# N101DU: 2018 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: 50020
- Year built: 2018
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 25, 2018
- Certificate issued: August 8, 2020
- Expires: August 31, 2027
- Mode S code: A008C9
- 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=101DU
- Page: https://openairdocs.org/aircraft/N101DU

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/N101DU/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 N101DU.

## FAA accident and incident reports

None matched to N101DU.

## Service difficulty reports (49)

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 DALA2026090104933](https://openairdocs.org/sdr/DALA2026090104933), Aug 30, 2026: CONTROL UNIT. FAULTY. DECLARED EMERGENCY DUE TO 24 ELECTRICAL FAULT - BPCU INOP WITH ASSOCIATED FLAP AND SLAT REDUNDANT LOSS AT CRUISE. REPLACED NR 1 BUS POWER CONTROL UNIT (BPCU). (
- [SDR DALA2025011400323](https://openairdocs.org/sdr/DALA2025011400323), Jan 13, 2025: VALVE. LEAKING. WASTE BALL VALVE LEAKING. REMOVED AND REPLACED WASTE BALL VALVE REF TO A220 AMP 38-31-03. COMPLIED WITH PRI 595069-14 REV 0, REV 01, REV 02, REV 03, AND FINAL E
- [SDR DALA2024102110276](https://openairdocs.org/sdr/DALA2024102110276), Oct 18, 2024: LIGHT. INOPERATIVE. FLIGHT CREW REPORTED EMERGENCY LIGHTS INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AS PER A220 AMP 33-51, OPS CHECK OK. (LP# 6419512)
- [SDR DALA2024100209612](https://openairdocs.org/sdr/DALA2024100209612), Sep 30, 2024: WARNING MESSAGE. FALSE ACTIVATION. SHIP 8101 - ATO - DUE TO "CONFIG RUDDER TRIM" WARNING MESSAGE. CORRECTIVE ACTION: PERFORMED OPERATIONAL AND FUNCTIONAL TEST OF TAKE-OFF CONFIGURATION. (LP# 5812
- [SDR DALA2024082908532](https://openairdocs.org/sdr/DALA2024082908532), Aug 28, 2024: LIGHT. INOPERATIVE. 2 OVER WING EMERGENCY EXT LIGHTS INOP. REMOVED AND REPLACED LT FWD AND AFT AND RT FWD OVERWING EMERGENCY LIGHTS PER A220 AMP 33-55. OPS NORMAL. (LP# 6201547)
- [SDR DALA2024040404064](https://openairdocs.org/sdr/DALA2024040404064), Apr 2, 2024: SKIN. CRACKED. RH WING LEADING EDGE CRACKED AT SLAT TRACK #7 CUT OUT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0684:2021-2065-
- [SDR DALA2024040204034](https://openairdocs.org/sdr/DALA2024040204034), Mar 30, 2024: BLOCK. BROKEN. RH OWEED FWD PIVOT BLOCK IS BROKEN AND UNABLE TO BE REPAIRED. REMOVED AND REPLACED RH OWEED SLIDE REF. A220 AMP 25-63-02. SLIDE, PACK, OW OFF 81-2563-9-0008 280
- [SDR DALA2024040204033](https://openairdocs.org/sdr/DALA2024040204033), Mar 28, 2024: FLOOR SUPPORT. CRACKED. AFT CARGO DOOR CUTOUT: FLOOR SUPPORT BEAM CRACKED AT OTBD END. 5 " AFT OF FR 64. (AFT OF DOOR HINGE). REPAIRED REF PRI 616272-14 REV 0, REV 1 AND ER/A 616272-14
- [SDR DALA2024032803892](https://openairdocs.org/sdr/DALA2024032803892), Mar 27, 2024: FLOORBEAM. CRACKED. AFT CARGO DOOR CUTOUT: FLOOR SUPPORT BEAM CRACKED AT OTBD END. 5 " FWD OF FR 63. (FWD OF DOOR HINGE). ATA 5311 RII: Y ENTR 00284754 W SUMMARY OF NR#416:ACCOMPLI
- [SDR DALA2024032803891](https://openairdocs.org/sdr/DALA2024032803891), Mar 27, 2024: DOOR FRAME. CORRODED. L1 DOOR FR20 FACING FWD FOUND 8 EACH FASTENERS HOLES CORROSION THROUGH NUT-PLATE. REPAIRED PER PRI 616196-14 REV 0, REV 1, REV 2, REV 3, AND ER/A 616196-14 REV 
- [SDR DALA2024032703851](https://openairdocs.org/sdr/DALA2024032703851), Mar 22, 2024: SKIN. CRACKED. LH LEADING EDGE CUT OUT FOR SLAT TRACK #7 HAS CRACK. REPAIRED CRACK PER PRI 615984-14 REV 0, REV 01, REV 02 AND FINAL ERA 615984-14 REV ORIGINAL.
- [SDR DALA2024032603830](https://openairdocs.org/sdr/DALA2024032603830), Mar 20, 2024: ROLLER. WORN. LH WING, #4 SLAT TRACK HAS HEAVY ROLLER WEAR. FWD, UPPER SURFACE . -M- LOG-PAGE UPDATED @ 20MAR24 1416 UTC 02 CORR BY SACHS 00583347 MSP 20MAR24 ATA 5742 RII: N
