# N125DU: 2019 Airbus Canada Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [Airbus Canada Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10) (registry code 1400010, 133 seats)
- Engine: [Pratt & Whitney PW1519G](https://openairdocs.org/engine/pratt-whitney-pw1519g) (registry code 52315)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership), [TCDS E00090EN](https://openairdocs.org/tcds/E00090EN) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 50044
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 2019
- Certificate issued: June 22, 2020
- Expires: June 30, 2027
- Mode S code: A066A3
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=125DU
- Page: https://openairdocs.org/aircraft/N125DU

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 75 in force

### Matched by airframe (Airbus Canada Ltd Ptnrsp BD-500-1A10)

- [AD 2026-15-14](https://openairdocs.org/ad/2026-15-14): Engine fuel and control · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 3, 2026
- [AD 2026-13-52](https://openairdocs.org/ad/2026-13-52): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 7, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-10-12](https://openairdocs.org/ad/2026-10-12): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-10](https://openairdocs.org/ad/2026-10-10): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-07](https://openairdocs.org/ad/2026-10-07): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-07-04](https://openairdocs.org/ad/2026-07-04): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 11, 2026
- [AD 2026-06-06](https://openairdocs.org/ad/2026-06-06): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2026
- [AD 2026-07-07](https://openairdocs.org/ad/2026-07-07): Air conditioning system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 17, 2026
- [AD 2026-04-04](https://openairdocs.org/ad/2026-04-04): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 8, 2026
- [AD 2025-20-08](https://openairdocs.org/ad/2025-20-08): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 30, 2025
- [AD 2025-19-07](https://openairdocs.org/ad/2025-19-07): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 6, 2025
- [AD 2025-19-01](https://openairdocs.org/ad/2025-19-01): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 23, 2025
- [AD 2025-17-01](https://openairdocs.org/ad/2025-17-01): Flight controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 29, 2025
- [AD 2025-16-01](https://openairdocs.org/ad/2025-16-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 18, 2025
- [AD 2025-09-02](https://openairdocs.org/ad/2025-09-02): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 18, 2025
- [AD 2025-06-06](https://openairdocs.org/ad/2025-06-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 2, 2025
- [AD 2025-05-07](https://openairdocs.org/ad/2025-05-07): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 15, 2025
- [AD 2025-02-06](https://openairdocs.org/ad/2025-02-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 9, 2025
- [AD 2025-03-05](https://openairdocs.org/ad/2025-03-05): Stabilizers · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 21, 2025
- [AD 2024-24-08](https://openairdocs.org/ad/2024-24-08): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 13, 2025
- [AD 2024-23-05](https://openairdocs.org/ad/2024-23-05): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 6, 2025
- [AD 2024-22-01](https://openairdocs.org/ad/2024-22-01): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 31, 2024
- [AD 2024-22-04](https://openairdocs.org/ad/2024-22-04): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 17, 2024
- [AD 2024-22-03](https://openairdocs.org/ad/2024-22-03): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 14, 2024
- [AD 2024-15-06](https://openairdocs.org/ad/2024-15-06): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 15, 2024
- [AD 2024-17-04](https://openairdocs.org/ad/2024-17-04): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 20, 2024
- [AD 2024-12-02](https://openairdocs.org/ad/2024-12-02): Portable Oxygen System · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 13, 2024
- [AD 2024-10-11](https://openairdocs.org/ad/2024-10-11): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2024
- [AD 2024-10-03](https://openairdocs.org/ad/2024-10-03): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 28, 2024
- [AD 2024-07-11](https://openairdocs.org/ad/2024-07-11): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 6, 2024
- [AD 2024-05-10](https://openairdocs.org/ad/2024-05-10): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-05-08](https://openairdocs.org/ad/2024-05-08): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-04-08](https://openairdocs.org/ad/2024-04-08): Electrical power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 23, 2024
- [AD 2023-24-01](https://openairdocs.org/ad/2023-24-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 2, 2024
- [AD 2023-20-01](https://openairdocs.org/ad/2023-20-01): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 9, 2023
- [AD 2023-16-03](https://openairdocs.org/ad/2023-16-03): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 25, 2023
- [AD 2023-16-02](https://openairdocs.org/ad/2023-16-02): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 22, 2023
- [AD 2023-12-09](https://openairdocs.org/ad/2023-12-09): Flight control system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 7, 2023
- [AD 2023-14-02](https://openairdocs.org/ad/2023-14-02): Navigation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 27, 2023
- [AD 2023-07-05](https://openairdocs.org/ad/2023-07-05): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10. Effective May 30, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-07-01](https://openairdocs.org/ad/2023-07-01): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 19, 2023
- [AD 2022-26-06](https://openairdocs.org/ad/2022-26-06): Placards and markings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Feb 2, 2023
- [AD 2022-25-19](https://openairdocs.org/ad/2022-25-19): Hardware, Engine Exhaust · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023
- [AD 2022-25-05](https://openairdocs.org/ad/2022-25-05): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023
- [AD 2022-21-03](https://openairdocs.org/ad/2022-21-03): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 14, 2022
- [AD 2022-16-02](https://openairdocs.org/ad/2022-16-02): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 25, 2022
- [AD 2022-16-08](https://openairdocs.org/ad/2022-16-08): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 1, 2022
- [AD 2022-11-21](https://openairdocs.org/ad/2022-11-21): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 15, 2022

