# N305DU: 2020 Airbus Canada LP BD-500-1A11

- Status: Valid registration
- Airframe: [Airbus Canada LP BD-500-1A11](https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11) (registry code 1400015, 153 seats)
- Engine: [Pratt & Whitney PW1521G SERIE](https://openairdocs.org/engine/pratt-whitney-pw1521g-serie) (registry code 51763)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership) (OpenAirDocs)
- Serial number: 55084
- Year built: 2020
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 2020
- Certificate issued: October 30, 2020
- Expires: October 31, 2027
- Mode S code: A33243
- 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=305DU
- Page: https://openairdocs.org/aircraft/N305DU

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): 71 in force

### Matched by airframe (Airbus Canada LP BD-500-1A11)

- [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 2025-12-04](https://openairdocs.org/ad/2025-12-04): Hydraulic Power · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 25, 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 2025-11-06](https://openairdocs.org/ad/2025-11-06): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective Jun 16, 2025
- [AD 2025-07-04](https://openairdocs.org/ad/2025-07-04): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A11. Effective May 27, 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 2024-09-01](https://openairdocs.org/ad/2024-09-01): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Jul 2, 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 2024-03-09](https://openairdocs.org/ad/2024-03-09): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A11. Effective Apr 16, 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 2023-10-02](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

### Matched by engine (Pratt & Whitney PW1521G SERIE)

None in force.

### 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

All 81: https://openairdocs.org/aircraft/N305DU/ads.md

## Information bulletins (advisory) (1 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

## NTSB investigations

None matched to N305DU.

## FAA accident and incident reports

None matched to N305DU.

