# N105DU: 2019 C Series Aircraft Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [C Series Aircraft Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/c-series-aircraft-ltd-ptnrsp-bd-500-1a10) (registry code 1400012, 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: 50024
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 15, 2019
- Certificate issued: June 26, 2020
- Expires: June 30, 2027
- Mode S code: A017A5
- 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=105DU
- Page: https://openairdocs.org/aircraft/N105DU

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 (C Series Aircraft 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/N105DU/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 N105DU.

## FAA accident and incident reports

None matched to N105DU.

## Service difficulty reports (39)

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 DALA2026021701091](https://openairdocs.org/sdr/DALA2026021701091), Feb 14, 2026: PLUG. LEAKING. AIRCRAFT DIVERTED TO ORD DUE TO LT ENGINE LOSS OF OIL QTY WITH PRESSURE DEGRADING. INSTALLED NEW GEARBOX DRAIN PLUG AND NEW HELICOIL INSERT. (LP 7651170).
- [SDR DALA2025062504756](https://openairdocs.org/sdr/DALA2025062504756), Jun 21, 2025: SCUFF PLATE. CORRODED. FORWARD CARGO COMPARTMENT SILL BEAM HAS CORROSION AROUND 3(EA) THRESHOLD SCUFF PLATE ATTACH FASTENER HOLES. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY 
- [SDR DALA2025062504766](https://openairdocs.org/sdr/DALA2025062504766), Jun 21, 2025: THRESHOLD. CORRODED. THE AFT PASSENGER DOOR THRESHOLD HAS CORROSION AROUND THE FORWARD SCUFF PLATE ATTACH FASTENER HOLE. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0527:5360-2023
- [SDR DALA2025062404722](https://openairdocs.org/sdr/DALA2025062404722), Jun 20, 2025: DOOR. CORRODED. FORWARD LEDGE OF LAV SERVICE DOOR OPENING HAS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0519
- [SDR DALA2025100207161](https://openairdocs.org/sdr/DALA2025100207161), Jun 19, 2025: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION IN TWO AREAS ADJACENT TO THE FORWARD CARGO COMPARTMENT LOWER SCUFF PLATE ATTACH FASTENER HOLE 12OL. SUMMARY SEE NR FOR ADDITIONAL IN
- [SDR DALA2025062404717](https://openairdocs.org/sdr/DALA2025062404717), Jun 19, 2025: THRESHOLD. CORRODED. AFT SERVICE DOOR THRESHOLD/ENTRY SILL HAS CORROSION AROUND FASTENER HOLE AT AFT I/B CORNER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0576:5300-2016/001 003
- [SDR DALA2025062404727](https://openairdocs.org/sdr/DALA2025062404727), Jun 19, 2025: THRESHOLD. CORRODED. AFT PASSENGER DOOR THRESHOLD/ENTRY SILL HAS CORROSION AT AFT I/B CORNER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0576:5300-2016/003 00360 REPLACED THRESHO
- [SDR DALA2025100207160](https://openairdocs.org/sdr/DALA2025100207160), Jun 14, 2025: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION ADJACENT TO THE FORWARD PASSENGER DOOR SCUFF PLATE ATTACH FASTENER HOLE 8OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 050-0001:5331
- [SDR DALA2025061804587](https://openairdocs.org/sdr/DALA2025061804587), Jun 14, 2025: SKIN. DENTED. DENT FOUND ON UPPER FUSELAGE SKIN JUST AFT OF FR 53, AND JUST OUTBOARD OF STRINGER L3. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL
- [SDR DALA2025061704570](https://openairdocs.org/sdr/DALA2025061704570), Jun 13, 2025: SEAT TRACK. CORRODED. FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 RBL 43.5. SSI: 53-21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATI
- [SDR DALA2025100207159](https://openairdocs.org/sdr/DALA2025100207159), Jun 11, 2025: SKIN. CORRODED. FUSELAGE SKIN HAS CORROSION AT THE FORWARD SERVICE SCUFF PLATE ATTACH FASTENER HOLE 15OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 020-0001:5331-01297- 01B/001