### Matched by engine (Pratt & Whitney PW1519G)

- [AD 2025-04-13](https://openairdocs.org/ad/2025-04-13): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 8, 2025
- [AD 2024-06-04](https://openairdocs.org/ad/2024-06-04): Turbine Engine Compressor Section; Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Apr 11, 2024
- [AD 2022-27-04](https://openairdocs.org/ad/2022-27-04): Engine Controls · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Jan 31, 2023
- [AD 2022-15-03](https://openairdocs.org/ad/2022-15-03): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 19, 2022
- [AD 2022-02-05](https://openairdocs.org/ad/2022-02-05): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Jan 27, 2022
- [AD 2021-20-01](https://openairdocs.org/ad/2021-20-01): Turbine Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 27, 2021
- [AD 2021-17-09](https://openairdocs.org/ad/2021-17-09): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 22, 2021
- [AD 2020-04-01](https://openairdocs.org/ad/2020-04-01): Turbine Engine Oil System · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Mar 27, 2020
- [AD 2019-16-15](https://openairdocs.org/ad/2019-16-15): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 1, 2019

### Historical (superseded or no longer in force)

- [AD 2025-06-01](https://openairdocs.org/ad/2025-06-01) (historical): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2025
- [AD 2024-04-11](https://openairdocs.org/ad/2024-04-11) (historical): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2024
- [AD 2024-04-06](https://openairdocs.org/ad/2024-04-06) (historical): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 22, 2024
- [AD 2023-05-08](https://openairdocs.org/ad/2023-05-08) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 12, 2023
- [AD 2022-25-51](https://openairdocs.org/ad/2022-25-51) (historical): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 27, 2022
- [AD 2022-19-09](https://openairdocs.org/ad/2022-19-09) (historical): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 27, 2022
- [AD 2021-09-03](https://openairdocs.org/ad/2021-09-03) (historical): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 4, 2021
- [AD 2021-04-05](https://openairdocs.org/ad/2021-04-05) (historical): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 30, 2021
- [AD 2019-23-15](https://openairdocs.org/ad/2019-23-15) (historical): Time Limits/ Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 16, 2020
- [AD 2018-25-04](https://openairdocs.org/ad/2018-25-04) (historical): Cargo and accessory compartment · C Series Aircraft Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 14, 2019
- [AD 2021-14-06](https://openairdocs.org/ad/2021-14-06) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Aug 12, 2021
- [AD 2020-07-02](https://openairdocs.org/ad/2020-07-02) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 5 more. Effective Apr 15, 2020
- [AD 2019-21-11](https://openairdocs.org/ad/2019-21-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Oct 29, 2019
- [AD 2019-19-11](https://openairdocs.org/ad/2019-19-11) (historical): Turbine Engine Compressor Section · Pratt & Whitney PW1519G, PW1521G, PW1521G-3 and 10 more. Effective Sep 26, 2019

