# N131DU: 2020 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: 50050
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 6, 2020
- Certificate issued: March 6, 2020
- Expires: March 31, 2030
- Mode S code: A07F46
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=131DU
- Page: https://openairdocs.org/aircraft/N131DU

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/N131DU/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 N131DU.

## FAA accident and incident reports

None matched to N131DU.

## Service difficulty reports (92, 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 DALA2026051302995](https://openairdocs.org/sdr/DALA2026051302995), May 12, 2026: WARNING MESSAGE. FALSE ACTIVATION. WING SLIDE CAUTION MESSAGE CAME ON DURING TAXI- MSG INFO- 52 WING SLIDE- LT OWEE SLIDE INOP. FOUND L/H OVERWING SLIDE PRESSURE LOW REF A220 AMP 25-63. R/R L/ H 
- [SDR DALA2026020300804](https://openairdocs.org/sdr/DALA2026020300804), Jan 28, 2026: VENT. CLOGGED. BURNING ELECTRICAL SMELL DURING CRUISE IN AFT PART OF FORWARD GALLEY BY DOOR 1R. TURNED OFF CIRCUIT BREAKERS. SMELL DISSIPATED. AFTER LANDING THERE IS STILL A T
- [SDR DALA2025102407822](https://openairdocs.org/sdr/DALA2025102407822), Oct 17, 2025: DOOR SILL. CORRODED. 1 REPORTED BY LINARES 00705131 MSP 17OCT25 ENTR 00532877 W FWD PAX DOOR - CORROSION NOTED AROUND MULTIPLE HOLES ALONG LOWER SILL AND SILL FLOOR (M)(P) LOG-PAGE 
- [SDR DALA2025102407814](https://openairdocs.org/sdr/DALA2025102407814), Oct 17, 2025: SKIN. CORRODED. FWD PAX DOOR - CORROSION NOTED ADJACENT TO LOWER SKIN HOLES 14OL , 13OL,10OL, AND 2OL. SSI:53-21-23-02 (M) SEE NR FOR ADDITIONAL INFORMATION 031-0001:5331-01297
- [SDR DALA2025102407813](https://openairdocs.org/sdr/DALA2025102407813), Oct 17, 2025: SKIN. CORRODED. DURING H-CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-01B (SB BD500-530010 ISSUE 004). DURING MODIFICATION , MAINTENANCE REPORTED CORROSIO
- [SDR DALA2025102407812](https://openairdocs.org/sdr/DALA2025102407812), Oct 17, 2025: FRAME. CORRODED. INSPECT FORWARD SERVICING AREA PASSENGER COMPARTMENT, WITH GALLEY AND LAVATORY REMOVED. FRAME 17 AFT HOLE 5, 7, 8 HAVE CORROSION. LOG-PAGE UPDATED @ 17OCT25 193
- [SDR DALA2025102407811](https://openairdocs.org/sdr/DALA2025102407811), Oct 17, 2025: DOOR SILL. CORRODED. DURING H-CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-01C (SB BD500-530010 ISSUE 004). DURING MODIFICATION , THE FWD CARGO DOOR SURROUND S
- [SDR DALA2025102407805](https://openairdocs.org/sdr/DALA2025102407805), Oct 17, 2025: FRAME. CORRODED. INSPECT FORWARD SERVICING AREA PASSENGER COMPARTMENT, WITH GALLEY AND LAVATORY REMOVED. FRAME 20 FWD SIDE OF FRAME HOLE 1, 4, 5, 6, 7, 8. HAVE CORROSION. LOG-PA
- [SDR DALA2026031101710](https://openairdocs.org/sdr/DALA2026031101710), Oct 15, 2025: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION LBL 23.0 AT FRAME 22. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2026031101709](https://openairdocs.org/sdr/DALA2026031101709), Oct 6, 2025: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION RBL 23.0 AT FRAME 20. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2026031101708](https://openairdocs.org/sdr/DALA2026031101708), Sep 30, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION RBL 43.5 AT FRAME 72 AND EXTENDING UNDER NICKEL MAT. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. COMPLI
- [SDR DALA2026031101707](https://openairdocs.org/sdr/DALA2026031101707), Sep 30, 2025: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAME 22. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2025100607256](https://openairdocs.org/sdr/DALA2025100607256), Sep 30, 2025: PANEL. CRACKED. RIGHT OVERWING EMERGENCY EXIT DOOR SLIDE (OWEED) PANEL TE (DAMAGED) CRACKS AND DELAMINATED. REMOVED AND REPLACED RT OWEED SLIDE PER AMDS 2563-4005. (LP# 1226999