- [SDR DALA2024031203252](https://openairdocs.org/sdr/DALA2024031203252), Mar 11, 2024: SEAT TRACK. CORRODED. FWD GALLEY: CORROSION IN FLOOR FITTING FR 22 RBL 43. -M-PIC. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:2530
- [SDR DALA2024031203251](https://openairdocs.org/sdr/DALA2024031203251), Mar 11, 2024: SEAT TRACK. CORRODED. FORWARD GALLEY: CORROSION IN FLOOR FITTING FR 22 RBL 43. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0240295)
- [SDR DALA2024031203248](https://openairdocs.org/sdr/DALA2024031203248), Mar 9, 2024: SEAT TRACK. CORRODED. AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 RBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. (LP# 0236714)
- [SDR DALA2024031203247](https://openairdocs.org/sdr/DALA2024031203247), Mar 9, 2024: SEAT TRACK. CORRODED. AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-00, CIC ACCOMPLISHED ON AMDS 5341-2017.
- [SDR DALA2024031203246](https://openairdocs.org/sdr/DALA2024031203246), Mar 9, 2024: SEAT TRACK. CORRODED. AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. (LP# 0236475)
- [SDR DALA2024031203249](https://openairdocs.org/sdr/DALA2024031203249), Mar 8, 2024: SEAT TRACK. CORRODED. AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. -M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:2530-2001/004 00319 REMOVED AND 
- [SDR DALA2024031203245](https://openairdocs.org/sdr/DALA2024031203245), Mar 8, 2024: SEAT TRACK. CORRODED. AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11.(LP# 0236202)
- [SDR DALA2025102107691](https://openairdocs.org/sdr/DALA2025102107691), Mar 7, 2024: SEAT TRACK. CORRODED. CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 RBL 23. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0234433)
- [SDR DALA2025102107690](https://openairdocs.org/sdr/DALA2025102107690), Mar 7, 2024: SEAT TRACK. CORRODED. CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-06 AND DWG C01303000. (LP# 0234426)
- [SDR DALA2025102107689](https://openairdocs.org/sdr/DALA2025102107689), Mar 7, 2024: SEAT TRACK. CORRODED. FWD GALLEY: CORROSION IN FLOOR FITTING AT FR22 RBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-20. (LP# 0234366)
- [SDR DALA2024030603066](https://openairdocs.org/sdr/DALA2024030603066), Mar 3, 2024: THRESHOLD. CORRODED. FWD CABIN FLOOR: SERVICE ENTRY DOOR THRESHOLD CORRODED AT FWD INBD CORNER FR 17. THRESHOLD REMOVED AND REPLACED PER A220 ASRP 51-41-02. CORROSION LEVEL 2,
- [SDR DALA2024030503039](https://openairdocs.org/sdr/DALA2024030503039), Mar 1, 2024: PUMP. GOUGED. LH WING FUEL SYSTEM - EJECTOR PUMP ASSEMBLY HAS CHAFING AND GOUGING AT COUPLING FLANGE. REF. AMDS 2820-01281-07A, ITEM 12. SEE PIC. SCEPTRE LOG PAGE ENTERED FOR
- [SDR DALA2024020101476](https://openairdocs.org/sdr/DALA2024020101476), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024020101475](https://openairdocs.org/sdr/DALA2024020101475), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024020101474](https://openairdocs.org/sdr/DALA2024020101474), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2024020101473](https://openairdocs.org/sdr/DALA2024020101473), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101472](https://openairdocs.org/sdr/DALA2024020101472), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101471](https://openairdocs.org/sdr/DALA2024020101471), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101470](https://openairdocs.org/sdr/DALA2024020101470), Jan 30, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101469](https://openairdocs.org/sdr/DALA2024020101469), Jan 29, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101468](https://openairdocs.org/sdr/DALA2024020101468), Jan 29, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101467](https://openairdocs.org/sdr/DALA2024020101467), Jan 