# N307DU: 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)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership) (OpenAirDocs)
- Serial number: 55096
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: January 29, 2021
- Expires: January 31, 2028
- Mode S code: A339B1
- 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=307DU
- Page: https://openairdocs.org/aircraft/N307DU

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

### 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/N307DU/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 N307DU.

## FAA accident and incident reports

None matched to N307DU.

## Service difficulty reports (62, 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 DALA2026092805386](https://openairdocs.org/sdr/DALA2026092805386), Sep 22, 2026: BEARING. SHEARED. L1 DOOR STUCK ON ARRIVAL. FOUND INTERLOCK BEARING SHEARED. REMOVED REMAINING PIECES IAW AMP 52-15. INSTALLED NEW INTERLOCK LEVER IAW AMP 52-15. DOOR OPS NORMAL.
- [SDR DALA2026080704583](https://openairdocs.org/sdr/DALA2026080704583), Aug 6, 2026: FITTING. CORRODED. FWD CARGO DOOR ENTRY WAY BETWEEN FR24 & FR29 FITTINGS 4EA AT ENTRY FOR SUPPORTING FLOOR HAVE CORROSION LEVEL 2 ON TOP SURFACE AND PAINT DETERIORATED. REPLACED T
- [SDR DALA2026080704582](https://openairdocs.org/sdr/DALA2026080704582), Aug 6, 2026: BUSHING. CORRODED. PITTING FOUND ON INNER RACE OF R3 INBOARD BUSHING. REPLACED BUSHING NR 436. (LP 1742279 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080504503](https://openairdocs.org/sdr/DALA2026080504503), Aug 3, 2026: THRESHOLD. CORRODED. FWD LT PASSENGER DOOR THRESHOLD 221 KLF HAS CORROSION IN FASTENER HOLE, FWD OTBD CORNER. R & R SILL ASSEMBLY PANEL 221KLF REF AMP 53-00-47. (LP# 1736819; AIRCRA
- [SDR DALA2026080504504](https://openairdocs.org/sdr/DALA2026080504504), Aug 2, 2026: SKIN. CRACKED. LEFT WING, LE, NR 2 SLAT TRACK CUTOUT CRACKED 0.219, AFT OTBD RADIUS, VERIFIED WITH HFEC IAW AND TP BD500-A-J51-01-08- 01AAA-353A-A. SEE NR FOR ADDITIONAL INFOR
- [SDR DALA2026080504502](https://openairdocs.org/sdr/DALA2026080504502), Aug 2, 2026: DOUBLER. CORRODED. WASTE BOX DOUBLER CORROSION AT CUTOUT ON FWD RH CORNER AND AFT EDGE. COMPLIED WITH ER/A 613288-14 REV A PRI REV 0, ER/A 613288-14 REV A PRI REV 1, AND FINAL ER/
- [SDR DALA2026080404483](https://openairdocs.org/sdr/DALA2026080404483), Jul 31, 2026: SCUFF PLATE. CORRODED. DURING C2 + 6 YEAR (HEAVY) CHECK IN MSP, MTC WAS ACCOMPLISHING AA 5331-01297-01C MOD WHEN THEY REPORTED CORROSION UNDER THE SCUFF PLATE, ON THE SUBJECT (PN C023
- [SDR DALA2026073104438](https://openairdocs.org/sdr/DALA2026073104438), Jul 29, 2026: FLOOR SUPPORT. CORRODED. PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR SUPPORT BEAM FR 76-78, AT RBL 37. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFOR
- [SDR DALA2026072804361](https://openairdocs.org/sdr/DALA2026072804361), Jul 27, 2026: THRESHOLD. NO DISCREPANCY. REMOVE AFT SERVICE DOOR THRESHOLD PANEL TO FOM. ADDITIONAL INFORMATION 001-0582:5300-2008/006 00536 REMOVED AND REINSTALLED THRESHOLD PANEL 242MRF PER A220 AMP 
