# Service difficulty reports: Airbus A350-941

A list on [Airbus A350-941](https://openairdocs.org/model/airbus-a350-941.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 730 reports

- [SDR DALA2026102105804](https://openairdocs.org/sdr/DALA2026102105804.md): Floor Panel · damaged · Oct 16, 2026 · N507DN · Airbus A350941 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152GAF DAMAGED. FABRICATED FLOOR PANEL 152DAF PER ERA 637563-14 REV ORIGINAL AND ASR A350-A-53-02-XX-07001-6621A-A UP TO STEP 4.C.(5) OK TO TREAT & PRIME QC 2013. TREATED, PRIMED AND PAINTED PER ERA 637563-14 REV ORIGINAL SEC III STEP 2.
- [SDR DALA2026102105803](https://openairdocs.org/sdr/DALA2026102105803.md): Floor Panel · damaged · Oct 16, 2026 · N507DN · Airbus A350941 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151DAF DAMAGED. FABRICATED FLOOR PANEL 152DAF PER ERA 637563-14 REV ORIGINAL AND ASR A350-A-53-02-XX-07001-6621A-A UP TO STEP 4.C.(5) OK TO TREAT & PRIME QC 2013. TREATED, PRIMED AND PAINTED PER ERA 637563-14 REV ORIGINAL SEC III STEP 2.
- [SDR DALA2026101505671](https://openairdocs.org/sdr/DALA2026101505671.md): Elevator · ground damage · Oct 11, 2026 · N512DN · Airbus A350941 · Wing Miscellaneous Structure
  > DAMAGE- AIRCRAFT RTB DUE LEFT WING STRUCK THE RIGHT ELEVATOR OF AIR CANADA AIRCRAFT, WHILE TAXIING. THE WINGLET SEVERED AND STUCK IN THE ELEVATOR OF THE OTHER AIRCRAFT. CORRECTIVE ACTION: WINGLET REPLACED. (LP# 8319112, 1852024, 1852021, 8319116, 8319118; AIRC
- [SDR DALA2026101505670](https://openairdocs.org/sdr/DALA2026101505670.md): Slide · faulty · Oct 8, 2026 · N503DN · Airbus A350941 · Escape Slide
  > 2L WONT ARM, AT DEPARTURE. REMOVED 2L SLIDE PER W/C 2560-4001. OK TO INSTALL L2 SLIDE (QC5458) INSTALLED SLIDE PER W/C 2562=4001 OPS 2562-4001 OPS CHK GOOD. (LP# 8808022; AIRCRAFT WAS GROUNDED)
- [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 DALA2026100505478](https://openairdocs.org/sdr/DALA2026100505478.md): Lamp · inoperative · Sep 29, 2026 · N509DN · Airbus A350941 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTING INOP AT SEATS 30C, 30G AND 44G. RELAMPED EMERGENCY FLOOR PATH LIGHT AT SEAT 30C AS REQUIRED. CONFIRMED THAT EMERGENCY FLOOR PATH LIGHTING AT 30G AND 44G ARE INOP. WIRE HARNESS PLUGS FOUND BAD. MOVED TO MEL 33-50-07A. (LP# 9339079
- [SDR DALA2026093005438](https://openairdocs.org/sdr/DALA2026093005438.md): Tire · low pressure · Sep 26, 2026 · N516DN · Airbus A350941 · Tire
  > DECLARED AN EMERGENCY, DUE TO NR 5 TIRE PRESSURE LOW ECAM. REPLACED THE NR 5 & 6 MLG TIRE ASSEMBLIES. (LP# 3604400; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805396](https://openairdocs.org/sdr/DALA2026092805396.md): Bypass Valve · faulted · Sep 24, 2026 · N574DZ · Airbus A350941 · Hydraulic System, Main
  > DE- DUE TO YELLOW HYDRAULIC TEMP HIGH ECAM MESSAGE. REPLACED HEAT EXCHANGER BYPASS VALVE (5050JM22). (LP# 9512789; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091705187](https://openairdocs.org/sdr/DALA2026091705187.md): Flap System · faulted · Sep 16, 2026 · N514DN · Airbus A350941 · Trailing Edge Flap Control System
  > DECLARED AN EMERGENCY DUE TO FLAPS LOCKED AT 5. FOUND FLAP SYSTEM 1+2 FAULT. PERFORMED FAULT CONFIRMATION AND FLAP SYSTEM 1 FAULTS. PLACED FLAP SYSTEM 1 ON MEL. (LP# 8540861: AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091105084](https://openairdocs.org/sdr/DALA2026091105084.md): Elec Connector · faulted · Sep 5, 2026 · N568DZ · Airbus A350941 · Light System Wiring
  > SEAT 20 B EMERGENCY LIGHT INOPERATIVE. RE-SEATED EMERGENCY PATHWAY LIGHT ELEC CONNECTOR AT SEAT 20B. OPS TESTED OK. IAW AMM 33-51. OK FOR SERVICE.