## Service difficulty reports (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 DALA2026061103538](https://openairdocs.org/sdr/DALA2026061103538), Jun 8, 2026: DOOR FRAME. DAMAGED. AFT SERVICE DOOR FR74 DURING DVI INSPECTION HOLE #9 PER ER/A 634028-14 FOUND HOLE #9 OUT OF ROUND FR76. FOR ADDITIONAL INFORMATION 001-0584:5300-2008/010 00579 
- [SDR DALA2026061003516](https://openairdocs.org/sdr/DALA2026061003516), Jun 6, 2026: INSERT. CORRODED. AFT PAX DOOR SURROUND PANEL ATTACH NUT INSERTS HAVE LIGHT CORROSION AT FR76. COMPLIED WITH ERA 634027-14 PRI REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, RE
- [SDR DALA2026061003515](https://openairdocs.org/sdr/DALA2026061003515), Jun 6, 2026: INSERT. CORRODED. AFT PASSENGER DOOR SURROUND ATTACH NUT INSERTS 8EA AT FR74 HAVE LIGHT CORROSION. COMPLIED WITH ERA 634027-14 PRI REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6
- [SDR DALA2026060903494](https://openairdocs.org/sdr/DALA2026060903494), Jun 5, 2026: SKIN. CORRODED. DURING C2 + 6 YEAR (HEAVY) CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING THE EO 5331-01297-01C WORKCARD / SB BD500-530010 MODIFICATION WHEN CORROSION WAS FOUND CO
- [SDR DALA2026060903493](https://openairdocs.org/sdr/DALA2026060903493), Jun 5, 2026: DOOR FRAME. CORRODED. DURING HEAVY CHECK IN MSP, MAINTENANCE FOUND CORROSION COMMON TO THE FWD SERVICE DOOR SURROUND FRAMES. FR 17 P/N C02316001-011 AND FR 20 P/N C02316003-011 ARE A
- [SDR DALA2026060903492](https://openairdocs.org/sdr/DALA2026060903492), Jun 5, 2026: SKIN. CORRODED. DURING C2 + 6Y ( H ) CHECK IN MSP, DAL FOUND CORROSION LOCALIZED AROUND THE SKIN SCUFF PLATE ATTACH HOLES PREVIOUSLY REPAIRED VIA REO 500-53-21-651. MTC REQUIRE
- [SDR DALA2026060403392](https://openairdocs.org/sdr/DALA2026060403392), Jun 2, 2026: FAIRING. CORRODED. NR 1 PYLON AFT FIXED FAIRING HAS CORROSION IN MULTIPLE FASTENER HOLES AND PITTING ON THE STRUCTURE. COMPLIED WITH ER/A 633933-14 PRI REV 0, 1 AND ER/A 633933-14
- [SDR DALA2026060403391](https://openairdocs.org/sdr/DALA2026060403391), Jun 2, 2026: BEARING. DAMAGED. BEARINGS FOUND DAMAGED ON PYLON SIDE LINK UPPER ATTACHMENT FITTING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH ERA 634589-14, PRI REV 0, 01, 02 A
- [SDR DALA2026060403390](https://openairdocs.org/sdr/DALA2026060403390), Jun 2, 2026: SEAT TRACK. CORRODED. SEAT TRACK LBL 43.5 NEAR FR74 AT AFT END HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH ERA 634276-14 PRI REV 0 AND E RA 634276-14 SEC
- [SDR DALA2026060303374](https://openairdocs.org/sdr/DALA2026060303374), May 31, 2026: BEARING. DAMAGED. SPHERICAL BEARINGS FOUND DAMAGED ON PYLON SIDE LINK LOWER ATTACHMENT FITTING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMAT
- [SDR DALA2026060403393](https://openairdocs.org/sdr/DALA2026060403393), May 21, 2026: THRUST REVERSER. CORRODED. DURING H CHK IN MSP, CORROSION AND/OR MISSING COATING WAS FOUND ON THE #2 ENG, INBD THRUST REVERSER (P/N 999-3001577 WITH FTN 5T0778) TORQUE BOX V-BLADE AT THE 
- [SDR DALA2026052003096](https://openairdocs.org/sdr/DALA2026052003096), May 20, 2026: SKIN. CORRODED. LEVEL 2 CORROSION FOUND ON THE EXTERNAL FUSELAGE SKIN SURFACE NEAR FR 35 AND STGR 1R AND 1L. BLENDED SKIN PER ER/A 634142-14 PRI REV 0,1,2 AND REV ORIGINAL MIN 
- [SDR DALA2026051803053](https://openairdocs.org/sdr/DALA2026051803053), May 16, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION. SEAT TRACK RBL 23.0 NEAR FR74 AT AFT END HAS CORRISION. CORRECTIVE ACTION: REPLACED SEAT TRACK REF A220 AS PER RP BD500-A-J51-77-00-00AAA-028
- [SDR DALA2026051803052](https://openairdocs.org/sdr/DALA2026051803052), May 16, 2026: BRAKE. NO TEST. HORIZONTAL STAB BRAKE FAILED FUNCTION TEST. REPLACED HORIZONTAL STAB BRAKE AND PERFORMED FUNCTION CHECK PER AMP 27-41-01. (LP 1596950 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302994](https://openairdocs.org/sdr/DALA2026051302994), May 9, 2026: SEAT TRACK. CORRODED. SEAT TRACK RBL 43.5 NEAR FR22 AT FRONT END HAS CORROSION -P- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/003 00387 REPAIRED PER ER/A 623174-14T
