N682DA
Service difficulty reports · 226
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N682DA' AND registry_match = 'registration' 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 = 'N682DA' AND registry_match = 'registration' 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 DU4R2006697Floorboard · corrodedCORROSION ON GALLEY FLOOR AT BS 1720 - BL 4L CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 17-1/2" BY 6-5/8" FROM 2024-T3 .063" BAC1517-2226 IAW B757 SRM 51-10-02, 53-00-51, 51-20-01, AND 53-60-51 FIG 201.SDR DU4R2006693Floor Panel · gougedGOUGES ON AFT GALLEY FLOOR AT BS 1682 BL-54L IN CABIN COMPARTMENT. FABRICATED AND INSTALLED REPAIR DOUBLER 9-1/2" BY 5-3/4" FROM 2024-T3 .063" IAW B757 SRM 53-00-51, 51-20-01, 53-60-51 FIG 201.SDR DALA1134770682Skin · corrodedAFT PIT LWR SKIN AT BS 1290, S-27L TO S-28L CORROSION REPAIRED IAW SRM 51-20-01 AND 53-00-01.SDR DU4R2006707Skin · corrodedCORROSION AFT PIT LWR SKIN BS 1290 BETWEEN S-27L AND S-28L. REMOVED CORRODED SKIN SECTION. FABRICATED AND INSTALLED DOUBLER 12-11/16" BY 12-1/2" FROM 2024-T3 .125" IAW B757 SRM 51-20-01 AND 53-00-01.SDR DALA1134760682Floorbeam · corrodedFWD CABIN FLOORBEAM AND HAT AT BS 377.7, RBL 10 CORROSION REPAIRED IAW SRM 53-10-51 AND 51-30-2.SDR DU4R2006705Crease Beam · corrodedCORROSION MAIN CABIN LT CREASE BEAM BS 1020. REMOVED CORRODED ANGLE. FABRICATED AND INSTALLED L ANGLE REPAIR 3-3/4" BY 3-1/2" BY 1-1/4" FROM 7075-T6 .090" IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006704Channel · corrodedCORROSION FWD CABIN FLOORBEAM AND HAT SECTION AT BS 377.7 RBL 10. REMOVED HAT SECTION. FABRICATED AND INSTALLED HAT SECTION FROM 3" BY 3"7075-T6 EXTRUSION IAW B757 SRM 53-10-51 AND 51-30-2.SDR DL757060997Fitting · gougedTHE LT WING SIDE LOAD FITTING HAS TWO HOLES THAT WERE OVERSIZED TO CLEAN UP TOOL DAMAGE. THE HOLES WERE OVERSIZED AND OVERSIZED FASTENERS WERE INSTALLED.SDR DU4R2006692Skin · dentedLOWER FUSELAGE BS 1540 S-27L - S-28L DENTED NEXT TO STRINGER. CUT OUT DENTED AREA, PERFORMED HFEC IAW B757 NTM PT. 6 51-10-00. FABRICATED AND INSTALLED SKIN REPAIR 16.5" BY 10.5" FROM 2024-T3 .080" IAW B757 SRM 53-00-01.SDR DU4R2006706Shear Tie · corrodedCORROSION AND DAMAGE LEVELING COMPOUND AFT CARGO BS 1620 FROM S-29L TO S-29R. REMOVED CORRODED SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE .75" BY 1.5" BY 1.5" BY 1.5" BY 4" FROM 7075-T6 .040" IAW B757 SRM 51-30-01 AND 51-40-02, AMM 51-21-03 AND PS 900-3-6SDR DU4R2006703Floorbeam · corrodedCORROSION CABIN FLOORBEAM AT BS 365.25 12" LEFT OF B/L 0. CUT OUT CORRODED SECTION OF FLOOR BEAM. FABRICATED AND INSTALLED FLOORBEAM REPAIRS 12" BY 1" FROM 7075-T6 .063", 12" BY 1" FROM 7075-T6 .090", 12" BY 1" FROM 7075-T6 .125" AND EXTRUDED TEE 12" BY 3" BSDR DALA1134690682Skin · corrodedCORROSION AFT PIT LOWER SKIN BS 1290 BETWEEN S-27L AND S-28L REPAIRED PER SRM.SDR DALA1134680682Skin · corrodedCORROSION ON SKIN UNDER AFT LAV SERVICE PANEL