# Service difficulty reports: N511DN

A list on [N511DN](https://openairdocs.org/aircraft/N511DN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DALA2026100505479](https://openairdocs.org/sdr/DALA2026100505479.md): Pump · failed · Oct 3, 2026 · N511DN · Airbus A350941 · Hydraulic Pump (Electric/Engine), Main
  > DE - 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)
- [SDR DALA2026021000944](https://openairdocs.org/sdr/DALA2026021000944.md): Tire · low pressure · Feb 9, 2026 · N511DN · Airbus A350941 · Tire
  > SHIP 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)
- [SDR DALA2026020500846](https://openairdocs.org/sdr/DALA2026020500846.md): Light · inoperative · Feb 2, 2026 · N511DN · Airbus A350941 · Emergency Lighting
  > LAV 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 REMOV
- [SDR DALA2024122411989](https://openairdocs.org/sdr/DALA2024122411989.md): Lens · missing · Dec 22, 2024 · N511DN · Airbus A350941 · Emergency Lighting
  > DURING SVC FOUND 1R LAV AFT EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LENS PER A350 AMM 33-51. OK FOR SERVICE. (LP# 6719720)
- [SDR DALA2025040102464](https://openairdocs.org/sdr/DALA2025040102464.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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
- [SDR DALA2025040102463](https://openairdocs.org/sdr/DALA2025040102463.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (430
- [SDR DALA2025040102462](https://openairdocs.org/sdr/DALA2025040102462.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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 L
- [SDR DALA2025040102461](https://openairdocs.org/sdr/DALA2025040102461.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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 ALLOWAB
- [SDR DALA2025040102460](https://openairdocs.org/sdr/DALA2025040102460.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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 LIGH
- [SDR DALA2025040102459](https://openairdocs.org/sdr/DALA2025040102459.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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-53-00-61-01001-661
- [SDR DALA2025040102458](https://openairdocs.org/sdr/DALA2025040102458.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (478
- [SDR DALA2025040102457](https://openairdocs.org/sdr/DALA2025040102457.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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, PLE
- [SDR DALA2025040102456](https://openairdocs.org/sdr/DALA2025040102456.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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) PLEAS
- [SDR DALA2025040102455](https://openairdocs.org/sdr/DALA2025040102455.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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-53
- [SDR DALA2025040102454](https://openairdocs.org/sdr/DALA2025040102454.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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) P
- [SDR DALA2025040102453](https://openairdocs.org/sdr/DALA2025040102453.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (430
- [SDR DALA2025040102452](https://openairdocs.org/sdr/DALA2025040102452.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (45884
- [SDR DALA2025040102451](https://openairdocs.org/sdr/DALA2025040102451.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (4788
- [SDR DALA2025040102450](https://openairdocs.org/sdr/DALA2025040102450.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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-A
- [SDR DALA2025040102449](https://openairdocs.org/sdr/DALA2025040102449.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LIGHTNING 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. (47888
- [SDR DALA2025040102448](https://openairdocs.org/sdr/DALA2025040102448.md): Skin · damaged · Nov 2, 2024 · N511DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > .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 C
- [SDR DALA2024041704502](https://openairdocs.org/sdr/DALA2024041704502.md): Fitting · migrated · Apr 11, 2024 · N511DN · Airbus A350941 · Horizontal Stabilizer Miscellaneous Structure
  > 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 FITTING. REAM MIGRATI
- [SDR DALA2024041504455](https://openairdocs.org/sdr/DALA2024041504455.md): Bushing · migrated · Apr 10, 2024 · N511DN · Airbus A350941 · Horizontal Stabilizer Structure
  > AIRCRAFT 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 FITTI
- [SDR DALA2024040404082](https://openairdocs.org/sdr/DALA2024040404082.md): None · none · Apr 1, 2024 · N511DN · Airbus A350941 · Standard Practices/Structures
  > AD/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 24