- [SDR DALA2026051302993](https://openairdocs.org/sdr/DALA2026051302993), May 9, 2026: SEAT TRACK. CORRODED. SEAT TRACK RBL 23.0 NEAR FR22 AT FRONT END HAS CORROSION -P- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/002 00386 REMOVED AND REPLACED PER SEA
- [SDR DALA2026051302992](https://openairdocs.org/sdr/DALA2026051302992), May 9, 2026: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE- FWD END OF THE SEAT TRACK AT LBL43.5, FR22 IS CORRODED. "M" SEE PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0573:5321-2022/004 004
- [SDR DALA2026051302991](https://openairdocs.org/sdr/DALA2026051302991), May 9, 2026: SEAT TRACK. CORRODED. SEAT TRACK AT 23LBL AT FR 74 HAS CORROSION. REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2015/001 0051
- [SDR DALA2026051302990](https://openairdocs.org/sdr/DALA2026051302990), May 9, 2026: SEAT TRACK. CORRODED. SEAT TRACK AT RBL43 AT FR 74 HAS CORROSION. REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2015/002 0051
- [SDR DALA2026050602885](https://openairdocs.org/sdr/DALA2026050602885), May 3, 2026: THRESHOLD. NOT REPORTED. PERFORMED AN OPPORTUNITY INSPECTION OF FWD AND AFT SERVICE AND PASSENGER DOOR THRESHOLD PANELS AND SURROUNDING STRUCTURE IAW AMP 05-40-00. SEE NR FOR ADDITIONAL
- [SDR DALA2026050402800](https://openairdocs.org/sdr/DALA2026050402800), Apr 30, 2026: LONGERON. CRACKED. WING TO BODY FAIRING LONGERON FOUND CRACKED. REPLACED WTBF LONGERON IAW ASRP 53-82-55 AND A220 ASRP 51- 42-21. (LP# 1570816; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051403013](https://openairdocs.org/sdr/DALA2026051403013), Apr 27, 2026: ATTACH FITTING. CORRODED. AFT RT GALLEY-AFT RT FLOOR ATTACH POINT CORRODED 8" FORWARD OF FR 79. REF SSI 53-61-43-02. NO REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0586:5
- [SDR DALA2026042802691](https://openairdocs.org/sdr/DALA2026042802691), Apr 25, 2026: SLIDE. NO TEST. RIGHT OVERWING SLIDE MECHANISM FAILED STEP 6C OF AMDS 5221-2001-02. (EXTERNAL SLIDE DEPLOYMENT MECHANISM ARM DID NOT RETURN TO NORMAL POSITION AFTER OWEED DOOR 
- [SDR DALA2026030401496](https://openairdocs.org/sdr/DALA2026030401496), Feb 25, 2026: LENS. MISSING. R1 DOOR OVERHEAD EMERGENCY LIGHT LENS MISSING. APPLIED ER/A 632694-14 REV. ORIG. SECTION 1: TIME LIMITED REPAIR . TEMPORARY LENS INSTALLED. PERMANENT RESTORATIO
- [SDR DALA2025121009038](https://openairdocs.org/sdr/DALA2025121009038), Dec 7, 2025: LANDING GEAR. FAULTED. ATB - DUE TO LOUD BANG AND "GEAR DISAGREE" AND "WOW FAIL" MESSAGES. SWITCHED TO SECONDARY NOSE LANDING GEAR STRUT SEALS, PERFORMED GEAR SWING TEST. OK FOR SERVI
- [SDR DALA2025091506775](https://openairdocs.org/sdr/DALA2025091506775), Aug 31, 2025: WIRE HARNESS. SHORTED. AFTER LEFT ENGINE START, ELECTRICAL FAULT LT FBW PC PMG INOPERATIVE. T/S IAW EFIM, FAULT CODE 2401F3249, RELAY PREVIOUSLY CHANGED, WIRING CHECK FOR PINS X1 & X2
- [SDR DALA2025042403239](https://openairdocs.org/sdr/DALA2025042403239), Apr 18, 2025: UNKNOWN. ODOR. ON SHUTDOWN ELECTRICAL ODOR IN FORWARD GALLEY AND FLIGHT DECK. T/S PER AMDS WORKCARD 0550-2001. NO TROUBLE FOUND.NO. FUMES COULD BE FELT. NO RESIDUAL ODORS NOTE
- [SDR DALA2024092609469](https://openairdocs.org/sdr/DALA2024092609469), Sep 25, 2024: SWITCH. MALFUNCTIONED. AIRCRAFT 8305, EMER LIGHTS ON STATUS MSG DURING FLIGHT. EMER LIGHTS BATT FAULT MSG ON CMC. CORRECTIVE ACTION: CYCLED EMERGENCY LIGHT POWER SWITCH IAW A220 AMP 3
- [SDR DALA2024080707861](https://openairdocs.org/sdr/DALA2024080707861), Aug 4, 2024: ENGINE. ODOR. ON GROUND (BEFORE TAKEOFF) FOUL SMELL THROUGH OUT CABIN AND COCKPIT. FA CREWS SAID THEY HAD THE SAME ODOR DURING THEIR LAST LEG OUT OF MSO. SAID THEY HAD MAINTE
- [SDR DALA2024022102404](https://openairdocs.org/sdr/DALA2024022102404), Feb 18, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. MEASURED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 6112