All 89: https://openairdocs.org/aircraft/N125DU/ads.md

## Information bulletins (advisory) (2 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NE-20-09](https://openairdocs.org/saib/NE-20-09): TURBINE ENGINE COMPRESSOR SECTION. Issued Apr 30, 2020

## NTSB investigations

None matched to N125DU.

## FAA accident and incident reports

None matched to N125DU.

## Service difficulty reports (68, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2026091105093](https://openairdocs.org/sdr/DALA2026091105093), Sep 9, 2026: ENGINE. ODOR. DECLARED EMERGENCY DUE TO WAXY / ACIDIC SMELL IN FLIGHT DECK AND CABIN. SMELL DISSIPATED ONE PACKS WERE ISOLATED. #02 ENGINE REPLACED. (LP# 9170256, 1804448, 91
- [SDR DALA2026091005074](https://openairdocs.org/sdr/DALA2026091005074), Sep 8, 2026: UNKNOWN. ODOR. DECLARED EMERGENCY AND DIVERTED TO RDU DUE TO ODOR IN THE MID CABIN. CARRIED OUT W/C 0550- 2001. REF A220 RD500-A-J79-00-00-00AAA-310A-A AND A-J49-91-00- 01AAA-
- [SDR DALA2026061703627](https://openairdocs.org/sdr/DALA2026061703627), Jun 13, 2026: SLIDE. UNRAVELED. GIRT BAR STATUS INDICATOR DOES NOT SHOW FULL RED WHEN 1L DOOR IS ARMED. FOUND L1 DOOR EMERGENCY SLIDE PACKING BEGINNING TO UNRAVEL. R/R L1 ESCAPE SLIDE ASSEMBLY
- [SDR DALA2025102107688](https://openairdocs.org/sdr/DALA2025102107688), Oct 15, 2025: DOOR SILL. NO DISCREPANCY. ERA 622251-14 REV A HAS FOLLOW-ON INSPECTION FOR THE FORWARD CARGO DOOR SILL AREA. ACCOMPLISH SECTION II WITHIN 28,600 FC OR 50,050 FH. THEN EVERY 9,400 FC OR 1
- [SDR DALA2026031301753](https://openairdocs.org/sdr/DALA2026031301753), Aug 29, 2025: BLADE. CORRODED. ENGINE, INBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0659:7830-2007-RH/003 00648. 
- [SDR DALA2026031301752](https://openairdocs.org/sdr/DALA2026031301752), Aug 29, 2025: BLADE. CORRODED. NR 1 ENGINE, OTBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALLED #2 ENG O/B T/R REF. AMDS WORKCARD 7830-4003-01-L
- [SDR DALA2025090206500](https://openairdocs.org/sdr/DALA2025090206500), Aug 29, 2025: STRUCTURE. DAMAGED. FWD CARGO DOOR, FWD LOWER CORNER DAMAGE. COMPLIED WITH ER/A 627697-14 PRI REV 0, ER/A 627697-14 PRI REV 1, ER/A 627697-14 PRI REV 2, ER/A 627697-14 PRI REV 3, E
- [SDR DALA2025090206499](https://openairdocs.org/sdr/DALA2025090206499), Aug 29, 2025: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON FLOOR SUPPORT BEAM GALLEY MOUNT NUT PLATE HOLE AT LBL40 BETWEEN FR76 AND FR78. REPAIRED BEAM PER ERA 628436-14 REV 0, 1, 2 AND PER ERA 628436
- [SDR DALA2025090206498](https://openairdocs.org/sdr/DALA2025090206498), Aug 29, 2025: WASTE BOX. CORRODED. AFT LOWER FUSELAGE LAV WASTE BOX HAS CORROSION ON AFT RECESSED DOOR FLANGE. COMPLIED WITH PRI 602523-14 REV 0 AND ER/A 602523-02523-14 REV 0 AND ER/A 602523-14 
- [SDR DALA2025090206491](https://openairdocs.org/sdr/DALA2025090206491), Aug 26, 2025: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON FLOOR SUPPORT BEAM GALLEY MOUNT NUT PLATE HOLE AT LBL40 BETWEEN FR76 AND FR78. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR
- [SDR DALA2025090206490](https://openairdocs.org/sdr/DALA2025090206490), Aug 26, 2025: FITTING. CORRODED. FOUND CORROSION ON FLOOR FITTING AFTER REMOVAL OF FLOOR ANGLE AT FR74 O/B OF LBL 43.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL
- [SDR DALA2026031301754](https://openairdocs.org/sdr/DALA2026031301754), Aug 15, 2025: BLADE. CORRODED. ENGINE, INBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED NO.1 ENGINE I/B T/R LOWER V BLADE SEGMENT PER GRAPW150
- [SDR DALA2025081105979](https://openairdocs.org/sdr/DALA2025081105979), Aug 10, 2025: FLOOR SUPPORT. CORRODED. R/H FLOOR SILL STRINGER 22 JUST AFT OF R2 DOOR SILL CORRODED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0193:2060-1007/003 00667 REMOVED AND REPLACED FLOOR 
