N511DN

Service difficulty reports · 42

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 = 'N511DN' 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.

SDR DALA2026100505479Pump · failedDE - DUE TO GREEN SYSTEM HYDRAULIC QTY LOSS. REPLACED #1 AND #2 ENG EDP. PERFORMED ALTERNATE FLUSHING PROCEDURES AND REPLACED ALL ASSOCIATED FILTERS. (LP# 9333162, 9333163, 9333164, 9333170; AIRCRAFT WAS GROUNDED)Oct 3, 2026 · N511DN · Airbus A350941 · Hydraulic Pump (Electric/Engine), MainSDR DALA2026021000944Tire · low pressureSHIP 3511 -DE- DUE TO NUMBER 6 TIRE PRESSURE LOW ECAM MESSAGE. CORRECTIVE ACTION: FOUND NUMBER 6 TIRE READING 175PSI. REPLACED NUMBER 5 AND 6 WHEEL ASSEMBLIES. (LP# 8265202)Feb 9, 2026 · N511DN · Airbus A350941 · TireSDR DALA2026020500846Light · inoperativeLAV 2R EMERGENCY LIGHT INOP. REPLACED LIGHT W/ MPN: 8595-1-00. NO JOY. TESTED VOLTAGE AT LIGHT. NO VOLTAGE WHEN EMERGENCY LIGHTS ARE ACTIVATED. FWD TO MEL 33-50-09A. NO "M" PROCEDURES. PLACARD INSTALLED. RESEAT LIGHT. CHECKS GOOD FOR SERVICE, MEL PLACARD REMOVFeb 2, 2026 · N511DN · Airbus A350941 · Emergency LightingSDR DALA2024122411989Lens · missingDURING SVC FOUND 1R LAV AFT EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LENS PER A350 AMM 33-51. OK FOR SERVICE. (LP# 6719720)Dec 22, 2024 · N511DN · Airbus A350941 · Emergency LightingSDR DALA2025040102464Skin · damagedLIGHTNING STRIKE FASTENER FRAME 20 STRINGER 43 AND 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. PREVIOUS ITEM FOR MON REF ENTERED IN ERROR. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102463Skin · damagedLIGHTNING STRIKE FASTENER FRAME 20 STRINGER 41LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (430Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102462Skin · damagedLIGHTNING STRIKE FASTENER FRAME 21 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350 -A-53-00-61-01001-661A-A FOUND TEMP ALLOWABLE LNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102461Skin · damagedLIGHTNING STRIKE OFF FASTNER FRAME 19 STRINGER 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350 -A-53-00-61-01001-661A-A FOUND TEMP ALLOWABNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102460Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSP. PER A350-A-53 -00-61-01001-661A-A , FOUND TEMP ALLOWABLE LIGHNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102459Skin · damagedLIGHTNING STRIKE FRAME 18 STRINGER 44 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. PREVIOUS STEP MON REF ENTERED IN ERROR, REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSP. PER A350-A-53-00-61-01001-661Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102458Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 41LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (478Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102457Skin · damagedLIGHTNING STRIKE FRAME 17 BELOW STRINGER 45 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR PITTING AT FASTENER WITHIN LIMITS. RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. QA, PLENov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102456Skin · damagedLIGHTNING STRIKE FRAME 28 STRINGER 44LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (478884) PLEASNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102455Skin · damagedLIGHTNING STRIKE FASTENER FRAME 22 STRINGER 43LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . PREVIOUS ITEM FOR MON REF ENTERED IN ERROR. REEVALUATED LIGHTNING STRIKE WHILE DOING REP INSPECTION PER A350-A-53Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102454Skin · damagedLIGHTNING STRIKE FRAME 17 ABOVE STRINGER 45 L/H . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR DAMAGE/PITTING AT FASTENER TO BE WITHIN LIMITS PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (458844) PNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102453Skin · damagedLIGHTNING STRIKE FASTENER FRAME 25 STRINGER 44LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10 . FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (430Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102452Skin · damagedLIGHTNING STRIKE FRAME 16 STRINGER 45 L/H . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. FOUND MINOR PITTING AT FASTENER TO BE WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (45884Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102451Skin · damagedLIGHTNING STRIKE FASTENER FRAME 24 STRINGER 43LH . PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10. FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (4788Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102450Skin · damagedLIGHTNING STRIKE AT FRAME 14 STRINGER 45 L/H. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REMOVED TAPE FROM LIGHTNING STRIKE AREA. FOUND DAMAGE AREA PITTING WITHIN LIMITS PER ASR A350-A-53-00-61-01001-661A-ANov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102449Skin · damagedLIGHTNING STRIKE FASTENER FRAME 23 STRINGER 42LH. PERFORMED TEMP SKIN PROTECTION USING HIGH SPEED TAPE REF A350 ASR 53-21-61-00004-662A-A FIG 10. FOUND MINOR PITTING AT FASTENER, WITHIN LIMITS, RESTORED FINISH PER ASR A350-A-53-00-61-01001-661A-A FIG 3. (47888Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2025040102448Skin · damaged.LIGHTNING STRIKE 5" AFT FRAME 13 BETWEEN STRINGERS 44 AND 45. PERFORMED TEMP. SKIN PROTECTION USING HIGH SPEED TAPE. REF A350 ASR 53-21-61-00004-662-A-A FIG 10. REMOVED TAPE FROM LIGHTNING STRIKE AREA. FOUND DAMAGED AREA/ BURN MARK < 15.7MM. REPAIR OF PAINT CNov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/SkinSDR DALA2024041704502Fitting · migratedWHILE ACCOMPLISHING MP INSPECTION TASK A350-A-55-11-XX-1U001-281A-A TRIMMABLE HORIZONTAL STABILIZER SPAR BOX - DETAILED INSPECTION OF THS REAR SPAR, LATERAL LOAD FITTING, LH/RH, THE UPPER BUSHING WAS FOUND MIGRATED ON THE RH LATERAL LOAD FITTING. REAM MIGRATIApr 11, 2024 · N511DN · Airbus A350941 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2024041504455Bushing · migratedAIRCRAFT 3511, WHILE ACCOMPLISHING MP INSPECTION TASK A350-A-55-11-XX-1U001-281A-A TRIMMABLE HORIZONTAL STABILIZER SPAR BOX - DETAILED INSPECTION OF THS REAR SPAR, LATERAL LOAD FITTING, LH/RH, THE UPPER BUSHING WAS FOUND MIGRATED ON THE RH LATERAL LOAD FITTIApr 10, 2024 · N511DN · Airbus A350941 · Horizontal Stabilizer StructureSDR DALA2024040404082None · noneAD/EM-EO TASK - RH WING W/C 5720-01102-05B STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. RH WING SEALANT APPLIED AS PER W/C 5720-01102-05B STEP 11. FOUND SATISFACTORY AND W/C STEP 24Apr 1, 2024 · N511DN · Airbus A350941 · Standard Practices/StructuresSDR DALA2024040404081None · noneAD/EM-EO TASK - LH WING W/C 5720-01102-05A STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LH WING SEALANT APPLIED AS PER W/C 5720-01102-05A STEP 11. FOUND SATISFACTORY AND W/C STEP 24Apr 1, 2024 · N511DN · Airbus A350941 · Standard Practices/StructuresSDR DALA2023111409378Unknown · unknownSHIP 3511 DOOR 2L WOULD NOT SHOW CLOSED & LOCKED ON COCKPIT DISPLAY. CORRECTIVE ACTION: CYCLED DOOR. OPS CKS FINE. DOOR ARMED OK. (4350978)Nov 12, 2023 · N511DN · Airbus A350941 · Door Warning SystemSDR DALA2023102208664Unknown · unknownAIRCRAFT 3511, APU FAILED TO COLD START 3 ATTEMPTS FL390 TEMP-60- PEAK EGT 805. CORRECTIVE ACTION: DEFERRED PER MEL 49-10-01A (19OCT23 MSP - REMOVED THERMOCOUPLE 59KV34 9:00 POSITION. FOUND PIECE ON TIP OF PROBE BROKEN OFF. LOOKED UP TAILPIPE FOR 59KV35 AT THEOct 16, 2023 · N511DN · Airbus A350941 · APU Start/Ignition SystemSDR DALA2023100308122Unknown · unknownSHIP 3511 EMERGENCY LIGHT AT SEAT AB INOP. CORRECTIVE ACTION: FOUND WIRE CONNECTOR OFF OF LIGHT IN SEAT ARMREST, RE-INSTALLED CKS OK. (4507411)Sep 30, 2023 · N511DN · Airbus A350941 · Light System WiringSDR DALA2023072706104Unknown · unknownSHIP 3511 INSTALLED CLOTH TAPE IN SEVERAL SPOTS IN AFT CARGO. CORRECTIVE ACTION: REF CARD 5325-01020-01B. (2885619)Jul 26, 2023 · N511DN · Airbus A350941 · Fuselage Structure (General)SDR DALA2023072706103Unknown · unknownSHIP 3511 INSTALLED CLOTH TAPE IN SEVERAL SPOTS IN FWD CARGO. CORRECTIVE ACTION: REF CARD 5325-01020-01A. (2885585)Jul 26, 2023 · N511DN · Airbus A350941 · Fuselage Structure (General)SDR DALA2023071105606Unknown · unknownSHIP 3511 DUE CRDC B01 INOP, CBN DOOR 2L LOCK MONITORING CONSIDERED INOP. CORRECTIVE ACTION: CRDC B01 REPLACED, CK'S GOOD. (4855105)Jul 9, 2023 · N511DN · Airbus A350941 · Door Warning SystemSDR DALA2022101706708Eec · faultedRIGHT ENGINE STATOR ANTI ICE VALVE CLOSED MESSAGE. NO RESET IN AIR AND AVOID ICING CONDITIONS. CORRECTIVE ACTION: MAINTENANCE FOUND MULTIPLE RIGHT ENGINE EEC MESSAGES. T/S PER A350TSM, REPLACED RIGHT ENGINE EEC PER AMM. C/W OPERATIONAL TEST, NO FAULTS NOTED. (Oct 17, 2022 · N511DN · Airbus A350941 · Fuel Controlling SystemSDR DALA2022060804004Cover · unlockedSHIP 3511E - DOOR 3R ESCAPE SLIDE FALLING OUT. CORRECTIVE ACTION: FOUND DECORATIVE COVER NOT LOCKED IN POSITION. REPOSITIONED AND LOCKED PER A350 AMM 25-62.(8511627)Jun 3, 2022 · N511DN · Airbus A350941 · Escape SlideSDR DALA2021063003596Warning Message · false activationSHIP 3511 AFTER LANDING GEAR EXTENSION BRAKES PART ALTN + EMER BRK FAULT ECAM. CORRECTIVE ACTION: SEL VALVE-ALTN BRK, GREEN NOTED LATCHED.BITE TEST OF BSCS SYS TEST C/OUT. MESSAGE CLEARED. (7612786)Jun 29, 2021 · N511DN · Airbus A350941 · Landing Gear Brake SystemSDR DALA2021062803506Lens · missingSHIP 3511 CLEAR LENS COVER EMERGENCY LIGHT MISSING AT OUTSIDE LAV R1. CORRECTIVE ACTION: REPLACED LIGHT LENS EMERGENCY COVER OUTSIDE LAV R1. (1850379)Jun 23, 2021 · N511DN · Airbus A350941 · Emergency LightingSDR DALA2021032501792Door Frame · dentedSHIP 3511 BULK CARGO DOOR OPENING CUT-OUT AFT SIDE ADJACENT TO 2ND FROM BOTTOM DOOR STOP FITTING SMALL DENT. CORRECTIVE ACTION: CHECKED DENT LIMITS REF. A350 ASR 53-41 AND RESTORED FINISH REF A350 ASR 51-75. WITHIN LIMITS. NO DISBOND NOTED. (1763526)Mar 24, 2021 · N511DN · Airbus A350941 · Fuselage Main, StructureSDR DALA2021011300200Oxygen Mask · unwanted deployOXYGEN PANEL MASK DEPLOYED LOCATIONS: 42G. CORRECTIVE ACTION: 42G OXY MASK PANEL RESECURED.Jan 11, 2021 · N511DN · Airbus A350941 · Passenger Oxygen SystemSDR DALA2020100603304Rccb · malfunctionedEMERGENCY EXIT LIGHTS ON FROM 1ST CLASS TO DOOR 3 ON NOT ABLE TO RESET. CREW REST EMERGENCY LIGHTS ON. CORRECTIVE ACTION: T/S AND R/R RCCB 102XP, PER A350 A-24-71-57. EPDS TEST PASSED MESSAGE CLEARED EMERGENCY LIGHTTS OPERATIONS NORMAL.Oct 4, 2020 · N511DN · Airbus A350941 · Emergency LightingSDR DALA2020091410095Skin · damagedUPON ARRIVAL AT CDG GROUND CREW REPORTED DAMAGE ON DOOR 4 LEFT OUTER SKIN. CORRECTIVE ACTION: TEMP REPAIR, PER ASR 51-77-12.Sep 9, 2020 · N511DN · Airbus A350941 · Passenger/Crew DoorsSDR DALA2020020701019Door · frozenDOOR 2R WILL DISARM BUT WILL NOT OPEN. SUSPECT FROZEN. MOVED TO HANGAR, THAWED DOOR, AND DRAINED HALF A GALLON OF WATER FROM BOTTOM OF DOOR FRAMED. LP 7152539, 7152541Feb 6, 2020 · N511DN · Airbus A350941 · Service DoorsSDR DALA201811206731Wing · mismanufacturedAIRBUS AOT A57P011-18-00 EXPLAINS THAT SOME WING RIB TO WING LOWER SKIN GAPS WERE NOT FILLED IN PRODUCTION AS REQUIRED. UNFILLED GAPS COULD ALLOW CONTACT AND SPARKS AND POTENTIAL EWIS CONCERNS. WORK TO BE COMPLETED, APPLY ADHESION PROMOTER, MIX AND POUR SEALANNov 14, 2018 · N511DN · Airbus A350941 · Standard Practices/StructuresSDR DALA2021032501791Skin · delaminatedSHIP 3511 IMPACT DAMAGE WHICH DELAMINATED AND CRACKED THE UPPER SKIN FORWARD OF THE ELEVATOR SPAR. CORRECTIVE ACTION: COMPLIED WITH ERA 569601-14 PERMANENT REPAIR. (0628982)Jul 2, 2018 · N511DN · Airbus A350941 · Elevator, Plate/Skin
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