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF5742-010128-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024020101466](https://openairdocs.org/sdr/DALA2024020101466), Jan 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024020101465](https://openairdocs.org/sdr/DALA2024020101465), Jan 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024020101464](https://openairdocs.org/sdr/DALA2024020101464), Jan 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01018-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024020101463](https://openairdocs.org/sdr/DALA2024020101463), Jan 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2023090807368](https://openairdocs.org/sdr/DALA2023090807368), Sep 3, 2023: UNKNOWN. UNKNOWN. PER AMDS CARD 5742-01028-02A- LH WING SLAT TRACK #7 HAS CORROSION ON UPPER AFT AND LOWER AFT SURFACES WITH PREVIOUS REWORK. CEPTRE LOG PAGE ENTERED FOR SDR REPO
- [SDR DALA2023050503526](https://openairdocs.org/sdr/DALA2023050503526), May 1, 2023: UNKNOWN. UNKNOWN. ERA 608468-14AD SECTION I ISSUED FOR CORROSION TO LH SLAT TRACKS. ACCOMPLISHED ERA 608468-14AD REV ORIGINAL SECTION 1. (LP# 2747021)
- [SDR DALA2023050503525](https://openairdocs.org/sdr/DALA2023050503525), May 1, 2023: UNKNOWN. UNKNOWN. ERA 608469-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VIS IT. FOLLOW ON ACTION IS REQUIRED. THIS AFFECTS RH WING SLAT TRAC KS 4-9. ACCOMPLISHED ER/A 6084
- [SDR DALA2023032102110](https://openairdocs.org/sdr/DALA2023032102110), Mar 17, 2023: UNKNOWN. UNKNOWN. AFTER STARTING ENG #2, FA REPORTED BURNING SMELL AND THIN SMOKE IN MID AND FWD CABIN. SMELL AND SMOKE DISSIPATED AFTER SHUTTING DOWN. THE ENGINE. EXPERIENCED SI
- [SDR DALA2023013000751](https://openairdocs.org/sdr/DALA2023013000751), Jan 26, 2023: OIL SYSTEM. OVERSERVICED. DURING AND JUST AFTER TOUCHDOWN ALL CABIN FA'S REPORTED ELECTRICAL ODOR AND MINOR HAZE OVER COMFORT PLUS SEATS. ODOR AND HAZE DISSIPATED AFTER AIRCRAFT WAS PARK
- [SDR DALA2022060904028](https://openairdocs.org/sdr/DALA2022060904028), Nov 2, 2021: NONE. NONE. ERA 594987-14 SECTION I ACCOMPLISHED DURING CCK IN MSP NOV2021. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 594987-14 SECTION II REPEAT INSPECTION EVERY 850 FH
- [SDR DALA2025011400326](https://openairdocs.org/sdr/DALA2025011400326), Oct 27, 2021: NONE. NONE. **AD RELATED** - LOWER AFT FUSELAGE / WASTE WATER SURROUND STRUCTURE / FR75-76 / CORROSION. ERA 595069-14AD ISSUED AND IS CURRENT. FOLLOW ON ACTION REQUIRED SEC
- [SDR DALA2022091606166](https://openairdocs.org/sdr/DALA2022091606166), Sep 28, 2021: NONE. NONE. A220 LH WING NO. 3 SLAT (MPN C01612004-001 / MSN 50038) WAS IMPACTED BY A STAND CREATING A DENT ON THE TOP SKIN. THE SUBJECT NO. 3 SLAT HAS BEEN REPAIRED PER ER
- [SDR DALA2020080302688](https://openairdocs.org/sdr/DALA2020080302688), Aug 2, 2020: WARNING MESSAGE. FALSE ACTIVATION. L ENG FUEL LO PRESS CAUTION MESSAGE INFLIGHT. RAN THROUGH QRH, AFTER 1 MINUTE MESSAGE DISSAPEARED. T/S PER A220 SOLUTION 2-33317, R/R LT ENG FEED PRESSURE SWITC
- [SDR DALA2020011600352](https://openairdocs.org/sdr/DALA2020011600352), Jan 14, 2020: LONGERON. CRACKED. FOUND RT WTBF INTERNAL LONGERON ASSY P/N C02383111-002 CRACKED VERTICAL. REMOVED DAMAGED AREA PER ERA 583765-14 SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 58430
- [SDR DALA2020011600351](https://openairdocs.org/sdr/DALA2020011600351), Jan 14, 2020: LONGERON. CRACKED. FOUND LT WTBF INTERNAL LONGERON ASSY P/N 602383111-001 CRACKED VERTICALLY. REMOVED DAMAGED AREA PER ERA 583765-14 RI SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 

## 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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