- [SDR DALA2025081105978](https://openairdocs.org/sdr/DALA2025081105978), Aug 9, 2025: FLOOR SUPPORT. CORRODED. L/H FLOOR SILL STRINGER 22 JUST AFT OF L2 DOOR SILL CORRODED ON FASTENER HOLE. BLENDED AND CHECKED LIMITS REF A220 ASRP 53-00-00-00AAA-661A-A. REMOVED .005" OF 
- [SDR DALA2026031101706](https://openairdocs.org/sdr/DALA2026031101706), Aug 5, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION RBL 43.5 AT FRAMES 62, 67, AND 74. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDIT
- [SDR DALA2025080705929](https://openairdocs.org/sdr/DALA2025080705929), Aug 5, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAMES 71-74. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. REPLACED SEAT TRACK REF A220 ER/A
- [SDR DALA2025080705925](https://openairdocs.org/sdr/DALA2025080705925), Aug 1, 2025: SEAT TRACK. CORRODED. AFT GALLEY CENTER F/A SEAT MOUNTING FLANGE CORRODED. REMOVED AND REPLACED FLOOR FITTINGS WITH REF CMM 25-30-18.
- [SDR DALA2025052704044](https://openairdocs.org/sdr/DALA2025052704044), May 24, 2025: SIGN. BURNED OUT. FOUND RT OVER WING EMERGENCY SIGN IN CABIN BURNT OUT. R/R EMERGENCY LIGHT LIGHT PER THE A220 AMP 33-54. OPS CHK GOOD. (LP#7054031)
- [SDR DALA2025021901227](https://openairdocs.org/sdr/DALA2025021901227), Feb 15, 2025: ENGINE. ODOR. FUMES DETECTED IN THE COCKPIT ON ARRIVAL PHASE AROUND 6,000 FEET. T/S PER A220 AMDS WORKCARD 0550-2001 FOUND LT ENGINE OVER SERVICED WITH OIL (27.4 QTS) ISOLATE
- [SDR DALA2025012300567](https://openairdocs.org/sdr/DALA2025012300567), Jan 19, 2025: UNKNOWN. ODOR. POTENTIAL ODOR EVENT. LITE "DIRTY SOCK" SMELL ON T/O TO ABOUT 10,000 FT. NOTHING VISIBLE ON THE FLIGHT DESK. MASK NOT DEPLOYED. ATTEMPTED TO ISOLATE SMELL PER W
- [SDR DALA2025010600113](https://openairdocs.org/sdr/DALA2025010600113), Jan 2, 2025: UNKNOWN. UNKNOWN. DTE, ER/A 612109-14AD REV B REQUIRES STAGE 3 DTA APPROVAL. A220-100 / FUSELAGE / REAR BARREL / FR70 TO FR72 AND STR23L TO STR25L / DENT. ER/A 612109-14AD REV B 
- [SDR DALA2024100809786](https://openairdocs.org/sdr/DALA2024100809786), Oct 4, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED W
- [SDR DALA2024100809785](https://openairdocs.org/sdr/DALA2024100809785), Oct 4, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WIT
- [SDR DALA2024100809784](https://openairdocs.org/sdr/DALA2024100809784), Oct 4, 2024: SLAT TRACK. NO DISCREPANCY. RH WING #5 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS
- [SDR DALA2024100809783](https://openairdocs.org/sdr/DALA2024100809783), Oct 4, 2024: SLAT TRACK. NO DISCREPANCY. RH WING #4 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS
- [SDR DALA2024100809782](https://openairdocs.org/sdr/DALA2024100809782), Oct 4, 2024: SLAT TRACK. NO DISCREPANCY. RH WING #3 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSP. IAW A220 ANDTP 51-01-353. NO CRACKS FOUN
- [SDR DALA2024100809781](https://openairdocs.org/sdr/DALA2024100809781), Oct 4, 2024: SLAT TRACK. NO DISCREPANCY. RH WING #2 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. NO CRACKS FOUND
- [SDR DALA2024100809780](https://openairdocs.org/sdr/DALA2024100809780), Oct 4, 2024: SLAT TRACK. NO DISCREPANCY. LH WING #1 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. (LP# 0592245)
- [SDR DALA2024081408143](https://openairdocs.org/sdr/DALA2024081408143), Aug 10, 2024: CONTROL LEVER. FAULTED. ON SELECTION OF GEAR DOWN, HEARD A LOUD "CLUNK" NOISE, FOLLOWED BY "GEAR FAIL" CTN MSG. RAN QRH, VERIFIED GEAR DOWN & LOCKED, PROCEEDED TO AN UNEVENTFUL LANDING
