N104DA
Service difficulty reports not matched to an aircraft · 32
They name N104DA, 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 = 'N104DA' 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 = 'N104DA' 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 DL767040957Odor · detectedRAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE.SDR DL767040009Beam · corrodedCORROSION WAS FOUND IN THE HOLE BORES OF THE '9-10' BEAM WHICH PROVIDES THE OUTBOARD SUPPORT FOR THE INBOARD FLAP ON THE LT WING. THE CORRODED HOLES WERE OVERSIZED TO REMOVE CORROSION AND BUSHED TO ALLOW INSTALLATION OF PROPER SIZE BOLTS. THE REPAIR WAS ACCOSDR DL767030284Wedge · debondedLEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767030130Duct · rupturedLEFT AND RIGHT DUCT LEAK INDICATION IN COCKPIT FOUND FWD CARGO HEAT DUCT AND CROSSOVER MANIFOLD RUPTURED PER IPC 36-11-01-10SDR DL767030092Line · chafedPILOT REPORT--AT 2500 AFTER T/O RT RSVR AND RT ENG PRESS LIGHT ILLUMINATED TOWER REPORTED SMOKE FROM RT ENGINE. RETURNED TO LAS NORMAL LANDING. RT HYD QTY ON EICAS IND -0- AND RF OVERWEGHT LANDING ACT LANDING WT 273100. FOUND NR 2 ENGINE HYD PRESSURE LINE SDR DL767011077Bulkhead · crackedDURING ACCOMPLISHMENT INSPECTIONS PER BAC S/B 767-53-0078, CRACKS WERE FOUND IN THE TENSION FITTING, FWD OUTER CHORD, AND SKIN. THE S/B ONLY COVERS CRACKS IN THE OUTER CHORD. CORRECTIVE ACTION: REPAIRED PER DAL ERA 397710-14ADSDR DL767011056Fitting · crackedWHILE ACCOMPLISHING THE STRUT IMPROVEMENT PROGRAM MODIFICATION ON THE LT WING SUPPORT STRUCTURE, A CRACK INDICATION WAS FOUND IN THE O/B ROW 2ND HOLE FROM BOTTOM COMMON TO THE RIB NR 8 ENGINE SUPPORT FITTING, THE FRONT SPAR, AND THE FRONT SPAR WEB. ER/A 39765SDR DL767010205Floorbeam · damagedTHE LOWER CHORD AREA OF THE FS 266.5 FLOORBEAM SUFFERED HEAT DAMAGE FROM AN ELECTRICAL WIRE ARCING BETWEEN RBL 23 & 30. THE LOWER CHORD AND LOWER PORTION OF THE FLOORBEAM WEB WERE CUT OUT OVER A 6.5 INCH LONG X 2.7 INCH HIGH AREA TO REMOVE ALL AREAS OFSDR DL767010161Harness · overheatedMULTIPLE EICAS WARNINGS AND AN ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND WIRE BUNDLE BURNED ABOVE P50 PANEL DUE TO CHAFING ON STRUCTURE. REPAIRED WIRE AND TESTED ON NR 1 THROUGH 120, EXCEPT 6, 7 AND 106.SDR DL767010052Harness · burnedMULTIPLE EICAS WARNINGS AND ELECTRICAL BURNT SMELL IN COCKPIT AND MID CABIN. FOUND INBOARD MOST WIRE BUNDLE IN RIGHT HAND TUNNEL AREA OF MAIN E AND E AT STATION 266.5 BURNT. WIRE BUNDLE NUMBER W451 AT CABIN FLOOR LEVEL. REPLACING WIRES, INTERNAL INVESTIGATISDR DL767010034Skin · damagedTHE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR WHICH WAS INSTALLED BETWEEN FS 500 & 521 AND BETWEEN STRINGERS 33L & 39L. THE UPPER PORTION OF THE REPAIR WAS REMOVED AND THE ADDITIONAL SKIN DAMAGE REMOVED WITH AN ADDITIONAL CUTOUT. A NEW ASDR DL767010023Skin · damagedTHE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR LOCATION AT FS 456 AND STRINGERS 33L-34L. THE REPAIR WAS REMOVED AND ALL UNDERLYING DAMAGED CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER B767 SRM 53-0SDR DL767010022Fitting · damagedTHE CORNER SPLICE FITTING OF THE FS 500 FRAME AT STRINGER 33L WAS DAMAGED BY GROUND EQUIPMENT STRIKING THE AIRCRAFT. THE DAMAGED FITTING WAS REMOVED AND A NEW FITTING MANUFACTURED AND INSTALLED PER ER/A 379704-14.SDR DL767001599Flashlight · inoperativeFLASHLIGHT AT 2R DOES NOT INDICATE CHARGE. FOUND LED INDICATOR INOP. REMOVED AND REPLACED FLASHLIGHT.SDR DL767991853Overheat Loop · failedAFTER T/O ENG EICAS MSG LT ENG OVHT LP1/LP2 FIRE OVHT SYS FAIL LIGHT ON. REPLACED M687 AND M688 LEFT OVHT LOOP 1 AND 2 CARDS, INSPECTED LEFT ENG PNEU DUCTS AND CLAMPS. RETORQUED CLAMPS. RAN ENGINES TO T/O POWER FOR SEVERAL