N102DA
Service difficulty reports · 37
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 = 'N102DA' 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 = 'N102DA' 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 DL767060433Skin · corrodedTHE NR 7 SLAT (RT WING INBD SLAT) T/E WEDGE WAS FOUND WITH SKIN AND CORE CORROSION TOTALLING 151 SQ IN. REPAIRED PER ERA090851-14AD.SDR DL767050386Yaw Damper · malfunctionedUNCOMMANDED RUDDER INPUT AT ROTATION, THOROUGHLY CHECKED SYSTEM. UNABLE TO DUPLICATE OR FIND FAULT.SDR DL767050267Shutoff Valve · sticksWHEN POWER INITIALLY REDUCED TO START INITIAL DESCENT A SMELL DEVELOPED IN THE AIRCRAFT. REPLACED NR 1 HPSOV.SDR DL767050080Line · leakingRT HYD SYS FAILURE. RT HYD SYS QTY DROPPED QUICKLY SUGGESTING A LEAK. FOUND RT ENGINE PRESSURE LINE CHAFED THROUGH, REPLACED SAME.SDR DL767050049Pseu · malfunctionedON FLAP RETRACTION GOT L/E FLAP DISAGREE. ON FINAL GOT L/E FLAP ASYM PLI WAS FLUCTUATING POS 5 DEG TO POS 12 DEG. T/S PER FIM 27-81-00. PSEU FAULTS CARD NR 10 AND SHOWS CODES 305 421 422 AND 301. REPLACED PSEU. FSEU SHOWS OUTBD SLAT RVDT MISSING AND 603 FLSDR DL767031053Skin · gougedDENT/GOUGE FOUND ON LOWER SURFACE OF LT HORIZONTAL STAB, FORWARD TORQUE BOX, INBD SKIN PANEL. DENT WAS DUE TO GROUND DAMAGE. REPAIRED PER ERA 423716-14.SDR DL767031012Support Fitting · corrodedCORROSION WAS FOUND IN THE HOLE BORES OF THE 6 FASTENERS WHICH ATTACH THE INBOARD FLAP TO THE OUTBOARD SUPPORT FITTINGS. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND BUSHED. THE ASSEMBLY WAS REINSTALLED WITH ORIGINAL STYLE HARDWARE. THE REPAIR WAS ACCOMPLISDR DL767030987Web · crackedHFEC INSPECTION OF THE AFT P-DOME WEB LAP JOINTS PER AD 88-19-03 REVEALED 26 CRACKS EMANATING FROM FASTENER HOLES ALONG THE LOWER ROW OF THE WEB LAP JOINT BETWEEN WL 190 & 230 (APPROX 210) ON THE RIGHT SIDE OF THE P-DOME.SDR DL767030786Power Supply · dischargedEMERGENCY LIGHTS STAY ON IN F/C GALLEY AND RT SIDE OF F/C SECTION. REPLACED POWER SUPPLY.SDR DL767030475Seat Belt · disconnectedDURING TURBULENCE PASSENGER SEAT BELT AT 36C BECAME DISCONNECTED FROM SEAT, CAUSING A PASSENGER TO BE EJECTED FROM THE SEAT. THE SEAT BELT WAS REMOVED AND REPLACED. THEN BELT WAS SENT TO ATL.SDR DL767030282Wedge · debondedLEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.SDR DL767020872Indicator · overheatedCAPTAIN EADI WENT BLANK. SELECTED ALT EFI AND INDICATOR REMAINED BLANK. ABOUT 5 MINUTES LATER SMOKE WAS SEEN COMINGFROM CAPTAIN EADI. PULLED C/B E3 AND SMOKE STOPPED. REMOVED LEFT ADI INSPECTED CONNECTORS NO DAMAGE FOUND. REPLA LEFT ADI WITH SEVISSDR DL767030058Skin · corrodedTHE FUSELAGE SKIN WAS FOUND WITH A CRACK BETWEEN TWO STRINGER ATTACH FASTENERS AT FS 452 