- [SDR DALA2024052105389](https://openairdocs.org/sdr/DALA2024052105389), May 16, 2024: UNKNOWN. FUMES. 'DIRTY SOCK' ODOR/FUMES ON BOTH FLIGHTS. PERFORMED HIGH POWER ENGINE RUN AFTER BOROSCOPES. NO FUMES NOTED . SNIFFER TEST RESULT 0.0 REF CARD 0550-2001 (703365).
- [SDR DALA2024032703852](https://openairdocs.org/sdr/DALA2024032703852), Mar 19, 2024: WARNING MESSAGE. ILLUMINATED. WING SLIDE CAUTION MESSAGE DURING PUSHBACK. PLACARDED AND DEFERRED OVERWING SLIDE CONDITION IND INOP. OPERATE AS PER MEL 25-63-02; R&R LT OVERWING SLIDE PER WOR
- [SDR DALA2024031803420](https://openairdocs.org/sdr/DALA2024031803420), Mar 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A
- [SDR DALA2024031803419](https://openairdocs.org/sdr/DALA2024031803419), Mar 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. L REPAIRED LH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER
- [SDR DALA2024031803418](https://openairdocs.org/sdr/DALA2024031803418), Mar 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024031803417](https://openairdocs.org/sdr/DALA2024031803417), Mar 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER AFT SURFACE IAW ER
- [SDR DALA2024031803416](https://openairdocs.org/sdr/DALA2024031803416), Mar 15, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024031803415](https://openairdocs.org/sdr/DALA2024031803415), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 LOWER FWD IB SIDE IAW ER/A
- [SDR DALA2024031803414](https://openairdocs.org/sdr/DALA2024031803414), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024031803413](https://openairdocs.org/sdr/DALA2024031803413), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024031803412](https://openairdocs.org/sdr/DALA2024031803412), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A
- [SDR DALA2024031803411](https://openairdocs.org/sdr/DALA2024031803411), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B.
- [SDR DALA2024031803410](https://openairdocs.org/sdr/DALA2024031803410), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024031803409](https://openairdocs.org/sdr/DALA2024031803409), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024031803408](https://openairdocs.org/sdr/DALA2024031803408), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024031803407](https://openairdocs.org/sdr/DALA2024031803407), Mar 15, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024011100501](https://openairdocs.org/sdr/DALA2024011100501), Jan 9, 2024: UNKNOWN. UNKNOWN. LOWER WTBF- CLIP CRACKED AT FORWARD LOWER RT. CORNER OF MID AVIONICS COMPARTMENT ACCESS CUTOUT. REMOVED AND REPLACED WTBF CLIP PER A220 ASRP 51-42-06. (LP# 0147
- [SDR DALA2024011100500](https://openairdocs.org/sdr/DALA2024011100500), Jan 9, 2024: UNKNOWN. UNKNOWN. WTBF LONGERON CRACKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 012-0001:5110-2001/002 00004 REMOVED AND REPLACED W
- [SDR DALA2023101808573](https://openairdocs.org/sdr/DALA2023101808573), Oct 12, 2023: UNKNOWN. UNKNOWN. PARKED AT GATE WE STARTED SMELLING A HOT OIL ODOR THROUGH THE VENTS WITH APU RUNNING ONLY. C/W WORK CARD ODI. REPLACED RECIRCULATION FILTERS PER WORK CARD 0550-
- [SDR DALA2024011600667](https://openairdocs.org/sdr/DALA2024011600667), Sep 13, 2023: SKIN. DAMAGED. ON ARRIVAL ACS FOUND DAMAGE FWD OF L2 DOOR. FOUND DENT/GOUGE FWD OF L2 DOOR BETWEEN FRAMES 70 AND 72, AND STRINGERS 23L AND 25L. DENT MEASURES 5 INCHES VERTICAL
- [SDR DALA2023091407570](https://openairdocs.org/sdr/DALA2023091407570), Sep 13, 2023: UNKNOWN. UNKNOWN. ATTEMPTED TO REOPEN 1L TO BOARD PAX. DOOR JAMMED. RE-SEQUENCED FWD PASSENGER DOOR REF A220 AMP 52-00. PERFORMED OPS TEST OF MODE SELECT HANDLE MECHANISM REF A22

