# N127DU: 2019 Airbus Canada Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [Airbus Canada Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10) (registry code 1400010, 133 seats)
- Engine: [Pratt & Whitney PW1519G](https://openairdocs.org/engine/pratt-whitney-pw1519g) (registry code 52315)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership), [TCDS E00090EN](https://openairdocs.org/tcds/E00090EN) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 50046
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 2019
- Certificate issued: June 22, 2020
- Expires: June 30, 2027
- Mode S code: A06E11
- 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=127DU
- Page: https://openairdocs.org/aircraft/N127DU

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/N127DU/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 N127DU.

## FAA accident and incident reports

None matched to N127DU.

## Service difficulty reports (46)

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 DALA2025080705927](https://openairdocs.org/sdr/DALA2025080705927), Aug 4, 2025: SKIN. GOUGED. AFT SERVICE DOOR- EXTERIOR SKIN HAS 2 SMALL GOUGES AT THE DOOR HANDLE CUTOUT FROM THE HANDLE CONTACTING THE SKIN. "M" SEE PIC. SCEPTRE LOG PAGE ENTERED FOR SDR 
- [SDR DALA2025072905701](https://openairdocs.org/sdr/DALA2025072905701), Jul 29, 2025: DOOR SILL. CORRODED. AIRCRAFT AFT SERVICE DOOR SILL, BOLT HOLE #4 HAS CORROSION EMITTING FROM IT. (P)(M). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0546:5360-2024/002 00539 REMO
- [SDR DALA2025072905697](https://openairdocs.org/sdr/DALA2025072905697), Jul 24, 2025: DUCT. DAMAGED. APU HIGH PRESSURE BLEED DUCT HAS PLY SEPARATION AT FIRE LOOP STANDOFF, 10 INCHES FWD OF FRAME 85. PER AMDS, REQUIRES CUSTOMER RESPONSE CENTER NOTIFICATION. SCEP
- [SDR DALA2025072205496](https://openairdocs.org/sdr/DALA2025072205496), Jul 20, 2025: SEAT TRACK. CORRODED. REAR BARREL SEAT TRACKS. AT LH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700. (LP# 
- [SDR DALA2025072205495](https://openairdocs.org/sdr/DALA2025072205495), Jul 20, 2025: SEAT TRACK. CORRODED. REAR BARREL SEAT TRACKS. AT LH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 DWG C01342700 AND A220 ASRP 51-42-00. (
- [SDR DALA2025072205494](https://openairdocs.org/sdr/DALA2025072205494), Jul 20, 2025: SEAT TRACK. CORRODED. REAR BARREL SEAT TRACKS. AT RH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700.
- [SDR DALA2025072205493](https://openairdocs.org/sdr/DALA2025072205493), Jul 19, 2025: SEAT TRACK. CORRODED. REAR BARREL SEAT TRACKS. AT RH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITI
- [SDR DALA2025070104903](https://openairdocs.org/sdr/DALA2025070104903), Jun 26, 2025: SLIDE. NO DISCREPANCY. LH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0402:2561-9101/
- [SDR DALA2025070104895](https://openairdocs.org/sdr/DALA2025070104895), Jun 26, 2025: SLIDE. NO DISCREPANCY. RH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. DEPLOYED SLIDE PER AMDS 2561-9006 STEP 1-4. SLIDE INSTALL WILL BE COMPLETED ON THE REMAINDER OF AMDS 2561
- [SDR DALA2024121111657](https://openairdocs.org/sdr/DALA2024121111657), Dec 8, 2024: LIGHT. INOPERATIVE. RT EXTERNAL REAR EMERGENCY LIGHT INOP. REMOVED AND REPLACED R/H AFT EXTERNAL LIGHT ASSEMBLY. OPS CHECKS GOOD REF A220 AMP 33-55.
- [SDR DALA2024120511474](https://openairdocs.org/sdr/DALA2024120511474), Dec 1, 2024: FAN. ABNORMAL. RECIRC AIR FAIL MSG DURING ENG START FA IN AFT GALLEY REPORTED ELECTRICAL SMELL AT SAME TIME. R/R BOTH RECIRC FILTERS PER A220 AMP 21-22-03. REMOVED RECIRC FAN 
- [SDR DALA2024082208371](https://openairdocs.org/sdr/DALA2024082208371), Aug 21, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NUMBER 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-010287-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024082208370](https://openairdocs.org/sdr/DALA2024082208370), Aug 21, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF A ROLLER WEAR MARK WITH REWORK REF 5742-01028-02B. MEASUREMENT DEPTH IS 0.011", OUTSIDE OF SPECIFIED REST