- [SDR DALA2026091105085](https://openairdocs.org/sdr/DALA2026091105085.md): Elec Connector · disconnected · Sep 1, 2026 · N505DN · Airbus A350941 · Light System Wiring
  > DURING CABIN WALK AROUND FOUND MULTI SEAT-MOUNTED LIGHTS INOPERATIVE. T/S IAW AWM 33-51-XX-00000-059A-A. FOUND CONNECTOR AT 541WL43 DISCONNECTED. RECONNECTED AND TESTED IAW AMM 33-51. NOW ALL EMERGENCY LIGHTS WORK NORMALLY. MEL AND PLAC REMOVED. (LP# 1789817
- [SDR DALA2026090405000](https://openairdocs.org/sdr/DALA2026090405000.md): Floor Panel · delaminated · Sep 1, 2026 · N519DN · Airbus A350941 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152MAF DELAMINATED AFT END. INSTALLED TEMP METAL REPAIR IAW ASR 53-02-XX-07001-662A. (LP# 9166816; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090104935](https://openairdocs.org/sdr/DALA2026090104935.md): Elec Connector · not seated · Aug 27, 2026 · N503DN · Airbus A350941 · Light System Wiring
  > ON A SERVICE CHK, FOUND SEATS 20 H/J AND 21 H/J EMERGENCY LIGHTS INOPERATIVE. DEFERRED TO MEL 33-50-07A, PLACARD INSTALLED. NO M PROCEDURES. OK FOR SERVICE. RE SEATED CONNECTOR AT 542WL43. NOW CHECKS OK PER A350 AMM 33-51. MEL AND PLACARD REMOVED. (LP 931717
- [SDR DALA2026090104934](https://openairdocs.org/sdr/DALA2026090104934.md): Elec Connector · misinstalled · Aug 26, 2026 · N531DN · Airbus A350941 · Light System Wiring
  > EMERGENCY LIGHT AT SEAT 8A INOPERATIVE. DEFERRED TO MEL 33-50-07A. CONFIRMED 28VDC. FOUND MISSING GND AT P-J3 (988017). T/S FOUND CONNECTOR PARTIALLY INSTALLED T SEAT 7A INTERCONNECT TO 8A REF A350 WDM 33 -51. OPS CHECKS GOOD AFTER SEATING CONNECTOR FOR 7A.