- [SDR DALA2025061004419](https://openairdocs.org/sdr/DALA2025061004419), Jun 7, 2025: BEARING. GOUGED. R/H MLG ASSEMBLY, AFT SPHERICAL BEARING GOUGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 211-0002:3210-4001-RH/001 
- [SDR DALA2025061004418](https://openairdocs.org/sdr/DALA2025061004418), Jun 6, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 22. SSI: 53- 61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REP
- [SDR DALA2025060204205](https://openairdocs.org/sdr/DALA2025060204205), Jun 1, 2025: SEAT TRACK. CORRODED. AIRCRAFT 8105, AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 43.5. SSI: 53-61-43-01. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A220 ASRP 51-77-00. (LP 09
- [SDR DALA2025053004149](https://openairdocs.org/sdr/DALA2025053004149), May 29, 2025: THRESHOLD. CORRODED. AIRCRAFT 8105, FWD SERVICE DOOR THRESHOLD, AFT I/B CORNER AND EDGE HAVE CORROSION. CORRECTIVE ACTION: REPLACED THRESHOLD PANEL REF. A220 AMP 53-00-47. (LP 09938
- [SDR DALA2025052704043](https://openairdocs.org/sdr/DALA2025052704043), May 25, 2025: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 RBL 22. SSI:53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. BLENDED AND CHECKED LIMITS PER A220 A
- [SDR DALA2025052704050](https://openairdocs.org/sdr/DALA2025052704050), May 23, 2025: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 LBL 43.5. SSI: 53-21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED.SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2025052704049](https://openairdocs.org/sdr/DALA2025052704049), May 23, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 43.5. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. ( M) (P). SUMMARY SEE NR FOR ADDITI
- [SDR DALA2025052704048](https://openairdocs.org/sdr/DALA2025052704048), May 23, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 22. SSI: 53- 61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2025051403745](https://openairdocs.org/sdr/DALA2025051403745), May 10, 2025: LIGHT. NOT REPORTED. L/H REAR BARREL EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND INSTALLED SERVICEABLE L/H REAR EXTERNAL EMERGENCY LIGHT PER A220 AMP 33-55-02, OPS TEST GOOD. (LP# 43
- [SDR DALA2023091807656](https://openairdocs.org/sdr/DALA2023091807656), Sep 16, 2023: UNKNOWN. UNKNOWN. SHIP 8105 - MISC/DE - DUE TO "BRAKE ON" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED ELECTRICAL MOTOR CONTROL UNIT (EMCU) #4. (LP# 4492648)
- [SDR DALA2023091807653](https://openairdocs.org/sdr/DALA2023091807653), Sep 12, 2023: UNKNOWN. UNKNOWN. SHIP 8105 - DIV - TO MKE DUE TO "CARGO BTL FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: CARGO BOTTLE PLACED ON MEL; R/R HRD FIRE BOTTLE. (LP# 4492632)
- [SDR DALA2023080806471](https://openairdocs.org/sdr/DALA2023080806471), Aug 3, 2023: UNKNOWN. UNKNOWN. LEFT WING #2 SLAT TRACK HAS CORROSION ON LOWER SURFACE AFT ROLLER AREA. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE 
- [SDR DALA2023080806470](https://openairdocs.org/sdr/DALA2023080806470), Aug 3, 2023: UNKNOWN. UNKNOWN. LEFT WING #1 SLAT TRACK HAS CORROSION ON LOWER SURFACE AFT ROLLER AREA. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE 
- [SDR DALA2023060704631](https://openairdocs.org/sdr/DALA2023060704631), Jun 6, 2023: UNKNOWN. UNKNOWN. CORROSION FOUND ON WASTE BOX DOOR MOUNTING SURFACE RH SIDE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 069-0001:3832-
- [SDR DALA2023020300861](https://openairdocs.org/sdr/DALA2023020300861), Jan 31, 2023: NOT ENTERED. NOT ENTERED. SHIP 8105 - DIV - DUE TO SUSPECTED CRACK IN WINDOW AT SEAT 20A. CORRECTIVE ACTION: MAINTENANCE INSPECTED WINDOW AND REPORTED NO TROUBLE FOUND. FLIGHT CONTINUED 