- [SDR DALA2024082208369](https://openairdocs.org/sdr/DALA2024082208369), Aug 21, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NUMBER 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FU
- [SDR DALA2025070204956](https://openairdocs.org/sdr/DALA2025070204956), Aug 19, 2024: TAPE. PEELING. LH WINGLET TIP LEADING EDGE EROSION TAPE FOUND PEELED UP. REQUIRES REPAIR. INSPECTED LH WINGLET TIP L E WHERE EROSION TAPE WAS DAMAGED & FOUND NO UNDERLYING DAM
- [SDR DALA2024052805555](https://openairdocs.org/sdr/DALA2024052805555), May 23, 2024: LANDING GEAR. FAULTED. SHIP 8127 - MISC/DE - DECLARED EMERGENCY DUE TO GEAR FAIL MSG. CREW DID RECEIVE ALL 3 GEARS DOWN AND LOCKED INDICATING GREEN. FLIGHT LANDED SAFELY. CORRECTIVE A
- [SDR DALA2025070805079](https://openairdocs.org/sdr/DALA2025070805079), Mar 10, 2024: TAPE. PEELING. ON WALK AROUND FOUND VERT STAB EROSION TAPE PEELED. GVI OF PAINT OK. FWD TO MON IAW A220 ASRP 55-32-01-01AAA-662A-A FOR 8500 FLT HRS. GVI DUE IN 850 FLT HRS. PE
- [SDR DALA2024010310787](https://openairdocs.org/sdr/DALA2024010310787), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK NBR 10 LOWER SURFACE HAS EVIDENCE OF CORROSION & PREVIOUS REWORK. REF AA6742-01028-02A. LIAISON ENGINEERING WILL. REPAIRED L/H SLAT TRACK NBR 10 
- [SDR DALA2024010310786](https://openairdocs.org/sdr/DALA2024010310786), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK NBR 1 UPPER SURFACE HAS EVIDENCE OF CORROSION & NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEF
- [SDR DALA2024010310785](https://openairdocs.org/sdr/DALA2024010310785), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK # 7 LOWER AFT SURFACE HAS WEAR AND PREVIOUSLY REWORK. REF AA5742-01028-02A. LIASON ENGINEERING WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLA
- [SDR DALA2024010310784](https://openairdocs.org/sdr/DALA2024010310784), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK NBR 8 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER
- [SDR DALA2024010310783](https://openairdocs.org/sdr/DALA2024010310783), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK NBR 7 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER 
- [SDR DALA2024010310782](https://openairdocs.org/sdr/DALA2024010310782), Dec 30, 2023: UNKNOWN. UNKNOWN. L/H SLAT TRACK NBR 2 UPPER SURFACE HAS EVIDENCE OF CORROSION NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFOR
- [SDR DALA2024010310781](https://openairdocs.org/sdr/DALA2024010310781), Dec 30, 2023: UNKNOWN. UNKNOWN. R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS RE-WORK. REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURT
- [SDR DALA2024010310780](https://openairdocs.org/sdr/DALA2024010310780), Dec 30, 2023: UNKNOWN. UNKNOWN. R/H SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTH
- [SDR DALA2023051203780](https://openairdocs.org/sdr/DALA2023051203780), May 11, 2023: UNKNOWN. UNKNOWN. WET SOCK SMELL NOTICED FROM PAX & CREW. C/W A220 NO-GO ODI 21-72. C/W W/C 0550-2001 +0550-6001. REF LOG 4086590 FOR FINDINGS. WHILE PERFORMING B.S.I. ON #2 ESN 
- [SDR DALA2023041102849](https://openairdocs.org/sdr/DALA2023041102849), Apr 8, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 8127, AD/ERA REQUIRES L/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L
- [SDR DALA2023041102848](https://openairdocs.org/sdr/DALA2023041102848), Apr 8, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 8127, AD/ERA REQUIRES R/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L
- [SDR DALA2023041102847](https://openairdocs.org/sdr/DALA2023041102847), Apr 8, 2023: UNKNOWN. UNKNOWN. AIRCRAFT 8127, ERA 607781-14AD SECTION I ISSUED FOR REPAIR TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: ERA 607781-14AD REV O SECTION I COMPL
- [SDR DALA2023020300859](https://openairdocs.org/sdr/DALA2023020300859), Feb 1, 2023: NOT ENTERED. NOT ENTERED. SHIP 8127 - DIV - TO LIT DUE TO "R ELEVATOR FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED #3 REU. (LP# 9432468)