- [SDR DALA2026081904729](https://openairdocs.org/sdr/DALA2026081904729.md): Skin · damaged · Aug 18, 2026 · N515DN · Airbus A350941 · Leading Edge Devices
  > RIGHT INBD DROOP NOSE DAMAGED. REPAIRED REF: A350 - ASR - A350-A-57-44-63-01001-664A-A - SLAT 1 INBOARD (DROOP NOSE) - DROOP NOSE - NOSE SKIN BETWEEN RIBS - PERMANENT REPAIR (CATEGORY A PERM REPAIR) (1763331) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026081704687](https://openairdocs.org/sdr/DALA2026081704687.md): Light · damaged · Aug 15, 2026 · N506DN · Airbus A350941 · Emergency Lighting
  > SEAT 40A/B EMER LIGHT MISSING/DAMAGED. REPAIRED WIRING HARNESS AND REPLACED LAMP ASSY AMM 33-51. (8774318) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026081404651](https://openairdocs.org/sdr/DALA2026081404651.md): Actuator · faulted · Aug 13, 2026 · N512DN · Airbus A350941 · Drag Control Actuator
  > MISC/DE- DUE TO (F/CTL PART SPLRS) FAULT DURING DESCENT. PLACED SPOILER NR 1 ON MEL 27-64-01A FOR DEACTIVATION WITHOUT COLLAR. (9094850) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026072804375](https://openairdocs.org/sdr/DALA2026072804375.md): Torsion Bar · damaged · Jul 27, 2026 · N519DN · Airbus A350941 · Landing Gear Doors
  > SHIP 3519 -MISC/DE- DUE TO LEFT LANDING GEAR DOOR DID NOT CLOSE AFTER GEAR EXTENSION. FOUND UPLOCK TORSION BAR DAMAGED. REPLACED SHEARED TORSION BAR AND INSTALLED SERVICEABLE UPLOCK FITTING. (L/P# 8393242, 8393243; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072804374](https://openairdocs.org/sdr/DALA2026072804374.md): Switch · faulted · Jul 27, 2026 · N529DN · Airbus A350941 · Weather Radar System
  > SHIP 3529 -DIV- TO SYD DUE TO NR 12 AFDX SWITCH FAULT WITH ASSOCIATED WXR FAULTS. REPLACED AFDX SWITCH 12 AND AESU #1. (LP# 89326952, 8926954, 8926957, 8926956, 8926958; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072804373](https://openairdocs.org/sdr/DALA2026072804373.md): Spar · damaged · Jul 26, 2026 · N515DN · Airbus A350941 · Wing Spar
  > LEFT CENTER WING FRONT SPAR FOUND OVERSIVE FASTENER DURING INSPECTION. LT CENTER WING FRONT SPAR FASTENER INSTALLED IAW ER/A 635874- 14 PRI REV 0 AND VA 103207 IN CONJUNCTION WITH WORK CARD 5714- 01003-05. COMPARED WITH FINAL ER/A 635874-14 AD REV 0 AND VA 103
- [SDR DALA2026072004250](https://openairdocs.org/sdr/DALA2026072004250.md): Skin · damaged · Jul 19, 2026 · N509DN · Airbus A350941 · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE APPROX FR34 - FR38 AND STR 34L - STR 33L HAS IMPACT DAMAGE.PERFORMED REPAIR TO SKIN AT FRAME 34 THROUGH FRAME 38 BETWEEN STRINGER 33 LEFT AND 34 LEFT IAW ER/A 635574-14, REV O. REPAIR IS LIFE LIMITED FOR 200 FLIGHT CYCLES AT THIS TIME. A/C OK FOR