- [SDR DALA2026071604193](https://openairdocs.org/sdr/DALA2026071604193), Jul 15, 2026: SEAT TRACK. CORRODED. AFT MOST CABIN SEAT TRACK RBL 23 SHOWS SIGNS OF CORROSION. COMPLIED WITH ER/A 635190-14 PRI REV 0, ER/A 635190-14 PRI REV 1 AND FINAL ER/A 635190-14 REV ORIGINA
- [SDR DALA2026071604191](https://openairdocs.org/sdr/DALA2026071604191), Jul 15, 2026: FLOORBEAM. CORRODED. LEFT PASSENGER FLOOR HAS CORROSION AT ATTACHMENT HOLE LOCATED FR76 LBL 52.5. REMOVED AND REPLACED FLOOR BEAM REF DWG C01342759 REV D AND A220 ASRP 51-42-00. (LP
- [SDR DALA2026071604192](https://openairdocs.org/sdr/DALA2026071604192), Jul 14, 2026: ATTACH FITTING. CORRODED. CORROSION FOUND ON RH OUTER UPPER FORWARD PYLON ATTACH FITTINGS R7 AND R8 . REMOVED AND REPLACED BEARINGS PER BOMBARDIER DWG C01627010 -B. (LP# 1700103; AIRCRAF
- [SDR DALA2026071604189](https://openairdocs.org/sdr/DALA2026071604189), Jul 14, 2026: FLOOR SUPPORT. CORRODED. PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, RBL 53. REPLACED EDGE SUPPORT MEMBER PER ASRP 51-42-06. (LP# 1699452; AIRCRAFT WAS 
- [SDR DALA2026071604187](https://openairdocs.org/sdr/DALA2026071604187), Jul 13, 2026: FITTING. CORRODED. RIGHT FLOOR FITTING HAS CORROSION NEAR FR 74 UNDER DOOR THRESHOLD PANEL. REMOVED AND REPLACED PER ASRP 51-77-00-00-028. CORROSION IS LEVEL 2. (LP 1697908; AIRCR
- [SDR DALA2026071504163](https://openairdocs.org/sdr/DALA2026071504163), Jul 11, 2026: FLOOR SUPPORT. CORRODED. PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, LBL 54.5. -M- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/004 0056
- [SDR DALA2026071304117](https://openairdocs.org/sdr/DALA2026071304117), Jul 9, 2026: SEAT TRACK. CORRODED. AFT MOST CABIN SEAT TRACK RBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-20. (LP# 1690284; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071304113](https://openairdocs.org/sdr/DALA2026071304113), Jul 8, 2026: SEAT TRACK. CORRODED. FWD SEAT TRACK RBL 23 SHOWS SIGNS OF CORROSION . SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2022/002 00
- [SDR DALA2026071304112](https://openairdocs.org/sdr/DALA2026071304112), Jul 8, 2026: FLOORBEAM. CORRODED. PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, LBL 49. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL I
- [SDR DALA2026071004050](https://openairdocs.org/sdr/DALA2026071004050), Jul 7, 2026: THRESHOLD. CORRODED. FWD SERVICE DOOR THRESHOLD, CORROSION FOUND AT AFT INBD CORNER. DRILLED NEW THRESHOLD, REF ASRP BD500-A-J51-77-00-00AAA-028A-A. INSTALLATION TO BE ACCOMPLISHED 
- [SDR DALA2026071004049](https://openairdocs.org/sdr/DALA2026071004049), Jul 7, 2026: THRESHOLD. CORRODED. FWD SERVICE DOOR THRESHOLD - CORROSION FOUND AT FWD INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:
- [SDR DALA2026070703958](https://openairdocs.org/sdr/DALA2026070703958), Jun 30, 2026: DOOR SILL. CORRODED. FWD RT SERVICE DOOR, FWD THRESHOLD ATTACHMENT HOLE HAS LIGHT CORROSION. SILL ASSEMBLY REPLACED IAW ASRP 53-21-24 AND DRAWINGS C02312000 AND C02316000. (LP# 1674