- [SDR DALA2024022102403](https://openairdocs.org/sdr/DALA2024022102403), Feb 18, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024022102402](https://openairdocs.org/sdr/DALA2024022102402), Feb 18, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024022102401](https://openairdocs.org/sdr/DALA2024022102401), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 UPPER AFT IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 UPPER AFT IB SIDE IAW ER/A
- [SDR DALA2024022102400](https://openairdocs.org/sdr/DALA2024022102400), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A
- [SDR DALA2024022102399](https://openairdocs.org/sdr/DALA2024022102399), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD IB SIDE IAW ER/A
- [SDR DALA2024022102398](https://openairdocs.org/sdr/DALA2024022102398), Feb 18, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN TWO LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD
- [SDR DALA2024022102397](https://openairdocs.org/sdr/DALA2024022102397), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024022102396](https://openairdocs.org/sdr/DALA2024022102396), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024022102395](https://openairdocs.org/sdr/DALA2024022102395), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024022102394](https://openairdocs.org/sdr/DALA2024022102394), Feb 18, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024022102393](https://openairdocs.org/sdr/DALA2024022102393), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A
- [SDR DALA2024022102392](https://openairdocs.org/sdr/DALA2024022102392), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024022102391](https://openairdocs.org/sdr/DALA2024022102391), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A
- [SDR DALA2024022102390](https://openairdocs.org/sdr/DALA2024022102390), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2024022102389](https://openairdocs.org/sdr/DALA2024022102389), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A
- [SDR DALA2024022102388](https://openairdocs.org/sdr/DALA2024022102388), Feb 18, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A
- [SDR DALA2023091907710](https://openairdocs.org/sdr/DALA2023091907710), Sep 9, 2023: UNKNOWN. UNKNOWN. SHIP 8305 - ATB - DUE TO FUEL IMBALANCE. CORRECTIVE ACTION: R/R RT WING TRANSFER FLOAT VALVE. (LP# 4035978)
- [SDR DALA2023081506639](https://openairdocs.org/sdr/DALA2023081506639), Aug 14, 2023: UNKNOWN. UNKNOWN. LH WING SLAT TRACK 4 DAMAGED, ON INBD UPPER FWD, LOWER AFT, LOWER OUTBD FWD. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATI
- [SDR DALA2023042603268](https://openairdocs.org/sdr/DALA2023042603268), Apr 22, 2023: UNKNOWN. UNKNOWN. R PACK OVHT CAUTION MSG FOLLOWED BY L PACK OVHT MSG ON TAXI COMPLIED WITH ABNORMAL CHECKLISTS. REFERENCE LOG 4748840 AND 2730343 FOR CORRECTIVE ACTION. OK FOR S
- [SDR DALA2022092906398](https://openairdocs.org/sdr/DALA2022092906398), Sep 25, 2022: NONE. NONE. SHIP 8305 - ATB - DUE TO NUMBER 2 HYDRAULIC QTY ZERO AND HYDRAULIC PRESSURE LOW. ATC DECLARED EMERGENCY FOR THE FLIGHT. CORRECTIVE ACTION: TIGHTENED PYLON HYDRA

## STCs that may be installed (OpenAirDocs) (13)

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 LP BD-500-1A11)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST04818NY](https://openairdocs.org/stc/ST04818NY): Installation of a Passenger Seat Re-Pitch. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST04803NY](https://openairdocs.org/stc/ST04803NY): Installation of a Panasonic Avionics In-Flight Entertainment System. Delta Engineering Coporation
- [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 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

## Related

- Other Airbus Canada LP BD-500-1A11 aircraft: https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11/aircraft.md
- The Pratt & Whitney PW1521G SERIE engine: https://openairdocs.org/engine/pratt-whitney-pw1521g-serie.md

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