- [SDR DALA2026090405001](https://openairdocs.org/sdr/DALA2026090405001.md): Tape · damaged · Jul 8, 2026 · N520DN · Airbus A350941 · Fuselage Miscellaneous Structure
  > WHILE WORKING WORKCARD 5325-01020-01A, FOUND SEALING TAPE IN UNPERMISSABLE CONDITION IN VARIOUS LOCATIONS THROUGHOUT FWD CARGO. PERFORMED TEMPORARY REPAIR TO ALL IMPERMISSIBLE LOCATIONS IAW ASR A350-A-53-02-XX-18001 -662A-A, (LP# 8776030; AIRCRAFT WAS GROUN
- [SDR DALA2026071404137](https://openairdocs.org/sdr/DALA2026071404137.md): Coffeemaker · damaged · Jul 7, 2026 · N501DN · Airbus A350941 · Buffet/Galleys
  > COFFEE MAKER DAMAGED, INOPERATIVE, AFT GALLEY COFFEE MAKER MADE POPPING SOUND AND THEN SMELLED ACRID SMELL. TURNED OFF UNIT AND SMELL WENT AWAY / INTERIOR. REMOVED BEVERAGE MAKER AND INSPECTED WIRING HARNESS AND ASSOCIATED CONNECTORS. NO DEFECTS NOTED. INSTAL
- [SDR DALA2026070503915](https://openairdocs.org/sdr/DALA2026070503915.md): Sealant · unknown · Jul 3, 2026 · N515DN · Airbus A350941 · Wing Miscellaneous Structure
  > W/C 5720-01102-05B -OUTER WING GLOW SEALANT OPTIMISATION RH WING. ACCOMPLISHED SEALANT APPLICATION AND INSPECTION PER W/C 5720-01102-05B AS PER STEP 23 W/C 5720-01102-05B AND TOPP 20-50-20. (LP 1680046 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070503914](https://openairdocs.org/sdr/DALA2026070503914.md): Sealant · unknown · Jul 3, 2026 · N515DN · Airbus A350941 · Wing Miscellaneous Structure
  > W/C 5720-01102-05A -OUTER WING GLOW SEALANT OPTIMISATION RT WING. ACCOMPLISHED SEALANT APPLICATION AND INSPECTION IAW W/C 5720-01102-05A AS PER STEP 23 W/C 5720-01102-05A AND TOPP 20-50-20. (LP 1680056 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062903824](https://openairdocs.org/sdr/DALA2026062903824.md): Wire · detached · Jun 24, 2026 · N505DN · Airbus A350941 · Light System Wiring
  > 30C FLOOR PATH SEAT MOUNTED LIGHT INOP. RE-TERMINATE CONNECTOR, EEPLS LIGHT CK GOOD PER CMM 25-26-91 AND A350 AWM 33-51. CLEARED MEL AND PLACARD REMOVED. (LP# 9214822; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503570](https://openairdocs.org/sdr/DALA2026061503570.md): Power Supply · no test · Jun 12, 2026 · N507DN · Airbus A350941 · Emergency Lighting
  > DURING EPSU CAP TEST FOUND FAULT 3350F00E. R/R EPSU 101WL2 REF A350 AMM 33-51 OPS CK GOOD (LP# 8318595; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060803424](https://openairdocs.org/sdr/DALA2026060803424.md): Battery Pack · inoperative · Jun 4, 2026 · N505DN · Airbus A350941 · Emergency Lighting