- [SDR DALA2025093007110](https://openairdocs.org/sdr/DALA2025093007110), Sep 26, 2025: DOOR SILL. CORRODED. AFT PASSENGER DOOR SILL HAS 6 LOCATIONS WITH SURFACE CORROSION AT OR NEAR THE SILL/ CORNER STRIKER FASTENER HOLES. HOLES 2, 3, 4, 11, 12, 14 COUNTING FWD TO AFT
- [SDR DALA2025093007111](https://openairdocs.org/sdr/DALA2025093007111), Sep 25, 2025: PANEL. DELAMINATED. LEFT OVERWING EMERGENCY EXIT DOOR SLIDE PANEL TE NUT PLATE MOUNTING SURFACE (DELAMINATED). REMOVED AND REPLACED OWEED SLIDE PER AMDS 2563-4002. (1217547)
- [SDR DALA2025092507001](https://openairdocs.org/sdr/DALA2025092507001), Sep 20, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION RBL 23.0 AT FRAME 72 AND EXTENDING UNDER NICKEL MAT. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. REMOVED AND REPLACED TRA
- [SDR DALA2025092507000](https://openairdocs.org/sdr/DALA2025092507000), Sep 20, 2025: SEAT TRACK. CORRODED. AFT FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAMES 71-72 AND EXTENDING UNDER NICKEL MAT. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. (M
- [SDR DALA2025070805081](https://openairdocs.org/sdr/DALA2025070805081), Jul 8, 2025: ENGINE. LEAKING. SHIP 8131 RETURNED TO SEA DUE TO DIRTY SOCK SMELL IN COCKPIT AND CABIN. CORRECTIVE ACTION: C/W W/C 0550-2001 & DETERMINED SOURCE TO BE #1 ENGINE. C/W W/C 0550-6
- [SDR DALA2025040802747](https://openairdocs.org/sdr/DALA2025040802747), Apr 4, 2025: SLAT TRACK. CORRODED. RH SLAT TRACK #7 RACK TEETH #2 HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 625
- [SDR DALA2025040802741](https://openairdocs.org/sdr/DALA2025040802741), Apr 2, 2025: SLAT TRACK. NO DISCREPANCY. RH SLAT TRACK #10 REQUIRES EDDY CURRENT INSPECTION TO BLENDED AREAS, CHECK FOR SIGNED OF CRACKS. UPPER FWD SURFACE. PERFORMED HFEEC ON RH SLAT TRACK #10 UPPER F
- [SDR DALA2025030501719](https://openairdocs.org/sdr/DALA2025030501719), Mar 3, 2025: ENGINE. ODOR. SHIP 8131 -ATB- RETURNED BOS DUE TO DIRTY SOCK SMELL ON CLIMB OUT. CORRECTIVE ACTION: T/S PER ODI WORKCARDS. C/C/O BORESCOPE INSP OF ENGINES. FOUND SLIGHT STAIN
- [SDR DALA2025030501717](https://openairdocs.org/sdr/DALA2025030501717), Feb 28, 2025: FILTER. ODOR. MOMENTARY MOIST TYPE SMELL ON CLIMB OUT. DISSIPATED QUICKLY. MOMENTARY SULPHUR TYPE SMELL ON INITIAL THRUST REDUCTION FOR DESCENT. DISSIPATED QUICKLY. NO SMELLS
- [SDR DALA2025021001041](https://openairdocs.org/sdr/DALA2025021001041), Feb 5, 2025: LIGHT. INOPERATIVE. FOUND LT FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT FWD OVERWING EMERGENCY LIGHT PER A220 AMP 33-55, OPS CHECK GOOD. (LP# 6772569)
- [SDR DALA2025012900711](https://openairdocs.org/sdr/DALA2025012900711), Jan 23, 2025: POWER UNIT. CONTAMINATED. AFT FLIGHT ATTENDANT REPORTED PLASTIC RUBBER BURNING SMELL ON DESCENT. IT WENT AWAY THEN FORWARD FLIGHT ATTENDANT HAD SIMILAR SMELL, AND IT WENT AWAY. I SMELLED
- [SDR DALA2024121011578](https://openairdocs.org/sdr/DALA2024121011578), Dec 9, 2024: OIL SYSTEM. LEAKING. SHIP 8131 -ATB- PERFORMED AN AIR TURN BACK TO JAX DUE TO LEFT ENGINE OIL QUANTITY LOW INDICATION. CORRECTIVE ACTION: ENGINE REPLACED. (LP# 0701574)
- [SDR DALA2024102810434](https://openairdocs.org/sdr/DALA2024102810434), Oct 26, 2024: UNKNOWN. ODOR. FUMES NOTED IN FLIGHT DECK AND FWD CABIN DURING DESCENT. ALT 15000' CHEMICAL SMELL. PERFORMED SMOKE AND FUMES IN COCKPIT CHK PER W/C 0550-2001. NO DEFECTS NOTED
- [SDR DALA2024101510106](https://openairdocs.org/sdr/DALA2024101510106), Oct 9, 2024: SHUTOFF VALVE. FAULTED. F/A REPORTED ODOR IN CABIN. T/S TO NBR 1 ENGINE. R/R PRSOV IAW A220 AMP 36-11. "M" PROCEDURE REVERSED OPS TEST NORMAL. (LP# 6417756)
- [SDR DALA2024101109976](https://openairdocs.org/sdr/DALA2024101109976), Oct 9, 2024: ENGINE. ODOR. FA ADVISED FUMES IN REAR OF AIRCRAFT WHEN CONFIGURING FOR APPROACH. FUMES HAD A CHEMICAL SMELL AND MADE THEM FEEL LIGHT HEADED. T/S PER A220 SMOKE AND FUMES W/C