- [SDR DALA2022042803007](https://openairdocs.org/sdr/DALA2022042803007), Apr 25, 2022: A/C PACK. OVERHEATED. ON DESCENT, THROUGH 180, AFTER TURN COWL-ANTI ICE OFF WITH ENGINES AT IDLE-BURNING OIL SCENT IN THE COCKPIT. ENGINE OFF IDLE SCENT WENT AWAY. ON TAXI IN AFTER S
- [SDR DALA2022020400722](https://openairdocs.org/sdr/DALA2022020400722), Jan 28, 2022: NONE. NONE. R/H HORIZONTAL STAB #3 RIB ELEVATOR HINGE CRACKED. ADDITIONAL INFORMATION 001-0293:2090-2039-RH/001 00148 ACCOMPLISHED PRI 596551-14, REV. 0; 596551-14, REV. 1;
- [SDR DALA2022020400721](https://openairdocs.org/sdr/DALA2022020400721), Jan 28, 2022: NONE. NONE. #2 HORIZONTAL STAB ELEVATOR RIB HINGE IS CRACKED. ADDITIONAL INFORMATION 001-0293:2090-2039-RH/002 00152 ACCOMPLISHED PRI 596562-14, REV. 0; 596562-14, REV. 1; 
- [SDR DALA2022020400720](https://openairdocs.org/sdr/DALA2022020400720), Jan 28, 2022: NONE. NONE. L/H HORIZONTAL STABILIZER #2 RIB ELEVATOR HINGE CRACKED. ADDITIONAL INFORMATION 001-0291:2090-2039-LH/001 00147 ACCOMPLISHED PRI 596563-14, REV. 0; 596563-14, R
- [SDR DALA2022012800579](https://openairdocs.org/sdr/DALA2022012800579), Jan 26, 2022: NONE. NONE. ON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 4 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 007 00239 COMPLETED INSTALL
- [SDR DALA2022012800578](https://openairdocs.org/sdr/DALA2022012800578), Jan 26, 2022: NONE. NONE. ON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 2 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 006 00238 COMPLETED INSTALL
- [SDR DALA2022012800580](https://openairdocs.org/sdr/DALA2022012800580), Jan 24, 2022: NONE. NONE. ER/A 596551-14 SECTION I ACCOMPLISHED FOR REPAIR OF THE RH HORIZONTAL STABILIZER, TRAILING EDGE, HINGE RIB #3. THE REPAIR WAS ACCOMPLISHED DURING 'C' CHECK IN M
- [SDR DALA2021112307195](https://openairdocs.org/sdr/DALA2021112307195), Nov 21, 2021: BLADES. CONTAMINATED. DIRTY/MUSTY SMELL ON T.O. AND CLIMB IN COCKPIT AND AFT CABIN, SMELL CAME BACK ON DSCT FROM 15,000 TILL GATE ARRIVAL. OPENED #1 ENGINE FOR BORO, REMOVED BORO PLU
- [SDR DALA2021112307197](https://openairdocs.org/sdr/DALA2021112307197), Nov 17, 2021: ENGINE. ODOR. ONCE AIRBORNE AFTER T/O A/C HAD A MUST SOCK SMELL. IT WAS NOTICEABLE NOT STRONG. ODOR STARTED TO FADE ONCE POWER WAS REDUCED TO CLIMB POWER. SLIGHT SMELL AFTER 
- [SDR DALA2021082404997](https://openairdocs.org/sdr/DALA2021082404997), Aug 23, 2021: REU. FAILED. SHIP 8105 - DIV - TO PDX DUE TO FLIGHT CONTROL FAULT/ REU INTERNAL MESSAGE AND FOLLOWED BY RUDDER FAIL MESSAGE. CORRECTIVE ACTION: REPLACED AFT REU-1. (LP# 7998
- [SDR DALA2020061802472](https://openairdocs.org/sdr/DALA2020061802472), Jun 17, 2020: COMPUTER. MALFUNCTIONED. SHIP 8105 - ATB/DE - DUE TO NUMEROUS FAULT WARNINGS ASSOCIATED WITH FAILURE OF THE DCM IN CONTROL TO INCLUDE EMERG DESCENT ANNUNCIATED. CORRECTIVE ACTION: TROUB
- [SDR DALA2019061103510](https://openairdocs.org/sdr/DALA2019061103510), Jun 8, 2019: SIGN. MISSING. LT OVERWING EMERGENCY EXIT SIGN MISSING. REPLACED LT OVERWING EXIT SIGN LENS REF A220 AMP 33-54-01. OK FOR SERVICE. (LP# 5707337)
- [SDR DALA2019042202545](https://openairdocs.org/sdr/DALA2019042202545), Apr 15, 2019: NONE. NONE. ACCOMPLISH ER/A 577289-14 TO INSTALL NEW CMS SOFTWARE. (REF. SERVICE BULLETIN BD500-441007 ISSUE NO. 1 AND SERVICE BULLETIN RDAK5151014-44-1S). (LP# 1031395)

## 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 (C Series Aircraft 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 C Series Aircraft Ltd Ptnrsp BD-500-1A10 aircraft: https://openairdocs.org/model/c-series-aircraft-ltd-ptnrsp-bd-500-1a10/aircraft.md
- The Pratt & Whitney PW1519G engine: https://openairdocs.org/engine/pratt-whitney-pw1519g.md

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