  > 3L BATTERY PACK INOP. FAULT 3350F0002 ON P.F.R. T/S AS PER A350 TSM 33-51-XX-01001- 421A-A, FAULT CONFIRMED. REPLACED EPSU BATTERY 111WL3, TEST PASS. MEL AND PLACARDS REMOVED. (LP# 8052101; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060803425](https://openairdocs.org/sdr/DALA2026060803425.md): Elec Connector · not seated · May 30, 2026 · N529DN · Airbus A350941 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHTS INOP AT SEAT 34G/36G. T/S PER A350 TSM 33-51-XX-0K043-421A-A AND FOUND J13 CONNECTOR NOT FULLY SEATED. RE-SEATED CONNECTOR AND LIGHTS OPS NORM. MEL/PLACARD REMOVED. 'M' PROC REVERSED. (LP# 8885250; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060303381](https://openairdocs.org/sdr/DALA2026060303381.md): Floor Panel · not reported · May 30, 2026 · N529DN · Airbus A350941 · Fuselage Floor Panel
  > AFT CARGO HAS NON PERMISSIBLE CARGO FLOOR SEAL AREAS PER CARD 5325-1020-01B ON PANELS 152MAF,152LAF,152KAF,151HAF. PERFORMED TEMP REPAIR PER A350 ASR A350-A-53-02-XX-180001-662- A-A ON PANELS 152MAF, 152LAF,152KAF,151HAF. PER STEP 7 OF CARD 5325-01020-01B ALL
- [SDR DALA2026060303380](https://openairdocs.org/sdr/DALA2026060303380.md): Floor Panel · not reported · May 30, 2026 · N529DN · Airbus A350941 · Fuselage Floor Panel
  > FWD CARGO HAS NON PERMISSIBLE CARGO FLOOR SEAL AREAS PER CARD 5325-1020-01A ON PANELS 131BAF, 132QAF, 131HAF, 131KAF. PERFORMED TEMP REPAIR PER A350 ASR A350-A-53-02-XX-180001-662- A-A ON PANELS 131BAF, 132QAF, 131HAF, 131KAF. PER STEP 7 OF CARD 5325-01020-01A
- [SDR DALA2026052603172](https://openairdocs.org/sdr/DALA2026052603172.md): Wire · damaged · May 26, 2026 · N570DZ · Airbus A350941 · Light System Wiring
  > SEAT 20J EMER LIGHT INOP. REPAIRED WIRING PER A350 AMM 33-51. (7895150) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026052603171](https://openairdocs.org/sdr/DALA2026052603171.md): Sealant · damaged · May 25, 2026 · N514DN · Airbus A350941 · Wing Main, Frame Structure
  > OUTER WING GLOW SEALANT OPTIMISATION RH WING A350. CORRECTIVE ACTION: ACCOMPLISHED SEALANT APPLICATION AND INSPECTION PER W/C 5720-01102-05B. LOG PAGE GENERATED AND SDR REPORTABLE CHECKBOX MARKED AS PER STEP 23 W/C 5720-001102-05B AND TOPP 20-50-20. (1611373)
- [SDR DALA2026052603170](https://openairdocs.org/sdr/DALA2026052603170.md): Sealant · damaged · May 25, 2026 · N514DN · Airbus A350941 · Wing Main, Frame Structure
  > OUTER WING GLOW SEALANT OPTIMISATION LH WING A350. ACCOMPLISHED SEALANT APPLICATION AND INSPECTION PER W/C 5720- 01102-05A. AS PER STEP 23 W/C 5720-001102-05A AND TOPP 20-50-20. (1611275) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026051803048](https://openairdocs.org/sdr/DALA2026051803048.md): Door Seal · damaged · May 18, 2026 · N531DN · Airbus A350941 · Passenger/Crew Doors
