N683DA
Service difficulty reports · 194
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 = 'N683DA' 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 = 'N683DA' 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 DALA1147580683Skin · damagedWHILE ACCOMPLISHING MTC SEVERAL MISDRILLED HOLES CAUSING 17 DAMAGED HOLES AT STA 1400 STR 27 LT TO 28 RT AT THE BUTT SPLICE AREA OF THE SKIN ONLYERA 495021-14 REV 0.SDR DALA1147440683Skin · damagedWHILE ACCOMPLISHING MAINTENANCE IN ATL, MTC MISDRILLED SEVERAL RIVET HOLES, CAUSING SEVENTEEN DAMAGED HOLE AT STATION 1400, FROM STRINGER 27 LEFT TO 28 RIGHT AT BUTT SPLICE AREA IN THE SKIN ONLY.SDR DALA1147600683Splice · corrodedINTERNAL BUTT SPLICE STA 1401 HAD SEVERE CORROSION ON THE INTERNAL SURFACE BETWEEN STR 27L AND 28L. REPAIRED AREA PER ERA 379695-14.SDR DL757091852Skin · damagedTHE FUSELAGE SKIN AT STATION 515 WAS DAMAGED BY A LIGHTNING STRIKE AT STRINGER 26R WHICH WAS ADJACENT TO AN EXISTING REPAIR ON THE FUSELAGE. REPAIR INSTALLED IN ACCORDANCE WITH ERA 478200-14.SDR DL757091590Skin · damagedAIRCRAFT DMG 12IN GASH FWD OF 2L DOOR. REPAIRED DMG PER ERA477438-14 REV A.SDR DL757090006Valve · leakingA/C ABORTED TAKEOFF AT 50 KTS FOR RT HYD PRESS AND RT HYD QUANTITY. FOUND NORMAL ANTI-SKID NR 2 FUSE VALVE LEAKING AND LOOSE EDP PRESS LINE ON NR 2 ENG. REPLACED VALVE WITH UNIT FROM UPS AT MIA.SDR DL757081238Spar · crackedDURING SHOP OVERHAUL VISIT, A CRACK WAS FOUND IN THE SKIN AND SPAR OF THE LT OUTBOARD AILERON. REPAIRED PER 470474-14.SDR DU4R2006673Housing · corrodedS/O 291025 N/R NR 24276 CORROSION ON TOP OF LAV SERVICING HOUSING BS 1681 TO BS 1701. FABRICATED AND INSTALLED CHANNEL 18.5 INCHES X 2 INCHES X 1INCH, CHANNEL 8 INCHES X 2.5 INCHES X .5 INCH AND 4 EA BRACKETS FROM 2024-T3 CLAD .032 INCH AND REPLACED DOOR P/N SDR DU4R2006675Skin · corrodedS/O 291025 N/R 25256 CORROSION ON FUSELAGE SKIN BS 1681 AND S-26R TO S-29R. COMMON TO AFT LAVE DRAIN PAN FWD FLANGE MOUNT. FABRICATED AND INSTALLED DOUBLER 10 INCHES X 14 INCHES AND FILLER 11.7 INCHES X 11.10 INCHES FROM 2024-T3 .063 INCH IAW ERA 458474-14 DASDR DU4R2006674Housing · corrodedS/O 291025 N/R 24877 CORROSION ON FRAME ON TOP OF LAV SERVICING HOUSING BS 1681 TO BS 1701. FABRICATED AND INSTALLED FRAME 17.3 INCH X 3.3 AND BEAM 4 INCHES X 1 INCH X 1 INCH AND 2 BRACKETS 1.3 INCH X 1.8 INCH AND 2 BRACKETS 2.5 INCHES X 1.5 INCH FROM 2024-T3 SDR DU4R2006672Fitting · migratedS/O 291025 N/R 24208 LT AND RT WING FORWARD OB DRAG FITTING, IB BUSHINGS HAVE MIGRATED .071 INCH AND 0.053 INCH. ACCOMPLISHED PERMANENT REPAIR IAW ERA 379641-14 REV. A CODE 6-57-42. FABRICATED AND INSTALLED BUSHING 1.7665 INCH X 2.040 INCH FROM A1-N1-BRONZE MSDR DU4R2006676Skin · dentedS/O 291025 N/R 24207 3 EA DENTS IN FUSELAGE SKIN BETWEEN S-16L AND S-17L FROM BS 600 - BS 630. REMOVED SKIN PANEL P/N 143N3320-4 AND INSTALLED SKIN PANEL P/N 654N0243-61 FROM PRODUCTION BUTT LINE AT BS 439 TO BS 661 AND FROM S-14L TO S-19L, FABRICATED AND INSSDR DL757060911Skin · corrodedDURING CURRENT HMV OF AIRCRAFT, CORROSION WAS FOUND ON THE FUSELAGE SKIN SURFACE AT FS 1682, S26R S29R, UNDER THE FORWARD FLANGE OF THE AFT LAV SERVICE PAN ASSEMBLY. THE CORROSION WAS BLENDED TO REMOVE THE DAMAGE, AND A BOEING