- [SDR DALA2022110807220](https://openairdocs.org/sdr/DALA2022110807220), Nov 5, 2022: HINGE BRACKET. CRACKED. R/H HORIZONAL /ELEVATOR HINGE BRACKET # 3 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 003 00114 COMPLIE
- [SDR DALA2022110807219](https://openairdocs.org/sdr/DALA2022110807219), Nov 5, 2022: HINGE BRACKET. CRACKED. R/H HORIZONAL /ELEVATOR HINGE BRACKET # 2 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 002 00113 COMPLIE
- [SDR DALA2022110407168](https://openairdocs.org/sdr/DALA2022110407168), Nov 3, 2022: FRAME. CORRODED. AIRCRAFT 8127, UPPER CORNER OF FRAME 75 HAS CORRODED SPOT FORWARD OF WASTE BOX. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM F
- [SDR DALA2022110407167](https://openairdocs.org/sdr/DALA2022110407167), Nov 3, 2022: PAN. CORRODED. AIRCRAFT 8127, CORROSION FOUND ON FORWARD EDGE OF LAV PAN, 2 LOCATIONS. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS,
- [SDR DALA2022110407166](https://openairdocs.org/sdr/DALA2022110407166), Nov 3, 2022: ACCESS DOOR. CORRODED. AIRCRAFT 8127, CORROSION FOUND ON FWD EDGE OF LAV WASTE SERVICE DOOR (146 BR). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FI
- [SDR DALA2022110407165](https://openairdocs.org/sdr/DALA2022110407165), Nov 3, 2022: HINGE. CORRODED. AIRCRAFT 8127, BOTH HINGES ON LAV WASTE SERVICE DOOR (146 BR) CORRODED. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS,
- [SDR DALA2022110407164](https://openairdocs.org/sdr/DALA2022110407164), Nov 3, 2022: PAN. CORRODED. AIRCRAFT 8127, SEVERAL AREAS CORRODED ON LAV PAN WASTE BOX (MARKED). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AN
- [SDR DALA2022110407163](https://openairdocs.org/sdr/DALA2022110407163), Nov 3, 2022: DOUBLER. CORRODED. AIRCRAFT 8127, CORROSION FOUND ON FWD SECTION OF THE WASTE ACCESS INTERNAL DOUBLER. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE A
- [SDR DALA2023022801499](https://openairdocs.org/sdr/DALA2023022801499), Nov 1, 2022: NONE. NONE. ERA 603257-14AD SECTION I ACCOMPLISHED IN MSPDURING C CHECK TO THE WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRE. ACCOMPLISH ERA 603257-14AD SECTION II EVERY 850 
- [SDR DALA2021091505503](https://openairdocs.org/sdr/DALA2021091505503), Sep 10, 2021: RADOME. DAMAGED. RADOME REPAIR PER ERA 588183-14. RADOME SKIN/CORE REPAIRED PER ERA 588183-14. REPETITIVE INSPECTION PER ERA 588183-14 SECTION II REQUIRED EVERY 850 HRS UNTIL AC
- [SDR DALA2020101903384](https://openairdocs.org/sdr/DALA2020101903384), Oct 19, 2020: BOTTLE. LOW PRESSURE. DURING SVC CK FOUND L2 DOOR EOAM PRESSURE LOW. SERVICED L2 DOOR EOAM PER A220 AMP 52-11. C/W RII VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.
- [SDR DALA2020101903385](https://openairdocs.org/sdr/DALA2020101903385), Oct 17, 2020: BOTTLE. LOW PRESSURE. L1 DOOR EOAM IN YELLOW. SERVICED L1 DOOR EOAM PER A220 AMP 52-11. OK FOR SVC. C/W RII. VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.
- [SDR DALA2020020430875](https://openairdocs.org/sdr/DALA2020020430875), Jan 31, 2020: BOTTLE. LOW PRESSURE. L-1 DOOR EOAM PSI BELOW MINIMUMS. ACTUATOR SAFETY PIN INSTALLED FOR MAINT. SERVICED L-1 DOOR EOAM ACTUATOR PER A220 AMP 52-11. COMPLIED WITH RII REQUIREMENTS PE
- [SDR DALA2020012870629](https://openairdocs.org/sdr/DALA2020012870629), Jan 27, 2020: DAMPER. LOW PRESSURE. L1 DOOR EOAM FORWARD PASSENGER DOOR DAMPER IS IN THE RED BAND REQUIRES RII AND SERVICING. SERVICED PASSENGER ENTRY DOOR L1 EOAM I.A.W CE SERIES AMP TASK BD500-A
- [SDR DALA2020012800631](https://openairdocs.org/sdr/DALA2020012800631), Jan 22, 2020: FAIRING. CRACKED. DURING A CHECK FOUND BELLY FAIRING CRACKED AT MID E&E ACCESS DOOR. REMOVED LONGERON PER AMP 53-82. INSTALLED LONGERON TO AFT WTBF LH SUPPORT STRUCTURE P/N C0238
- [SDR DALA2019110206394](https://openairdocs.org/sdr/DALA2019110206394), Nov 2, 2019: B-NUT. LOOSE. #2 ENG FIRE EXTINGUISHING HOSE B NUT LOSE AND TORQUE STRIPE BROKEN ON ENGINE CONNECTING SIDE OF THE HOSE. REPLACE HOSE ACCORDING TO AD RELATED TASK CARD 2620-01

## 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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