- [SDR DALA2024040404081](https://openairdocs.org/sdr/DALA2024040404081.md): None · none · Apr 1, 2024 · N511DN · Airbus A350941 · Standard Practices/Structures
  > AD/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 24
- [SDR DALA2023111409378](https://openairdocs.org/sdr/DALA2023111409378.md): Unknown · unknown · Nov 12, 2023 · N511DN · Airbus A350941 · Door Warning System
  > SHIP 3511 DOOR 2L WOULD NOT SHOW CLOSED & LOCKED ON COCKPIT DISPLAY. CORRECTIVE ACTION: CYCLED DOOR. OPS CKS FINE. DOOR ARMED OK. (4350978)
- [SDR DALA2023102208664](https://openairdocs.org/sdr/DALA2023102208664.md): Unknown · unknown · Oct 16, 2023 · N511DN · Airbus A350941 · APU Start/Ignition System
  > AIRCRAFT 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 THE
- [SDR DALA2023100308122](https://openairdocs.org/sdr/DALA2023100308122.md): Unknown · unknown · Sep 30, 2023 · N511DN · Airbus A350941 · Light System Wiring
  > SHIP 3511 EMERGENCY LIGHT AT SEAT AB INOP. CORRECTIVE ACTION: FOUND WIRE CONNECTOR OFF OF LIGHT IN SEAT ARMREST, RE-INSTALLED CKS OK. (4507411)
- [SDR DALA2023072706104](https://openairdocs.org/sdr/DALA2023072706104.md): Unknown · unknown · Jul 26, 2023 · N511DN · Airbus A350941 · Fuselage Structure (General)
  > SHIP 3511 INSTALLED CLOTH TAPE IN SEVERAL SPOTS IN AFT CARGO. CORRECTIVE ACTION: REF CARD 5325-01020-01B. (2885619)
- [SDR DALA2023072706103](https://openairdocs.org/sdr/DALA2023072706103.md): Unknown · unknown · Jul 26, 2023 · N511DN · Airbus A350941 · Fuselage Structure (General)
  > SHIP 3511 INSTALLED CLOTH TAPE IN SEVERAL SPOTS IN FWD CARGO. CORRECTIVE ACTION: REF CARD 5325-01020-01A. (2885585)
- [SDR DALA2023071105606](https://openairdocs.org/sdr/DALA2023071105606.md): Unknown · unknown · Jul 9, 2023 · N511DN · Airbus A350941 · Door Warning System
  > SHIP 3511 DUE CRDC B01 INOP, CBN DOOR 2L LOCK MONITORING CONSIDERED INOP. CORRECTIVE ACTION: CRDC B01 REPLACED, CK'S GOOD. (4855105)
- [SDR DALA2022101706708](https://openairdocs.org/sdr/DALA2022101706708.md): Eec · faulted · Oct 17, 2022 · N511DN · Airbus A350941 · Fuel Controlling System
  > RIGHT 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. (
- [SDR DALA2022060804004](https://openairdocs.org/sdr/DALA2022060804004.md): Cover · unlocked · Jun 3, 2022 · N511DN · Airbus A350941 · Escape Slide
  > SHIP 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)
- [SDR DALA2021063003596](https://openairdocs.org/sdr/DALA2021063003596.md): Warning Message · false activation · Jun 29, 2021 · N511DN · Airbus A350941 · Landing Gear Brake System
  > SHIP 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)
- [SDR DALA2021062803506](https://openairdocs.org/sdr/DALA2021062803506.md): Lens · missing · Jun 23, 2021 · N511DN · Airbus A350941 · Emergency Lighting
  > SHIP 3511 CLEAR LENS COVER EMERGENCY LIGHT MISSING AT OUTSIDE LAV R1. CORRECTIVE ACTION: REPLACED LIGHT LENS EMERGENCY COVER OUTSIDE LAV R1. (1850379)
- [SDR DALA2021032501792](https://openairdocs.org/sdr/DALA2021032501792.md): Door Frame · dented · Mar 24, 2021 · N511DN · Airbus A350941 · Fuselage Main, Structure
  > SHIP 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)
- [SDR DALA2021011300200](https://openairdocs.org/sdr/DALA2021011300200.md): Oxygen Mask · unwanted deploy · Jan 11, 2021 · N511DN · Airbus A350941 · Passenger Oxygen System
  > OXYGEN PANEL MASK DEPLOYED LOCATIONS: 42G. CORRECTIVE ACTION: 42G OXY MASK PANEL RESECURED.
- [SDR DALA2020100603304](https://openairdocs.org/sdr/DALA2020100603304.md): Rccb · malfunctioned · Oct 4, 2020 · N511DN · Airbus A350941 · Emergency Lighting
  > EMERGENCY 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.
- [SDR DALA2020091410095](https://openairdocs.org/sdr/DALA2020091410095.md): Skin · damaged · Sep 9, 2020 · N511DN · Airbus A350941 · Passenger/Crew Doors
  > UPON ARRIVAL AT CDG GROUND CREW REPORTED DAMAGE ON DOOR 4 LEFT OUTER SKIN. CORRECTIVE ACTION: TEMP REPAIR, PER ASR 51-77-12.
- [SDR DALA2020020701019](https://openairdocs.org/sdr/DALA2020020701019.md): Door · frozen · Feb 6, 2020 · N511DN · Airbus A350941 · Service Doors
  > DOOR 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, 7152541
- [SDR DALA201811206731](https://openairdocs.org/sdr/DALA201811206731.md): Wing · mismanufactured · Nov 14, 2018 · N511DN · Airbus A350941 · Standard Practices/Structures
  > AIRBUS 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 SEALAN
- [SDR DALA2021032501791](https://openairdocs.org/sdr/DALA2021032501791.md): Skin · delaminated · Jul 2, 2018 · N511DN · Airbus A350941 · Elevator, Plate/Skin
  > SHIP 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)

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N511DN/reports

---
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