BS 1681 AND S-26R TO S-29R REPAIRED PER SRM.SDR DALA1133790682Gear · unknownTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.SDR DALA1133760682Link · damagedNACELLE STRUT UPPER LINK WING AND STRUT FITTING BUSHING REPLACED IAW EA 06-075079-03, ME01, ME02.SDR DL757050014Starter · failedMAIN ENGINE STARTER CAME TO THE SHOP WITH SEPARATED INLET HOUSING AND A PIECE MISSING FROM TURBINE ROTOR. REMOVED FROM NR 1 ENGINE DUE TO FAILURE.SDR DL757040417Wire · damagedANTI-SKID CYCLES ON REPEATEDLY. OVERHEAD ANTI-SKID ILLUMINATED ON STATUS PAGE. NORMAL AND ALT ANTI-SKID ARE ON. RESET C/BS TESTED NORMAL FOR 5 MIN THEN CAME BACK ON. BITE ON ANTI-SKID BOX SHOWS BOX1-5 AND TRANSDUCER NR 1. PULLED OUT TRANSDUCER 1 AND CHECKED WSDR DL757040156Odor · detectedAPPROX 1 HR INTO FLIGHT, THE FLIGHT ATTENDANTS IN THE AFT GALLEY COMPLAINED OF AN ODOR, MAYBE OF A CHEMICAL NATURE COMING FROM AFT GALLEY AND ABOUT 4 ROWS OF SEATS FWD OF GALLEY. ODOR WAS OFF AND ON FOR REMAINDER OF FLIGHT. TURNED ON ALL LIGHTS, OVENS AND CSDR DL757002270Skin · tool damageAN EXISTING TEMPORARY REPAIR DOUBLER WAS REMOVED FROM THE FUSELAGE SKIN AT FS 500 BETWEEN STRINGERS 27R & 28R TO ACCOMPLISH A PERMANENT REPAIR. ADDITIONAL TOOLING DAMAGE WAS INFLICTED ON THE SKIN AT THE REPAIR LOCATION. TO REMOVE ALL DAMAGE, THE EXISTINSDR DL757002271Skin · dentedTHE FUSELAGE SKIN WAS FOUND WITH A 12 X 7 INCHES DENT AT FS 1350 BETWEEN STRINGERS 27L AND 28L. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 379213- 14.SDR DL757990435Engine · failedLT OIL FILTER EICAS MESSAGE DURING CLIMBOUT. FOLLOWED POM, SHUTDOWN ENGINE. REPLACED NUMBER 1 ENGINE.SDR DL757990351Engine · bird strikeON T/O, A/C HIT FLOCK OF BIRDS. REPLACED RT NOSE LAND AND TAXI LIGHT AND RT WING STATIC WICK. C/W BIRD STRIKE INSPECTION. REPLACED VOICE REC, NR 1 AND 2 ENG FAN BLADES AND PERFORM VIBRATION SURVEY PER PFHB.SDR DL757980247Wedge · delaminatedTHE NR 9 SLAT ON THE RT WING WAS FOUND WITH 1.25 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE, 39 FROM THE OUTBD END. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363885-14AD.SDR DL757971299Actuator · failedAFTER T/O, WHEN FLAPS RETRACTED LEADING EDGE SLAT DISAGREE LIGHT ILLUM. FOUND NR 6 SLAT ROTARY ACTUATOR OVERLOAD IND POPPED. MTC IN PROGRESS REPLACING ACTUATOR.SDR DL757960579Fseu Computers · malfunctionedCLIMBING THROUGH FL390 FLAP UP, L/E SLAT ASYMMETRICAL EICAS MSG AND L/E CAUTION LIGHT. CYCLING ALTN L/E SLAT SWITCH HAD NO EFFECT. PERFORMED 20 DEGREE FLAP LANDING PER PILOTS OPS MANUAL. LIGHT AND MSG EXTINGUISHED ON TAXI IN WITH FLAPS UP AND BOTH CAME BACSDR DL757953010Skin · lightning strikeFOUND DURING LETTER CHECK, LIGHTNING DAMAGE ON UPPER LT SIDE OF FUSELAGE, STARTING JUST FORWARD OF THE L-2 DOOR AND GOING PAST THE AFT OVER WING EXIT. BURNISHED AND DYE CHECKED ALL STRIKES, EXCEPT AT STATION 1000. OK TO TREAT AND PAINT ALL EXCEPT STA 1000 AN
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