N110DL
Service difficulty reports not matched to an aircraft · 22
They name N110DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
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 n_number = 'N110DL' AND registry_match IS NULL 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 n_number = 'N110DL' AND registry_match IS NULL 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 DL767050551Wire · shortedNOTICED ELECTRICAL PLASTIC ODOR NEAR CAPTAINS GLARESHIELD LIGHT CONTROL PANEL, NEAR LOWER LEFT CORNER OF WINDSCREEN. FOUND L1 WINDOW SENSOR CONNECTION BAD AND SHORTED. REMOVED AND REPLACED L1 WINDOW ASSY PER AMM.SDR DL767050067Engine · failedWHILE RUNNING APU ON GND WITH PACKS ON MTC NOTICED SMOKE IN THE CABIN AND SMOKE OUT OF APU EXHAUST. FOUND APU COMPRESSOR OUTLET DRIPPING OIL. REPLACED APU.SDR DL767021274Wedge · delaminatedAFT FLAP T/E WEDGE BONDED ASSY WAS FOUND DELAMINATED BEYOND THE SCOPE OF A LOCALIZED REPAIR. REPAIR PER ER/A 417896-14.SDR DL767002274Idg · lack of lubeON T/O ROLL, LT GEN DRIVE EICAS MSG CAME ON. ABORT T/O AT 100 KNTS. BPCU INDICATES SERVICE IDG. SERVICED IDG AND RAN ENGINE.SDR DL767002096Skin · corrodedCORROSION DAMAGE FOUND ON THE UPPER SURFACE OF THE CENTER WING SKIN AND IN THE UPPER SPAR CAP AT STA 955, RBL 70 - 90. IN NORDER TO VERIFY REMOVAL AND FACILITRATE A REPAIR THE LOWER CHORD OF THE RBL 74.81 FLOORBEAM WAS CUT FWD TO THE DAMAGE AND THE AFT SECTIOSDR DL767002097Bulkhead · wornHOLE FOUND ELONGATED IN THE AFT BULKHEAD OF THE NR 1 PYLON ON THE LOWER FWD GSE HOLE (6TH FROM THE TOP). THE RIVET HOLES INSTALLED PER BOEING S/B 767-54-0010 WERE DOUBLE DRILLED. ADDITIONAL WEAR DAMAGE FOUND JUST BENEATH THE GSE HOLE. ER/A 396279-14.SDR DL767992631Skin · puncturedTHE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 1197 & 1219 AND BETWEEN STRINGERS 36L & 38L. STRINGERS 36L & 37L WERE CRACKED AND THE O/B SKIN FLANGE OF STRINGER 38L WAS CRACKED. THE DAMAGED SKIN WAS CUT OUT WITH A 10 X 18 CUTOUT AND THE DAMAGED FLANGE OF STR 38SDR DL767990482Door · missingPASSING 12,000 FT, FLT ATTENDANT REPORTED LOUD NOISE. ALSO, HAD LT SLIDE DOOR EICAS MSG AND OVERHEAD DISCREET EMER DOORS. SLIDE HAD DEPARTED A/C WITH FAILURE OF DOOR. REPLACED DOOR SLIDE AND DAMAGED PANELS.SDR DL767990442Slide · deployedLT OVERWING SLIDE DEPLOYED IN FLIGHT PASSING THRU FL 12 OUT OF ATL. MTC OBSERVED LINKAGE ON DOOR RELEASE MECHANISM, FOUND THIRD LINKAGE FROM FORWARD EDGE BENT AND BROKEN, CAUSING CENTER TWO LATCHES TO RELEASE. FORWARD AND AFT LATCHES WERE FOUND INTACT WITH DSDR DL767990432Slide · detachedPASSING 21,000 FT MSL, FLT ATTENDANTS COMPLAINED OF LOUD NOISE. ALSO, HAD EICAS MSG LT SLIDE DOOR AND OVERHEAD DISCREET EMERG