ALONG STRINGER 30R. THE UNDERLYING STRINGER WAS FOUND CORRODED. THE CORRODED AREA OF STRINGER WAS CUTOUT AND REPAIRED PER THE B767 SRM. THE SKIN CRACK WAS REMOVED WITH SDR DL767011691Battery Pack · dischargedON L/O FOUND L-1DOOR AND 3 LT OVERWING EGRESS EMER LTS. INOPREPLACED M-736 BATTERY PACK, OPS CK GOODSDR DL767010883Frame · crackedINSPECTION OF THE FS 1809.5 BULKHEAD CHORDS PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE AFT CHORD, 2 FASTENER HOLE CRACKS IN THE FWD CHORD, AND A FASTENER HOLE CRACK IN THE MID CHORD. THE AFT CHORD WAS REPLACED, THE FWD CHORD CUT AND SPLSDR DL767000308Bolt · damagedWHILE PERFORMING OPN 5940 RC587 FOUND TENSION TIE BOLTS ROTATING AT FS 1702. UPON INSPECTION FOUND BOTH BARREL NUTS L/R AFT POSTION AT FS 1702 HAD FAILED. FOUND TO BE HEAVILY RUSTED. ENGRG ISSUED ERA 373376-14 TO C/W E0 1-74297-12. BOLT AND NUT REPLACEMENTSDR DL767992214Stringer · corrodedFUSELAGE STRINGER S-21AR, BS 1010, RBL 97.42, CORROSION REPAIR. STRINGER 21AR WAS FOUND WITH EXTENSIVE CORROSION AT FS 1010 AND RBL 97.42. THE STRINGER FORMS AN END CAP FOR THE MLG HORIZONTAL PRESSURE BULKHEAD. THE CORROSION WAS REMOVED WITH A 5 INCH CUTOSDR DL767990695Switch · dirtyLEFT MAIN GEAR GREEN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS LOWERED. THE LIGHTS DID NOT PRESS TO TEST WITH GEAR HANDLE UP OR DOWN. CLEANED SWITCH CONTACTS AND RELAMPED, OPERATION NORMAL.SDR DL767990334Power Supply · inopROW 37 AND BACK EMERGENCY LIGHTS INOP. REPLACED BATTERY SUPPLY PACK M9010, CKS GOOD.SDR DL767990158Actuator · failedLEFT MAIN GEAR REMAINED DOWN ON DEPARTURE FROM LAX. LOWERD LANDING GEAR AND RECEIVED NORMAL INDICATION. RETURNED TO LAX. TROUBLESHOOTING REVEALED LT GEAR SIDE LOCK ACTUATOR BYPASSING. REMOVED ROD END AND FOUND UPPER PORTION OF ROD ATTACHED TO PISTON SHEARSDR DL767981766Light · inoperativeAFT EMERGENCY LIGHT ON SEAT 25F INOP. REPLACED LIGHT ASSY, CKS GOOD.SDR DL767980419Wedge · delaminationTHE UPPER SKIN OF THE LT WING NR 4 SLAT TRAILING EDGE WEDGE WAS FOUND WITH 2 AREAS 2 INCH DIAMETER DELAMINATIONS. THE THE DAMAGE WAS REPAIRED PER THE B767 SRM AND DOCUMENTED PER ER/A 364074-14AD.SDR DL767980328Power Supply · inoperativeSECTIONS OF SEAT MOUNTED EMERGENCY LIGHTING INOP. FOUND ON PREFLIGHT. REPLACED POWER SUPPLY, SYSTEM CKS GOOD.SDR DL767971506Skin · corrosionCORROSION DAMAGE TO THE WING CENTER SECTION UPPER SKIN WAS FOUND AT NUMEROUS LOCATIONS AT THE UPPER SKIN TO STRINGER ATTACH FASTENER HOLES ON STR 1 TO 8, 10 TO 12, 14 AND 15. ALSO, CORROSION WAS FOUND AROUND SEVERAL SKIN TO REAR SPAR ATTACH FASTENER HOLES. RSDR DL767971505Seat Track · crackedTHE FUSELAGE SEAT TRACKS LOCATED AT LBL 33, 55 AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROX