/M, DOOR IND OPS NORMAL.SDR DL733020424Wire · disconnectedEMERGENCY EXIT LIGHT ON SEAT 12D INOP. FOUND WIRES PULLED FROM CONNECTOR. REWIRED CONNECTOR, LIGHT OPNS NORMAL.SDR DL733020423Skin · delaminatedOUTBOARD SPOILER UPPER SKIN WAS FOUND DELAMINATED. REPAIR PER ER/A 411175-14 AND NORDAM EWO E0037508 REV I/R.SDR DL733020391Beam · corrodedCORROSION WAS FOUND ON THE CROWN BEAM LUG BORES ON THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO REMOVE THE CORROSION AND REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL733020358Skin · delaminatedUPPER SKIN OF THE OUTBOARD SPOILER WAS FOUND DELAMINATED IN TWO AREAS. REPAIR PER ER/A 411104-14 NORDAM EWO E0037119 REV I/R.SDR DL733020337Attach Fitting · wornA BEARING WAS FOUND MIGRATED FROM THE LUG BORE OF THE AFT FITTING ON THE NR 2 PYLON CROWN BEAM. AFTER REMOVAL OF THE BEARING LIGHT GOUGES WERE FOUND IN THE LUG BORE. THE LUG WAS REAMED TO A LARGER DIAMETER, A STEEL REPAIR BUSHING INSTALLED, AND A NEW BEARINGSDR DL733020307Actuator · leakingNR 1 ENGINE LOW PRESSURE HYDRAULIC (A) SYSTEM LIGHT ILLUMINATED WITH ASSOCIATED A SYSTEM QUANTITY DECREASED TO ZERO. FOLLOWED POM PROCEDURE NO OTHER INDICATION. MADE UNEVENTFUL LANDING. REPLACED O-RING AND FITTING ON A SYSTEM AILERON AUTOPILOT CONTROL ACTUASDR DL733020273Attach Fitting · corrodedTHE VERTICAL STABILIZER ATTACH LUGS AND THE FUSELAGE CLEVIS LUGS WERE FOUND TO BE CORRODED DURING AN INSPECTION. THE LUG BORES WERE OVERSIZED AND THE FACES SPOTFACED TO REMOVE THE CORROSION AND OVERSIZED BUSHINGS WERE INSTALLED.SDR DL733020272Wire · shortedSPARKS COMING FROM SIDEWALL AT SEAT 1A. FOUND WIRING TO SIDEWALL LIGHTING SHORTED TO INSULATION HOLD DOWN CLAMP. REPINNED CONNECTOR TO LIGHT, OP CHECKS NORMAL.SDR DL733020227Power Supply · inoperativeL2 DOOR AND AFT AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY.SDR DL733020135Door Frame · crackedFWD CARGO DOOR ARRIVED IN THE SHOP DUE TO CRACKING FOUND IN THE LOWER FWD AND AFT CORNER FRAMES AS WELL AS THE FWD AND AFT SECTIONS OF THE LWD STOP BEAM. REPAIR PER ER/A 410793-14AD.SDR DL733020122Keelbeam · crackedCORROSION WAS FOUND ON THE LOWER KEEL CHORD AT FS 727 AND STR 27R. ADDITIONALLY, SEVERAL WEAR LOCATIONS WERE FOUND BETWEEN FS 727 AND FS 715 AND A CRACK WAS FOUND ON THE AFT END OF THE PART AT FS 727A. THE CORROSION WAS BLENDED AND THE CRACK WAS CUT OUT AND SDR DL733020121Web · crackedTHE KEEL BEAM LOWER SKIN PANEL WAS FOUND CRACKED IN SEVERAL PLACES_BETWEEN FS 661 AND FS 721. THE PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV.SDR DL733020062Support Fitting · damagedFWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410877-14AD.SDR DL733020061Support Fitting · damagedFWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410878-14AD.SDR DL733020059Beam · corrodedCORROSION WAS FOUND ON THE CROWN BEAM LUG BORES OF THE NR 1 AND NR 2 PYLONS. THE BORES WERE OVERSIZED AND REPAIR BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV.SDR DL733020003Compressor · stalledON CLIMBOUT, LOUD THUMP FOLLOWED BY COMP STALL WITH RED EGT LIGHT AND ZERO OIL QTY ON NR 2 ENGINE. REPLACED ENGINE.SDR DL733011991Pin · out of adjAT CRUISE ALTITUDE L-1 DOOR HANDLE POPPED UP APPROX .5 INCH. FOUND DOOR STOP PINS AND GATE UPPER AND LOWER RODS OUT OF ADJUSTMENT. RIGGED BOTH PER MM, PRESSURIZED ACFT TO 7.0 PSID, WITH CABIN PRESSURE ON UNABLE TO MOVE HANDLE.SDR DL733011958Bear