APPROVED REPAIR WAS INSTALLED PESDR DU4R2006653Support Beam · corrodedS/O 291025 N/R 25189 CORROSION IN SCREW HOLES AND DRILLED OFF SCREWS AT SUPPORT BEAM AFT PIT FLOOR LEVEL S-27R FROM BS 1380 TO 1440. OVERSIZED HOLE, INSTALLED FREEZE PLUG, FABRICATED AND INSTALLED REPAIR STRAP 2.50 INCHES X .90 INCHES FROM 7075-T6 .063 INCH ISDR DU4R2006646Support · corrodedS/0 291025 N/R 24243 CORROSION ON WING TO BODY FAIRING SUPPORT FRAME AT FS 860 (LWR PANEL). CUT OUT CORRODED SECTION OF ANGLE. FABRICATED AND INSTALLED DOUBLER 23 INCH X 1INCH X 1INCH FRP, 775-T6 .050 INCH, 2 EA. DOUBLERS 23 INCH X 1INCH X 1 INCH AND 1 EA. 12SDR DU4R2006652Intercostal · corrodedS/O 291025, NR 25180 CORROSION AT BS 1480 TO 1500 S-27R INTERCOSTAL UPPER AND INNER SURFACE.CUT OUT CORRODED INTERCOSTAL CAP. FABRICATED AND INSTALLED REPAIR INTERCOSTAL CAP 18.8750 INCH X 2 INCHES FROM 7075-T6 .050 INCH IAW SRM 51-30-01, 51-20-01 AND 51-40-02SDR DU4R2006648Support Beam · corrodedS/O 291025 NR 24879, CORROSION ON L4 DOOR LOWER SILL SUPPORT BEAM AROUND FASTENER HOLES, CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER 40.0 INCH X 6 INCH FROM 7075-T6 .071 INCH IAW SRM 51-70-11.SDR DU4R2006651Floorbeam · corrodedS/O 291025, NR 25013 CORROSION ON UPPER T-CAP OF FLOORBEAM IN PASSENGER CABIN AT BS 720 B/L 3R. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED ANGLE REPAIR 11INCHES X 1 INCH X 2 INCH FROM BAC1490-2865 AND ANGLE DOUBLER 14 INCHES X 2 INCHES X 1INCH FROM BAC SDR DU4R2006647Skin · corrodedS/O 291025, N/R 24770 CORROSION ON FUSELAGE SKIN AT BS 1510 BETWEEN S-28R AND S-29R.CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 7.0 INCHES X 12.75 INCHES X 6.6 INCHES FROM 2024-T3 .063 INCH IAW SRM 51-40-05, 53-00-01 FIG. 1, 51-20-02 AND 53-SDR DU4R2006650Shear Web · corrodedS/O 291025 NR 24959 CORROSION ON SHEAR DECK LOCATED NEAR RT AFT CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER 9.00 INCHES X 5.70 INCHES FROM 2024-T3 .063 INCHES IAW SRM 51-20-01, 51-10-02 AND 53-60-51, FIG. 101.SDR DU4R2006649Shear Web · corrodedS/O 291025, NR 24881 CORROSION ON SHEAR DECK LEADING EDGE AROUND FASTENER HOLES. FABRICATED AND INSTALLED REPAIR DOUBLER 9.60 INCH X 4.60 INCH FROM 2024-T3 .063 INCH IAW SRM 51-20-01 AND 53-60-51, FIG 201.SDR DL757060930Skin · damagedPART REMOVED FROM AC 683. SENT TO SHOP FOR CSVE. WEDGE HAD HAIL DAMAGE AND IS A REQUIRED REPORTING ITEM IAW SRM 57-43-02D. WEDGE REPLACED IAW SRM57-43-02D. SLAT WAS RETURNED TO SERVICE AND SENT TO STOCK AS SPARE ON 11/08/06.SDR DL757060641Light · inoperativeESCAPE PATH LIGHTS AT ROWS 25, 46, 45 INOP. REPLACED LIGHT ASSEMBLIES.SDR DL757050552Apu · smokeLIGHT SMOKE VISABLE IN COCKPIT DURING TAXI IN. SEEMED TO APPEAR AFTER BLEED SOURCE SWITCHED TO APU. UNABLE TO DUPLICATE OR LOCATE FAULT.SDR DL757050238Odor · detectedA/C DIVERTED TO DEN DUE TO ACRID ODOR IN CABIN. AFTER INTENSIVE TROUBLESHOOTING, COULD NOT DUPLICATE ODOR. ALL A/C SYSTEMS FUNCTIONING AND OPERATING NORMALLY.SDR DL757040465Coffeemaker · overheatedMID GALLEY COFFEE MAKER OVERHEATED, REPLACED COFFEE MAKER.SDR DL757040138Tire · puncturedFOUND BOLT IN NR 7 MLG TIRE. REMOVED AND REPLACED NR 7 MLG WHEEL ASSY PER MM.SDR DL757031141Light · brokenON INSPECTION FOUND EMERGENCY PATH LIGHT