  > DIV- TO MIA DUE TO NOISE/VIBRATION IN THE AFT CABIN. R/R 4L AND 4R DOOR SEAL. PRESSURIZATION AND LEAK CHECK GOOD. (LP# 8613808; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051803049](https://openairdocs.org/sdr/DALA2026051803049.md): Pump · leaking · May 16, 2026 · N575DZ · Airbus A350941 · Hydraulic Pump (Electric/Engine), Main
  > DE- DUE TO NUMBER ONE ENGINE GREEN HYDRAULIC PUMP FAULT WITH GREEN RESERVOIR LOW MESSAGE. FOUND FLUID LEAKING FROM PUMP HOUSING. REPLACED #1 G EDP AND #2 G EDP. (LP# 8857255, 8857254, 1595497; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051202969](https://openairdocs.org/sdr/DALA2026051202969.md): Engine · stalled · May 10, 2026 · N518DZ · Airbus A350941 · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTED ON TAKEOFF POSSIBLE LIGHTNING STRIKE WITH LEFT ENGINE STALL MESSAGE. T/S LEFT ENGINE LIGHTNING INDUCED STALL MESSAGE PER A350TSM. PERFORMED BOROSCOPE INSPECTION ON LEFT ENGINE WITH NO RESTRICTIVE DAMAGE NOTED. (L/P# 1586468, 1586423, 158
- [SDR DALA2026043002745](https://openairdocs.org/sdr/DALA2026043002745.md): Light · intermittent · Apr 26, 2026 · N501DN · Airbus A350941 · Emergency Lighting
  > 2L GREEN RUNNING MAN EXIT SIGN DID NOT ILLUMINATE ON ARRIVAL. NEED LIGHT COVER LIGHT IS INTERMITTENT. REMOVED AND REPLACED LIGHT ASSEMBLY PER 350WDM 33-5. OPS CK GOOD. OK FOR SERVICE. (LP# 8858106)
- [SDR DALA2026042202597](https://openairdocs.org/sdr/DALA2026042202597.md): Drain Line · damaged · Apr 21, 2026 · N512DN · Airbus A350941 · Hydraulic System, Main
  > MISC/DE- DUE TO YELLOW HYDRAULIC SYSTEM LOSS. FOUND NUMBER 2 ENGINE EDP CASE DRAIN LINE DAMAGED AT SADDLE CLAMP. SAME REPLACED. REPLACED EDPS AND RELATED HP FILTERS, CASE DRAIN FILTERS ON BOTH THE ENGINES, PER AIRBUS RECOMMENDATION. (LP# 8370426, 8370427, 83
- [SDR DALA2026042202596](https://openairdocs.org/sdr/DALA2026042202596.md): Oxygen Gen · tripped · Apr 21, 2026 · N502DN · Airbus A350941 · Passenger Oxygen System
  > EA/EO DUE TO INCOMING OPEN UP CHECK FOUND AT DOOR #4L THE CHEMICAL GENERATOR DISCHARGED. REMOVED AND REPLACED O2 CONTAINERS AS PER A350 AMM A350-A-25-33- 66. PERFORMED OPERATIONAL TEST AS PER WORK CARD 3520-2001. (LP# 1555191)
- [SDR DALA2026041502403](https://openairdocs.org/sdr/DALA2026041502403.md): Tire · low pressure · Apr 13, 2026 · N572DZ · Airbus A350941 · Tire
  > DE- DUE TO NUMBER 7 TIRE PRESSURE LOW ECAM MESSAGE. FOUND TIRE PRESSURE AT 175 PSI. REPLACED NUMBER 7 AND 8 TIRE/WHEEL ASSEMBLIES. (LP# 8588038)
- [SDR DALA2026041002297](https://openairdocs.org/sdr/DALA2026041002297.md): Elec Connector · disconnected · Apr 6, 2026 · N515DN · Airbus A350941 · Light System Wiring
  > AIRCRAFT 3515, DURING SERVICE CHECK FOUND EMERGENCY LIGHT AT SEAT 20AB & 21AB INOP. FOUND CONNECTOR LOOSE AT FLOOR. DISCONNECTED BOX. RECONNECTED. NOW LIGHTS OPS NORMAL. AIRCRAFT WAS GROUNDED.