- [SDR DALA2024091609038](https://openairdocs.org/sdr/DALA2024091609038), Sep 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 11 LWR AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY C
- [SDR DALA2024091609037](https://openairdocs.org/sdr/DALA2024091609037), Sep 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 7 LWR INB SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CU
- [SDR DALA2024091609036](https://openairdocs.org/sdr/DALA2024091609036), Sep 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY 
- [SDR DALA2024091609035](https://openairdocs.org/sdr/DALA2024091609035), Sep 12, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY 
- [SDR DALA2024091609034](https://openairdocs.org/sdr/DALA2024091609034), Sep 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY 
- [SDR DALA2024091609033](https://openairdocs.org/sdr/DALA2024091609033), Sep 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY 
- [SDR DALA2024091609032](https://openairdocs.org/sdr/DALA2024091609032), Sep 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 LOWER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY 
- [SDR DALA2024090608788](https://openairdocs.org/sdr/DALA2024090608788), Sep 3, 2024: LIGHT. INOPERATIVE. ON SVC CHECK FOUND 1R DOOR EXTERNAL EMERGENCY LIGHT INOP. R/R 1R EXTERNAL EMERGENCY LIGHT PER A220 AMP 33-55. OPS CHECK GOOD. (LP# 5721704)
- [SDR DALA2024021502207](https://openairdocs.org/sdr/DALA2024021502207), Feb 12, 2024: SKIN. CORRODED. L/H SLAT NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024021402186](https://openairdocs.org/sdr/DALA2024021402186), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 
- [SDR DALA2024021402185](https://openairdocs.org/sdr/DALA2024021402185), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 5 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 LOWER FWD I/B SIDE IAW E
- [SDR DALA2024021402184](https://openairdocs.org/sdr/DALA2024021402184), Feb 12, 2024: SLAT TRACK. CORRODED. RH 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 FUR
- [SDR DALA2024021402183](https://openairdocs.org/sdr/DALA2024021402183), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/
- [SDR DALA2024021402182](https://openairdocs.org/sdr/DALA2024021402182), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 10 UPPER FWD SURFACE IAW ER/
- [SDR DALA2024021402181](https://openairdocs.org/sdr/DALA2024021402181), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 LOWER FWD SURFACE IAW ER/
- [SDR DALA2024021402180](https://openairdocs.org/sdr/DALA2024021402180), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 9 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024021402179](https://openairdocs.org/sdr/DALA2024021402179), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 4 LOWER FWD O/B SIDE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 4 LOWER FWD O/B SIDE IA
- [SDR DALA2024021402178](https://openairdocs.org/sdr/DALA2024021402178), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 9 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER FWD I/B SIDE IAW ER/
- [SDR DALA2024021402177](https://openairdocs.org/sdr/DALA2024021402177), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 4 UPPER AFT I/B SIDE IA
- [SDR DALA2024021402176](https://openairdocs.org/sdr/DALA2024021402176), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 8 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 LOWER FWD I/B SIDE IAW ER/
- [SDR DALA2024021402175](https://openairdocs.org/sdr/DALA2024021402175), Feb 12, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION IN TWO SEPERATE LOCATIONS AND NO PREVIOUS REWORK REF 5742-01028 -02B. REPAIRED R/H SLAT TRACK N
- [SDR DALA2024021402174](https://openairdocs.org/sdr/DALA2024021402174), Feb 12, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 LOWER FWD I/B SIDE IAW ER/

All 92: https://openairdocs.org/aircraft/N131DU/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

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