FS 786 AS DESCRIBED IN S/B 767-57-0029. IN ADDITION, PREVENTATIVE MODIFICATIONS TO THE LBL/RBL 33 AND LBL/RBL 54 FLOORBEAMS ARE BEINGSDR DL767971504Skin · corrosionCORROSION WAS FOUND JUST AFT OF STA 1307 UNDER THE UHF ANTENNA BOX. THE DAMAGE WAS CUTOUT AS SHOWN IN FIGURE 1. THE SKIN AT THIS LOCATION HAS A MAX THICKNESS OF .135 AND IS CHEM-MILLED FROM 2024-T3 CLAD SHEET. A PREVIOUS REPAIR IS LOCATED JUST FORWARD OF THSDR DL767971482Skin · corrosionCORROSION WAS DISCOVERED ON THE UPPER SURFACE OF THE WING CENTER SECTION UPPER SKIN PANELS AT BUTT SPLICE BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRINGER 17, BETWEEN RBL 74.81 AND 97.42. THE SKIN WAS TRIMMED TO REMOVE THE CORROSION IN THE FORWARD AND AFT SDR DL767970336Slat · damagedA/C DIVERTED INTO MCO WITH FLAP/SLATS LOCKOUT. ON ARRIVAL, FOUND NR 8 SLAT DAMAGED. REPLACED NR 8 SLAT, OPS CHECK NORMAL.SDR DL767970089Battery Pack · dischargedRT OVERWING SLIDE AND LEFT SPOILER SQUIBS FAILED TEST ON THE MAINTENANCE PANEL. REPLACED THE BATTERY PACK.SDR DL767970117Skin · corrosionSKIN AND STRINGERS WERE FOUND CORRODED AT FS 1540 BETWEEN STR 34L AND 39L. A 3.75 BY 2.25 CUTOUT WAS MADE. STRS 34L TO 39L REQUIRED NEW SECTIONS TO BE SPLICED IN. ADDITIONAL DAMAGE WAS FOUND AFTER INITIAL RELEASE OF ER/A. A SECOND 2 BY 3 CUTOUT WAS MADE BESDR DL767962732Skin · corrodedNR 95 CORROSION THROUGH FUSELAGE SKIN AT STA 1542 STR 35. NR 177 THROUGH 182 WRITTEN FOR STRINGER DAMAGE STR 34L THROUGH 39L WILL REPAIR PER ERA 360836-14 AS OF 12/19/96 ERA PENDING FAA APPROVAL.SDR DL767962148Fan · shortedSTRONG ELECTRICAL ODOR IN AIRCRAFT ON TAXI-OUT. FWD EXHAUST EQUIPMENT COOLING FAN POPPED C/B. FWD TO MCO AND PLAC PER MEL 21-58-04A, NEEDS FAN DAL 211002542.SDR DL767960829Actuator · failedDURING FLT CONTROL CHECK, AILERON AND ELEVATOR FELT VERY HEAVY. AIRCRAFT RETURNED TO BLOCK. REPLACED RT LCCA, RIGGED AND LEAK CHECKED, OPERATION NORMAL.SDR DL767960691Light · inoperativeON LAYOVER, FOUND LEFT AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK.SDR DL767960729Sensor · out of adjustON TAKEOFF, GEAR COULD NOT BE RAISED WITHOUT USING LOCK OVERRIDE. AIRCRAFT WAS FERRIED ATL FOR REPAIRS. PSEU SHOWS 246 RT GEAR TILT TARGET SHOWS FAR RESET. ADJUSTED SENSOR PER MM, OPERATION NORMAL.SDR DL767954712Fan · failedELECTRICAL SMELL IN COCKPIT AT CRUISE. FORWARD EQ EXHAUST FAN EICAS MSG. SMELL DISSIPATED IN COCKPIT. F/A REPORTED SMELL DIRECTED AFT THROUGH CABIN. FOUND FAN AT FAULT. DEFERRED PER MEL, THEN REPLACED FAN, OPERATION NORMAL.SDR DL767951153Flap · cap damagedFOUND DURING O-2 CHECK, NR 1 FLAP L/E CAP DAMAGED 2 PLACES. INSTALLED PERMANENT REPAIR AS PER SRM 51-70-03 FIG 201.
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