# N137DU: 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: 50056
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 2020
- Certificate issued: October 29, 2020
- Expires: October 31, 2027
- Mode S code: A09590
- 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=137DU
- Page: https://openairdocs.org/aircraft/N137DU

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/N137DU/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 N137DU.

## FAA accident and incident reports

None matched to N137DU.

## Service difficulty reports (56, 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 DALA2026061503583](https://openairdocs.org/sdr/DALA2026061503583), Jun 10, 2026: LONGERON. CORRODED. ER/A 634632-14; A220-100, MID FUSELAGE WING TO BODY FAIRING LONGERONS BTWN FR36-38, FR42-FR45, & FR48-FR52 CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. A
- [SDR DALA2026061503582](https://openairdocs.org/sdr/DALA2026061503582), Jun 10, 2026: SKIN. CORRODED. CORROSION FOUND ON EXTERNAL FUSELAGE SKIN AT FR57-61 STR36-L . C/W ER/A 634830-14AD REV ORIGINAL. (LP# 1639893; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503581](https://openairdocs.org/sdr/DALA2026061503581), Jun 9, 2026: STRUCTURE. CORRODED. WHILE WORKING NRC 00177 FOR REMOVAL OF WASTE SERVICE INTERNL SKIN DOUBLER, FOUND ADDITIONAL CORROSION ON WASTE BOX INTERNAL AREA AT AFT RT SENSOR . C/W DELTA ER
- [SDR DALA2026061103541](https://openairdocs.org/sdr/DALA2026061103541), Jun 9, 2026: DOUBLER. CORRODED. ER/A 635012-14; A220-100 FUSELAGE REAR BARREL SKIN DOUBLER , WASTE ACCESS AND WASTE BOX ASSY / BTW FR75 - FR76, STR 32L - STR 36L / CORROSION. SUBJECT REPAIR RE
- [SDR DALA2026060903491](https://openairdocs.org/sdr/DALA2026060903491), Jun 5, 2026: FRAME. CORRODED. CORROSION ON FR81 INNER AND OUTER SURFACES APPROX. 4 IN FROM STRINGER 19L TOWARD RT (INTERCOASTAL LOWER FR80-81) AT AFT EQUIPMENT COMPARTMENT DOOR CUTOUT SURROU
- [SDR DALA2026060903490](https://openairdocs.org/sdr/DALA2026060903490), Jun 5, 2026: FRAME. CORRODED. WHILE WORKING ON FR81 INNER AND OUTER SURFACES DAMAGE ON CC# 00187, FOUND FR80 WITH CORROSION BETWEEN LBL 7 AND RBL7. REMOVED AND REPLACED FRAMES AT FR 80 L/H A
- [SDR DALA2026060303375](https://openairdocs.org/sdr/DALA2026060303375), Jun 1, 2026: FLOOR PANEL. CORRODED. AFT SERVICE ENTRY FLOOR PANEL WITH CORROSION. REMOVED AND REPLACED AFT SERVICE ENTRY FLOOR PANEL IAW A220 AM BD500-A-J53-00-47-14AAA-720A-A. (LP# 1624367; AIRCR
- [SDR DALA2026053003278](https://openairdocs.org/sdr/DALA2026053003278), May 29, 2026: FLOOR SUPPORT. CORRODED. CORROSION LEVEL 2 ON FLOOR EDGE SUPPORT AT FR-76, RBL-51, WL-151. REMOVED SILL WEB DAMAGED AND INSTALLED NEW SILL WEB AT FR 76 RBL 51 WL 151 IAW PL C01342700 RE
- [SDR DALA2026052803247](https://openairdocs.org/sdr/DALA2026052803247), May 27, 2026: SUPPORT ANGLE. CORRODED. CORROSION LEVEL 2, WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR33-L AND STR33-R. REMOVED DAMAGED WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR 33-L AND STR 33-R 
- [SDR DALA2026052403143](https://openairdocs.org/sdr/DALA2026052403143), May 23, 2026: FLOOR PANEL. CORRODED. AIRCRAFT 8137, FWD SERVICE ENTRY FLOOR PANEL WITH CORROSION LEVEL 2. REPLACED FWD SERVICE DOOR FLOOR PANEL IAW A220 AMP BD500-J53-00-47-12AAA-720A-A. (LP 160904
- [SDR DALA2026052303126](https://openairdocs.org/sdr/DALA2026052303126), May 22, 2026: SEAT TRACK. CORRODED. AIRCRAFT 8137, CORROSION LEVEL 2 FORWARD CABIN RIGHT O/B SEAT TRACK CORROSION ON FORWARD END RBL 43.5 FR20 WL 151.5. REPLACED SEAT TRACK RBL 43.5 FR20 TO FR30 I