DOORS. AIR TURNBACK TO ATL. FOUND LT OVERWING SLIDE PANEL AND SLIDE DEPARTED AIRCRAFT. SEVERAL SMALL ABRASIONS AROUND SURROUNDING SDR DL767990388Skin · delaminatedTHE UPPER SKIN ON THE NR 3 SLAT TRAILING EDGE WAS FOUND WITH A 3 X 4 DENTED/DELAMINATED AREA. THE DAMAGED SKIN WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 366773-14AD.SDR DL767982109Oven · contaminatedSHORTLY AFTER TAKEOFF, SMOKE OBSERVED FROM AFT GALLEY OVENS. COULD NOT DETERMINE SOURCE OF SMOKE, FOOD OR ELECTRICAL. FOUND BURNT SUBSTANCE IN CORNER OF LOWER LEFT OVEN IN AFT GALLEY. REPLACED OVEN ASSEMBLY AND NEW OVEN, OPS NORMAL.SDR DL767981726Floorbeam · corrodedCORROSION DAMAGE WAS FOUND ON THE UPPER CAP OF THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 54, FROM BS 850 TO THE AFT END OF THE UPPER CAP AT APPROX BS 1000. THE UPPER CAP WAS REPLACED, BUT THE ORIGINAL EXTRUSION COULD NOT BE OBTAINED. REPAIRED PER ERA 332058SDR DL767981707Floorbeam · corrodedCORROSION WAS FOUND ON THE UPPER SURFACE OF THE BS 287 FLOORBEAM UPPER CHORD. IN ADDITION, AN EXISTING REPAIR WAS ALSO LOCATED IN THE SAME AREA. REPAIRED PER ERA 332044-14.SDR DL767981469Wedge · delaminatedDELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD.SDR DL767972696Skin · puncturedTHE FUSELAGE SKIN AT FS 422 BETWEEN STRINGERS 21L AND 22L WAS PUNCTURED BY GROUND EQUIPMENT. THE FINAL SKIN CUTOUT WAS 6.5 BY 5. THE DAMAGE WAS REPAIRED WITH A SKIN DOUBLER. INSTALLED PER THE PROCEDURES OF THE B767 SRM AND DOCUMENTED PER ER/A 300885-14, REVSDR DL767971572Union · brokenAFTER T/O, RETRACTED GEAR, RAISED FLAPS TO 5 DEG, THEN 1 DEG AND LOST HYD FLUID IN CTR SYS. FLAPS REMAINED AT 5 DEG, RAISED WITH ALT SYS. MTC FOUND UNION (P/N S270T230- 20) ON OUTLET OF ADP PUMP BROKEN. REPLACED WITH AS1582C10.SDR DL767961449Check Valve · inoperativeAFTER T/O, A/C WOULD NOT COOL. HOT AIR ENTERED PASSENGER CABIN AND COCKPIT UNABLE TO STOP HOT AIR ISOLATED BOTH SIDES, NO HELP. REPLACED RT PACK TRIM AIR CK VALVE (P/N 211102808) (MFG/NR 3202726-1) (S/N 2347).SDR DL767961188Skin · dentedTHE NR 1 SLAT, TRAILING EDGE WEDGE WAS FOUND DENTED IN THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767-200 SRM 51-70-10 FIG 9.SDR DL767954539Fan · failedDURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN. DEACTIVATED RECIRC FAN AND ODOR DISSIPATED. REPLACED RECIRC FAN, OPERATION NORMAL.SDR DL767954159Te Wedge · delaminationRT WING NR 9 AND NR 11 SLAT TRAILING EDGE WEDGES HAVE AREAS OF DELAMINATION. ACCOMPLISHED REPAIRS PER DL ERA 272145-14AD.SDR DL767951148Flap · delaminatedNR 7 INTERM REPAIR TO L/E OF O/B FLAP JUST I/B OF THE NBR 8 FLAP DRIVE IS DELAMINATED.
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