MIN, NO OVHT MSG OR CAUTION. INSSDR DL767991612Latch · wornTHE RT OVERWING SLIDE DOOR WOULD NOT OPEN MANUALLY DUE TO WORN SPOTS IN THE LATCH CAM PLATE. THE DOOR OPERATED NORMALLY AFTER REPLACING THE WORN LATCHES.SDR DL767991227Coffeemaker · dirtyELECTRICAL SMELL IN FWD GALLEY AFTER LANDING, STRONG ODOR UTILITY BUSSES TURNED OFF. NO ELECTRICAL ODOR NOTED ON ENTRY. CKD ALL COMPONENTS IN GALLEY, ALL CK NORMAL. NOTED SPILLED AND BURNED COFFEE ON RT FWD COFFEEMAKER. SUSPECT THIS WAS ODOR REPORTEDSDR DL767981281Skin · delaminatedDELAMINATION WAS FOUND ON SEVERAL T/E WEDGES OF THE L/E SLATS (NR 1, 2, 4 AND 5). REPAIRED PER ERA 365004-14AD.SDR DL767971849Hyd Line · leakingLT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AN APPROVED INTERIM LINE HAD BEEN INSTALLED AT MIA BECAUSE OF A HYDRAULIC LEAK. REPLACED LINE WITH PERMANENT REPAIR. BLED AND PURGED SYS PER MM TRUCK POSITIONING ACTUATOR REPLACEMENT PROCEDURES. SUSPECTSDR DL767971118Skin · dentedTHE RT SIDE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT BELOW THE C3 CARGO DOOR, RESULTING IN A DEEP DENT AT FS 1435 ABOVE STRINGER 35L. THE DAMAGE REQUIRES REMOVAL, REQUIRING A CUTOUT SIZED APPROX 2.0 (RWD/AFT) BY 6.0 (UP/DOWN). STR 35L IS ALSO DEEPLY DENSDR DL767971010Power Supply · inoperativeRT CEILING EMERGENCY LIGHTS OUT. REPLACED POWER SUPPLY M730.SDR DL767970728Skin · corrodedDURING HMV, EXTENSIVE CORROSION WAS FOUND IN THE BELLY SKIN AND STRINGERS BETWEEN STA 1220 TO 1362 AND BETWEEN STRINGERS S-36L AND S-36R. THE FWD SKIN WAS TRIMMED AT STATION 1230 AND REMOVED FROM THE LAP SPLICES ON EITHER SIDE AT S-36L AND S-36R TO THE EOP ATSDR DL767970727Stringer · corrodedMTC DETERMINED THAT ALL STRINGERS FROM 34L TO 32R, EXCEPT 35R, ARE CORRODED BEYOND ALLOWABLE LIMITS. INSTRUCTIONS GIVEN TO SPLICE IN NEW STRINGER SECTIONS.SDR DL767970729Skin · gougedTHE FUSELAGE SKIN WAS FOUND TO BE DAMAGED IN SEVERAL LOCATIONS AFT OF THE LOWER PORTION OF THE L2 DOOR CUTOUT. THE DAMAGE CONSISTED OF SEVERAL GOUGES, A DENT AND AN EXISTING DOUBLER REPAIR ALL WITHIN CLOSE PROXIMITY.SDR DL767970710Skin · dentedA FUSELAGE DENT RUNNING FROM S-39L TO S-34L AND BETWEEN FS 500 AND FS 552 WAS FOUND TO BE OUTSIDE OF ALLOWABLE DAMAGE LIMITS. THE DAMAGE REQUIRES A CUTOUT OF THE DAMAGED SKIN COVERING A FACTORY SKIN JOINT. THE LOWER SKIN IS MACHINED TO 0.056 AND MADE FROM SDR DL767970373Skin · corrosionDURING HMV, BULGING WAS DISCOVERED ON THE UPPER SURFACE OF THE CENTER WING, UPPER SKIN PANEL AT THE BUTT-SPLICE, BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRINGER 17 AND BETWEEN RBL 74.81 AND 97.42. THE SKIN WAS TRIMMED TO REMOVE THE CORROSION IN THE FORWARSDR DL767970305Skin · corrosionDURING AN INSPECTION OF THE FAR AFT BELLY SKIN, FURTHER CORROSION WAS FOUND AROUND A CUTOUT REPAIRED PREVIOUSLY BY DAL MTC PER SRM GUIDELINES. THE CUTOUT, APPROX 6.125 BY 7 IN SIZE, IS LOCATED BETWEEN FS 1788 AND FS 1809 AND ON EITHER SIDE OF BL 0 (BETWEEN STSDR DL767961183Wire · cutSECTION OF FLOOR TRACK LIGHTS INOP IN MID GALLEY. REPAIRED WIRING.SDR DL767960487Press Line · leakingLEFT HYDRAULIC SYSTEM FAILURE IN-FLIGHT. RETURNED DFW. FOUND ENGINE PRESSURE LINE WITH HOLE IN IT. REPLACED LINE.SDR DL767954722Fan · failedIR - GASPER FAN OFF LIGHT ILLUMINATED WITH SWITCH ON AND ACCOMPANIED BY ELECTRICAL SMELL REPORTED IN CABIN. FORWARD TO MCO AND PLACKARD PER MEL. REPLACED GASPER FAN, OPERATION NORMAL.SDR DL767954656Extinguisher · leakingVERBAL FROM CREW ON ARRIVAL, AFT CABIN WATER FIRE EXTINGUISHER LEAKING. REPLACED EXTINGUISHER.SDR DL767953734Eel · inoperativeAFT LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED AFT LEFT OVERWING EMERGENCY LIGHT. LIGHT OPS CHECK NORMAL.
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