- [SDR DALA2026052203124](https://openairdocs.org/sdr/DALA2026052203124), May 21, 2026: SEAT TRACK. CORRODED. CORROSION LEVEL 2 RIGHT OTBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 43.5 WL 151.5. REPLACED SEAT TRACK RT OTBD RBL 43.5, FR 74 - 61 IAW ASRP BD500-A-J51-40-11
- [SDR DALA2026051903060](https://openairdocs.org/sdr/DALA2026051903060), May 18, 2026: SEAT TRACK. CORRODED. LEFT INBD SEAT TRACK AFT END CORRODED AT FR74 LBL 23 WL 151.5. REMOVED AND REPLACED SEAT TRACK L/H / I/B FROM FR 61 TO FR 74 LBL 23 WL 151.5 I.A.W A220 ASRP BD5
- [SDR DALA2026051903059](https://openairdocs.org/sdr/DALA2026051903059), May 18, 2026: SEAT TRACK. CORRODED. RIGHT INBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 23 WL151.5. REMOVED DAMAGED SEAT TRACK FROM FR 61 TO FR 74 RBL 23 WL 151.5 AND INSTALLED NEW SEAT TRACK I.A.
- [SDR DALA2026051803051](https://openairdocs.org/sdr/DALA2026051803051), May 15, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, FORWARD CABIN RIGHT I/B SEAT TRACK CORROSION ON FORWARD END RBL 23 FR20 WL151.5. REPLACED FWD CABIN R/H I/B SEAT TRACK AT RBL 23, BTW FR=20 T
- [SDR DALA2026051803050](https://openairdocs.org/sdr/DALA2026051803050), May 14, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, L/H O/B SEAT TRACK AFT END CORRODED AT FR74 LBL 43.5 WL 151.5. REPLACED L/H O/B SEAT TRACK FROM FR60 TO FR74 LBL 43.5 WL 151.5 PER BOMBARDIER
- [SDR DALA2025101307463](https://openairdocs.org/sdr/DALA2025101307463), Oct 8, 2025: HINGE FITTING. CRACKED. FOUND RUDDER HINGE #1 CRACKED AND RUDDER LOWER CLOSURE RIB CRACKED. REPAIRED PER PRI 629727-14 REV 0 AND ER/A 629727-14 REV ORIGINAL. (LP# 1240208)
- [SDR DALA2025040102431](https://openairdocs.org/sdr/DALA2025040102431), Mar 29, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #9 PINION TEETH (1EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2025040102430](https://openairdocs.org/sdr/DALA2025040102430), Mar 29, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #9 RACK TEETH(1EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2025040102429](https://openairdocs.org/sdr/DALA2025040102429), Mar 29, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2025040102428](https://openairdocs.org/sdr/DALA2025040102428), Mar 29, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORD REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024102110274](https://openairdocs.org/sdr/DALA2024102110274), Oct 16, 2024: LIGHT. MISSING. DURING CRV FOUND 2FT REFLECTING ESCAPE PATH MARKING MISSING AT 01B. REPLACED ESCAPE PATH MARKING 01B A220 25-28 AMP. (LP# 6094396)
- [SDR DALA2024082908531](https://openairdocs.org/sdr/DALA2024082908531), Aug 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVE
- [SDR DALA2024082908530](https://openairdocs.org/sdr/DALA2024082908530), Aug 29, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS.REMOVED
- [SDR DALA2024081308069](https://openairdocs.org/sdr/DALA2024081308069), Aug 11, 2024: LONGERON. CRACKED. WHEN PREFORMING WING TO BODY FAIRING SUPPORT STRUCTURE INSPECTION CARD 5353-01038-01B CHECK . FOUND RIGHT LONGERON P/N C02383111-002 CRACKED. STARTED TO REMOVE 
- [SDR DALA2024051505241](https://openairdocs.org/sdr/DALA2024051505241), May 14, 2024: FUEL LINE. WORN. RH FUEL TANK, DURING ACCOMPLISHMENT OF AMDS 2820-01281-07B STEP 17, ITEM 6 NOTED FUEL TUBE FLANGE WORN BEYOND LIMITS (0.010). REPLACED RH FUEL TANK, ITEM 6 FUEL
- [SDR DALA2024030603078](https://openairdocs.org/sdr/DALA2024030603078), Mar 5, 2024: SMOKE DETECTOR. FAILED. SHIP 8137 - DIV - TO OMA DUE TO AN EQUIPMENT BAY SMOKE FAIL MESSAGE. CORRECTIVE ACTION: REPLACED AVIONICS AND ELECTRICAL BAY SMOKE DETECTOR SYSTEMS AND TUBING F
- [SDR DALA2024012200962](https://openairdocs.org/sdr/DALA2024012200962), Jan 16, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK #3 LOW AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHE
- [SDR DALA2024012200961](https://openairdocs.org/sdr/DALA2024012200961), Jan 16, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024012200960](https://openairdocs.org/sdr/DALA2024012200960), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200959](https://openairdocs.org/sdr/DALA2024012200959), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200958](https://openairdocs.org/sdr/DALA2024012200958), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200957](https://openairdocs.org/sdr/DALA2024012200957), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200956](https://openairdocs.org/sdr/DALA2024012200956), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200955](https://openairdocs.org/sdr/DALA2024012200955), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200954](https://openairdocs.org/sdr/DALA2024012200954), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200953](https://openairdocs.org/sdr/DALA2024012200953), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200952](https://openairdocs.org/sdr/DALA2024012200952), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200951](https://openairdocs.org/sdr/DALA2024012200951), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024012200950](https://openairdocs.org/sdr/DALA2024012200950), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200949](https://openairdocs.org/sdr/DALA2024012200949), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200948](https://openairdocs.org/sdr/DALA2024012200948), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHE
- [SDR DALA2024012200947](https://openairdocs.org/sdr/DALA2024012200947), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2024012200946](https://openairdocs.org/sdr/DALA2024012200946), Jan 16, 2024: SLAT TRACK. CORRODED. L/H SLAT TRACK #9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER
- [SDR DALA2024012200945](https://openairdocs.org/sdr/DALA2024012200945), Jan 16, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK #10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. AA 5742-10128-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER
- [SDR DALA2024011100503](https://openairdocs.org/sdr/DALA2024011100503), Jan 10, 2024: UNKNOWN. UNKNOWN. FOUND WTBF SUPPORT BEAM CLIP CRACKED. REMOVED SUPPORT BEAM + CLIP (R LARSON 437286) INSTALLED LONGERON ASSY REF A220 WORK CARD 5352-01038-05A C022383111-001, RE
- [SDR DALA2024011100502](https://openairdocs.org/sdr/DALA2024011100502), Jan 10, 2024: UNKNOWN. UNKNOWN. WORKING AD RELATED WORK CARD 5352-01038-01B FOUND LONGERON P/N C02383111-001 AT LBL 4010 CRACKED FROM FRAME C02383123-001 TO FRAME C02383037-001 25" ALONG THE N
- [SDR DALA2023110309046](https://openairdocs.org/sdr/DALA2023110309046), Nov 2, 2023: UNKNOWN. UNKNOWN. WHEN APU IS STARTED AND TAKES OVER A/C PACKS, WE GET A BAD DIRTY SOCKS SMELL. DURING INSPECTIONS FOUND APU STARTER ORING LEAKING. REPLACED PER A220 AMP 49-41 (A
- [SDR DALA2023083007066](https://openairdocs.org/sdr/DALA2023083007066), Aug 29, 2023: UNKNOWN. UNKNOWN. CORROSION ON WASTE BOX DOUBLER RIGHT SIDE AND AFT SIDE. -M-. 001-0244:2021-2025/001 00020 COMPLIED WITH ER/A 611382-14 PRI REV 0, ER/ A 611382-14 PRI REV 1, ER/
- [SDR DALA2026061103540](https://openairdocs.org/sdr/DALA2026061103540), Aug 23, 2023: NONE. NONE. ERA 611382-14 SECTION I ACCOMPLISHED IN MSP DURING CCK AUG 2023. FOLLOW ON ACTION IS REQUIRED. REPAIR WAS TO WASTE BOX AREA. ACCOMPLISH ERA 611382-14 SECTION II

All 56: https://openairdocs.org/aircraft/N137DU/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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