All 68: https://openairdocs.org/aircraft/N125DU/reports.md

## STCs that may be installed (OpenAirDocs) (15)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Airbus Canada Ltd Ptnrsp BD-500-1A10)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST02570LA](https://openairdocs.org/stc/ST02570LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04792NY](https://openairdocs.org/stc/ST04792NY): Update of Intelsat 2Ku. Delta Engineering Corporation
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST04483AT](https://openairdocs.org/stc/ST04483AT): Installation of the Avionics Support Group Constant Friction Mount (cfMount) with Cradle. Avionics Support Group Inc
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST03972NY](https://openairdocs.org/stc/ST03972NY): Installation of Honeywell Satcom SBB Upgrade and WiFi Network Activation. UMLAUT ENGINEERING GMBH
- [STC ST04073NY](https://openairdocs.org/stc/ST04073NY): Installation of navAero Electronic Flight Bag provisions. Delta Engineering Corporation
- [STC ST00149IB](https://openairdocs.org/stc/ST00149IB) (historical): Installation of a Cabin air exhaust muffler, to reduce this noise to a more comfortable level by installing a valve cap and sound damping system. DOA21 LIMITED

## Related

- Other Airbus Canada Ltd Ptnrsp BD-500-1A10 aircraft: https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10/aircraft.md
- The Pratt & Whitney PW1519G engine: https://openairdocs.org/engine/pratt-whitney-pw1519g.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.