Strap · crackedAT FS 795 AT THE LWR FWD CORNER OF THE C-2 DOOR, A 1 INCH CRACK WAS FOUND IN THE BEARSTRAP. IN ADDITION AN EXISTING SKIN REPAIR NEAR STR 23R. THE EXISTING REPAIR IS FOR A CUTOUT IN THE SKIN AND BEARSTRAP. THE BEARSTRAP CRACK WAS GROWING FROM EXISTING EDGE DSDR DL733011903Spar · crackedFORWARD SPAR DAMAGED AT THE CUTOUT FOR THE EXHAUST GATE ACTUATOR ROD. DAMAGE CAUSED BY INSTALLATION OF INCORRECT ARM THAT MADE THE ROD TOO HIGH AND BOLT ATTACHING ROD TO ARM CONTACT THE SPAR.SDR DL733011881Spar · crackedTHE NR 3 MID FLAP FRONT SPAR UPPER CHORD AND WEB WERE FOUND DAMAGED. REPAIRED PER ER/A 410644-14.SDR DL733011754Sensor · dirtyCLIMBING THRU 4000 FT FWD CARGO LIGHT ILLUMINATED. RETURNED FOR LANDING. MAINTENANCE CONFIRMED DOOR CLOSED AND LOCKED. CLEANED FWD SENSOR OF FOREIGN SUBSTANCE, OP CHECKS GOOD.SDR DL733011709Gcu · failedAPU OVERSPEED, NR 1 GEN WAS ALREADY ON MCO. RESET OVERSPEED ON APU ACCY UNIT. APU WORKS NORMAL. REPLACED NR 1 GCU NR 1 GEN WORKS NORMAL.SDR DL733011509Battery · dischargedLWR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT INOP. REPLACED BATTERY AND BRACKET.SDR DL733011494Skin · misdrilledFUSELAGE / SKIN / FS 178 / STRG. 19R : REPAIR OF MISDRILLED HOLES SEVERAL MISSDRILLED HOLES WERE FOUND IN THE FUSELAGE SKIN AT FS 178 NEAR STRINGER 19R DURING ACCOMLISHMENT OF THE FS 178 BULKHEAD MODISDR DL733011450Skin · gougedFUSELAGE / SKIN / FS 907-1156 / STRG. 25L-25R : TAIL STRIKE REPAIR THE FUSELAGE SKIN SUFFERED A TAIL STRIKE ON TAKEOFF WHICH RESULTED IN MULTIPLE GOUGES, SCRAPES, AND HOLES IN THE FUSELAGE SKIN FROM FSDR DL733011409Tire · separatedNR 1 MAIN TIRE TREAD SEPARATED FROM TIRE ON TAKE OFF. DAMAGING LEFT I/B FLAPS AND LEFT GEAR DOOR. CA REPLACED TIRE, GEAR DOOR AND REPAIRED FLAP DAMAGE.SDR DL733011356Safety Switch · out of adjUPON DEPARTURE ATL LDG WOULD NOT RETRACT. GEAR HANDLE WOULD ONLY RAISE TO THE OFF POSITION. ADJUSTED AND TESTED GROUND SPOILER INTERLOCK AND SAFETY SWITCHES. REF MM 27-62-51-5 AND E2-09-01-5. ALL CHECKS OK.SDR DL733011306Mec · failedNR 1 ENGINE FAILED TO REACH TAKEOFF ON TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 65 KTS. REPLACED ENGINE MEC.SDR DL733011297Warning System · malfunctionedCABIN PRESSURE WARNING SOUNDED IN FLIGHT, WOULD NOT SILENCE. PRESSURE GOOD. REPLACED AURAL WARNING UNIT AND CABIN ALT SWITCH.SDR DL733011161Bulkhead · crackedINSPECTION OF THE BL 17.1 AND BL 5.7 VERTICAL BEAMS OF THE AFT SIDE OF THE FS 178 BULKHEAD PER BAC S/B 737-53A1225. REVEALED A CRACK IN THE RBL 5.7 BEAM WEB AT WL 185 AND IN THE LBL 17.1 BEAM WEB AT WL 230. THE WEBS OF ALL 4 BEAMS WERE REMOVED AND NEW WEBS ISDR DL733011010Skin · damagedTHE FUSELAGE BELLY SKIN WAS GOUGED, DENTED AND PUNCTURED AT SEVERAL LOCATIONS BETWEEN FS 400 & 470 AND BETWEEN STRINGERS 26L & 26R.SDR DL733010931Pin · burnedON DESCENT DFW THE APU DET INOP LIGHT ON FIRE PANEL ILLUM. FOLLOWED POM PROCEDURE. APU AND APU BLEEDS WERE OFF AT THE TIME. ON FINAL THE APU FIRE WARN ILLUM. FOLLOWED POM PROCEDURE AND DISCHARGE FIRE BOTTLE. APU FIRE WARN REMAINED ILLUM FOR 3-5 MINUTES. SDR DL733010925Web · crackedDURING INSPECTION PER SB 737-53A1173 REVISION 3, FOUND COCKPIT FLOOR WEBS JUST AFT OF 178 BULKHEAD CRACKED.SDR DL733010815Light · missingFOUND SEAT EMERGENCY LIGHT MISSING AT 16D. REPLACED MISSING LIGHT AND CABLE ASSY.
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