- [SDR DALA2026040602191](https://openairdocs.org/sdr/DALA2026040602191.md): Pump · damaged · Apr 3, 2026 · N513DZ · Airbus A350941 · Turbine Engine Oil System
  > AIRCRAFT DIVERTED TO ANF (ANTOFAGASTA, CHILE) AFTER THE FLIGHT CREW PERFORMED A RIGHT ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE. CORRECTIVE ACTION: INSPECTED NR 2 ENGINE PRESSURE FILTER, SCAVENGE FILTER AND ODMS. FOUND FERROUS METAL ON SENSORS. REPLACED NR 2 ENG
- [SDR DALA2026040302148](https://openairdocs.org/sdr/DALA2026040302148.md): Oil System · low pressure · Mar 31, 2026 · N513DZ · Airbus A350941 · Engine Oil Pressure
  > AIRCRAFT DIVERTED TO ANF (ANTOFAGASTA, CHILE) AFTER THE FLIGHT CREW PERFORMED A RIGHT ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE. OPEN
- [SDR DALA2026033102112](https://openairdocs.org/sdr/DALA2026033102112.md): Anti-Ice Valve · faulted · Mar 27, 2026 · N519DN · Airbus A350941 · Engine Anti-Icing System
  > AIRCRAFT DIVERTED TO LAX DUE TO RIGHT ENGINE STATOR ANTI-ICE VALVE CLOSED FAULT. FLIGHT UNABLE TO CONTINUE DUE TO ICING. PERFORMED RIGHT ENGINE FADEC SYSTEM TEST PER A350AMM, TEST OK AND MESSAGE CLEARED. (LP# 8376425)
- [SDR DALA2026033102111](https://openairdocs.org/sdr/DALA2026033102111.md): Elec Connector · loose · Mar 27, 2026 · N501DN · Airbus A350941 · Light System Wiring
  > PER CREW REPORT EMERGENCY EXIT LIGHT ABOVE DOOR 2L INOP. FOUND CONNECTOR ON LIGHT LOOSE, RESECURED CONNECTOR OPS TEST GOOD AT THIS TIME. (LP# 8181924)
- [SDR DALA2026032702029](https://openairdocs.org/sdr/DALA2026032702029.md): Coffeemaker · odor · Mar 25, 2026 · N529DN · Airbus A350941 · Buffet/Galleys
  > ELECTRICAL ODOR AT 1R, IMMEDIATELY SHUT OFF FORWARD GALLEY COFFEE MAKER, OVENS, AND CHILLERS. ODOR DECREASED IMMEDIATELY BUT COULD STILL SMELL IT. SHUT OFF CABIN FANS, SELECTED HI FLOW AND AVIONICS EXTRACT TO INCREASE AIRFLOW AND SHUT OFF GALLEY POWER ODOR FIN
- [SDR DALA2026032702030](https://openairdocs.org/sdr/DALA2026032702030.md): Display · faulted · Mar 24, 2026 · N523DN · Airbus A350941 · Communications System
  > ON INITIAL TAXI OUT THE SCREEN AT 2A POPPED, REBOOTED AND ACCOMPANIED WITH ELECTRICAL SMELL. RETURNED TO NORMAL AND RETURNED TO GATE. INSPECTED ORIG MONITOR, NO SMELL AND WORKING OK, R/R 2A MONITOR FOR PRECAUTION PER DELTA MTC. P/N RD-FJ7884-01. S/N ON H753552
- [SDR DALA2026032401981](https://openairdocs.org/sdr/DALA2026032401981.md): Eec · faulted · Mar 23, 2026 · N574DZ · Airbus A350941 · Fuel Controlling System
  > ATB- AIRCRAFT RETURNED TO SEA DUE TO RIGHT ENGINE STATOR ANTI-ICE VALVE CLOSED FAULT. FLIGHT CANNOT CONTINUE DUE TO ICING. REPLACED #2 ENGINE EEC. REMOVED WATER FROM P30 SENSOR TUBE. CARRIED OUT ENGINE OPERATIONAL TEST. NO FAULTS. OK FOR SVC. (LP# 8423850, 8
- [SDR DALA2026031001669](https://openairdocs.org/sdr/DALA2026031001669.md): Seal · out of position · Mar 9, 2026 · N526DN · Airbus A350941 · Cargo/Baggage Doors
  > WORKING W/C 5325-01020-01B FOUND ORIGINAL SEAL PUSHED OUT BEYOND 0.46 INCH ALONG 3 TRACKS RT OF TRACKS JUST FWD OF CARGO DOOR IN AFT CARGO. EACH TRACK HAS 6FT SECTIONS NEEDING TEMP REPAIR. REPAIRED AREAS IN AFT CARGO WITH GLASS CLOTH TAPE IAW ASR A350-A -53-02

Next page: https://openairdocs.org/model/airbus-a350-941/reports.md?page=2

## 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 aircraft_model_key = 'A350941'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a350-941/reports

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