BROKEN OFF SEAT AT 4CD. REPLACED LIGHT ASSY, SHROUD-BACKING PLATE AND LENS. OPS OF LIGHT NORMAL.SDR DL757020619Light · inoperativeL-1 DOOR EXT DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED REFLECTOR.SDR DL757010680Inverter · failedA/C 683 FLT 988. ENROUTE SLC-MSY DIVERTED TO OKC DUE TO SULFUR SMELL FUMES IN COCKPIT. IDENTIFIED THE STATIC INVERTER M217 DPN 241702694, MFG P/N 1-002-0102-1000, SERIAL NBR CJ001250 AS SOURCE. REPLACED INVERTER.SDR DL757010135Splice · corrodedTHE SKIN BUTT SPLICE STRAP AT FS 1401 WAS FOUND CORRODED BETWEEN STRINGERS 27L & 28L. THE SPLICE WAS CUT BETWEEN STRINGERS 26L & 27L AND THE LOWER SECTION WITH THE CORROSION REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED WITH AN ALUMINUM REPAIR STRAP SDR DL757010143Skin · crackedTHE LT SIDE SKIN ON THE NR 1 PYLON WAS FOUND EMANATING FROM THE FWD UPPER CORNER OF THE FWD ACCESS HOLE. ADDITIONAL TOOLING DAMAGE WAS INCURRED ON THE SIDE SKIN AFT OF THE CUTOUT ALONG THE UPPER CHORD ATTACH AREA. THE DAMAGE WAS ROUTED OUT OF THE SIDE SKIN ASDR DL757010120Skin · lightning strikeTHE FUSELAGE SKIN WAS FOUND WITH SEVERAL LIGHTNING STRIKES NEAR STRINGER 25R BETWEEN FS 480 & 510. REMOVAL OF THE DAMAGE REQUIRED 4 SMALL 2 - 4 INCH CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOULBER INSTALLED PER ER/A 379SDR DL757010119Skin · dentedTHE FUSELAGE SKIN WAS FOUND WITH THREE DENTED AREAS BETWEEN FS 590 & 630 AND BETWEEN STRINGERS 16L & 17L. THE SKIN WAS CUT AT FS 590 AND AT FS 630 FROM THE STRINGER 14L LAP JOINT TO THE STRINGER 19L LAP JOINT. THE DAMAGED SECTION OF SKIN WAS REMOVED AND A NESDR DL757010094Skin · gougedL-2 DOOR WAS FOUND WITH OUTER SKIN DAMAGE AT STA 701.74. REPAIRED PER ER/A 401226-14.SDR DL757010060Skin · gougedTHE FUSELAGE SKIN WAS FOUND GOUGED FROM FS 537 TO 563 BETWEEN STRINGERS 16L & 17L. THE GOUGE WAS REMOVED WITH A 25 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 379604-14, REV A.SDR DL757982104Floor Panel · corrodedMID VISIT, CORROSION ON FIXED FLOOR PANEL RT STA 760 TO 800, REPAIRED.SDR DL757982103Floorbeam · corrodedMID VISIT, FLOORBEAM CORRODED AT STA 345 TO 379 BL 0, REPAIRED.SDR DL757982102Beam · corrodedMID VISIT, CORROSION ON CREASE BEAM AT R2 DOORWAY, STA 680 TO 785 RBL65.SDR DL757982101Beam · corrodedMID VISIT, CREASE BEAM CORRODED AT STATION 660 LBL63, REPAIRED.SDR DL757982100Floorbeam · corrodedMID VISIT, FLOORBEAM AT STA 1640 LBL 0 TO LBL 58 CORRODED, REPAIRED.SDR DL757981759Wedge · dentedTHE NR 3 SLAT TRAILING EDGE WEDGE WAS FOUND DENTED FROM A BIRD STRIKE. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 (AS REFERENCED IN SRM 57-43-02). SINCE THE SLAT WEDGES ARE THE SUBJECT OF AD T91-22-51, THE REPAIR WAS DOCUMENTED PER ER/A 365517-14AD.SDR DL757960034Te Wedge · wornDURING SHOP INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH TRAILING EDGE WEDGE WORN AND GOUGED. REPAIRED WEDGE PER SRM 51-70-10.SDR DL757953250Connector · looseAPU QUIT INFLIGHT WITH APU FAULT LIGHT. NR 2 IDG WAS ON MCO/PLAC AS INOPERATIVE, RETURNED TO ATL. APU EEC FAULTS APU INLET DOOR. REPLACED DOOR ACTUATOR, NO HELP. MANUALLY OPENED DOOR AND RESEATED CANNON PLUG. APU START AND OPERATION NORMAL. NR 2 IDG CONT
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