- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 0265
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 2, 2022
- Certificate issued
- July 15, 2021
- Expires
- July 31, 2028
- Mode S code
- A75DA8
Airbus A350-941TCDS T00063IBAirframe · Airbus A350-941TCDS E00086ENEngine · Rolls-Royce TRENT XWB-84
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 124
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2017 | 3 |
|---|---|
| 2018 | 13 |
| 2019 | 18 |
| 2020 | 22 |
| 2021 | 19 |
| 2022 | 21 |
| 2023 | 26 |
| 2024 | 13 |
| 2025 | 17 |
| 2026 | 13 |
See all 165 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N574DZMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A350-941 aircraft
FAA incident reports
No FAA accident or incident reports matched to N574DZMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A350-941 aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026092805396Bypass Valve · faultedDE- DUE TO YELLOW HYDRAULIC TEMP HIGH ECAM MESSAGE. REPLACED HEAT EXCHANGER BYPASS VALVE (5050JM22). (LP# 9512789; AIRCRAFT WAS GROUNDED)SDR DALA2026032401981Eec · faultedATB- 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, 8SDR DALA2025080105758O-Ring · leakingCREW DIVERTED TO ANC DUE TO REPORTED FUEL LEAK SUSPECTED ECAM MESSAGE WITH 8,000LB BELOW PLANNED BURN. REPLACED O-RINGS FOR ENGINE CORE FUEL TUBES P/N FW83547 AND FW83548. PERFORMED LEAK CHECK AND RTS. (LP# 7569084)SDR DALA2025061204473Elec Connector · looseDISPATCH MSG CABIN EMER EXIT LIGHT ON ECAM. R/R EPSU NO 101WLA A3UVE 1R DOOR. PER A350 AMM 33-51. NO HELP. WHILE T/S FOUND CANNON PLUG LOOSE FWD OF 1R DOOR. SECURED OPS CHECK GOOD. AFTER 20 MIN MSG CAME BACK STILL T/S (184563) RESET EPSU'S 8EA. IAW A350 AMM -ASDR DALA2025050503447Sealant · missingAD/EM-EO TASK - LH WING W/C 5720-01102-08A STEP 13. REPAIR LH WING REAR LOWER SEALANT APPLIED AS PER W/C 5720-01102-08A STEP 6. FOUND SATISFACTORY AND W/C STEP 13SDR DALA2025050503446Sealant · missingAD/EM-EO TASK - RH WING W/C 5720-01102-08B STEP 29. RH WING REAR LOWER SEALANT APPLIED AS PER W/C 5720-01102-08B STEP 6. FOUND SATISFACTORY AND W/C STEP 13 "SDR REPORTABLE" CHECKBOX IS MARKED. (LP# 0933625)SDR DALA2025032702248Unknown · unknownAD/EM-EO TASK - LH WING W/C 5720-01102-06A STEP 35. 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 5720-01102-06A STEP 15. FOUND SATISFACTORY AND W/C STEP 35SDR DALA2025032702247Unknown · unknownAD/EM-EO TASK - RH WING W/C 5720-01102-06B STEP 29. 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 5720-01102-06B STEP 13. FOUND SATISFACTORY AND W/C STEP 29SDR DALA2024060405786Unknown · odorAFTER CLOSING A/C CABIN DOOR INTERNMENT ELECTRICAL SMELL AROUND ROW 17,18,19. NOTICED BY PASSENGER AND FLIGHT ATTENDANTS. REF LOGPAGE#0375129. NO ISSUES NOTED AT THIS TIME. A/C OK FOR SVC. (LP# 5816334)SDR DALA2026030301463Skin · damagedFOUND LIGHTNING STRIKE IN BETWEEN FR 21 AND FR 22 24" LEFT OF RADIO ALT. H.I.T. DIMENSION 66MM/11MM "363 SQMM". INSPECTED LIGHTNING STRIKE AND CRITERIA MEETS A350 ASR 53-00-61-01001-661A-A. REPAIR CARRIED OUT AS PER ASR A350-53-11-61-09002- -664A-A REV 78. (LP
STCs that may be installed · 27
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 27 STCs