- [SDR DALA2026070703956](https://openairdocs.org/sdr/DALA2026070703956), Jun 28, 2026: SEAT TRACK. CORRODED. FWD SEAT TRACK LBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK REF. A220 ASRP 51-77-00. (LP# 1670327; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070703955](https://openairdocs.org/sdr/DALA2026070703955), Jun 28, 2026: SEAT TRACK. CORRODED. FWD SEAT TRACK RBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW ASRP BD500- A-J51-42-00-00AAA-028A-A AND DWG C02312600. (LP# 1670326; AIRC
- [SDR DALA2026070703953](https://openairdocs.org/sdr/DALA2026070703953), Jun 27, 2026: BEARING. CORRODED. CORROSION FOUND ON NR 1 ENGINE PYLON UPPER FORWARD SPHERICAL BEARINGS R7 AND R8. REMOVED AND REPLACED BEARINGS IAW DWG C01627010 -B. (LP# 1669886; AIRCRAFT WAS 
- [SDR DALA2026070703952](https://openairdocs.org/sdr/DALA2026070703952), Jun 27, 2026: BEARING. DAMAGED. NR 1 ENGINE PYLON BOX BEAM R7. REMOVED AND REPLACED THE BEARINGS IAW DWG C01701332. (LP# 1669877; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062303732](https://openairdocs.org/sdr/DALA2026062303732), Jun 20, 2026: THRESHOLD. CORRODED. LEFT PASSENGER DOOR THRESHOLD, CORROSION FOUND IN ATTACHMENT HOLE AT FR 74 LBL 54.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL I
- [SDR DALA2026062303735](https://openairdocs.org/sdr/DALA2026062303735), Jun 20, 2026: FLOOR SUPPORT. CORRODED. PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR SUPPORT FR 76-78, AT LBL 37. REMOVED AND REPLACED FLOOR SUPPORT PER ASRP 51-77-00. (LP# 1656729; AIRCRAFT WAS GRO
- [SDR DALA2025122309351](https://openairdocs.org/sdr/DALA2025122309351), Dec 21, 2025: LONGERON. CRACKED. LONGERON AT RBL 40.0 CRACKED AT FWD END APPROX 18"LONG AT RADIUS BETWEEN VERT & OUTER FLANGES. AD RELATED, WC 5352-01038-01B. REMOVED AND REPLACED LONGERON @ RB
- [SDR DALA2025051303717](https://openairdocs.org/sdr/DALA2025051303717), May 9, 2025: PINION. CORRODED. LH SLAT TRACK #11 MEASUREMENTS WERE OUT-OF-LIMITS. ENGINEERING REQUESTS TO REMOVE AND REPLACE PINION P/N: C01612526-001. REMOVED SLAT PINION #11 IAW A220 AMP 27
- [SDR DALA2025051303716](https://openairdocs.org/sdr/DALA2025051303716), May 9, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #11, RACK TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION AFT PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. CO
- [SDR DALA2025051303715](https://openairdocs.org/sdr/DALA2025051303715), May 9, 2025: PINION. CORRODED. LH PINION #11, TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION LWR PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WI
- [SDR DALA2025051303714](https://openairdocs.org/sdr/DALA2025051303714), May 9, 2025: PINION. CORRODED. LH PINION #4, TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION LWR & PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED W
- [SDR DALA2025051303713](https://openairdocs.org/sdr/DALA2025051303713), May 9, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4, RACK TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION AFT PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COM
- [SDR DALA2025031902076](https://openairdocs.org/sdr/DALA2025031902076), Mar 16, 2025: LONGERON. BROKEN. FOUND 1 EA LONGERON ASSEMBLY P/N: C02383111-001 BROKEN. REMOVED AND REPLACED LONGERON P/N: C02383111-001 IAW AMDS W/C 5352-01038-05A. (LP# 0860849)
- [SDR DALA2024091208944](https://openairdocs.org/sdr/DALA2024091208944), Sep 7, 2024: SLAT TRACK. NOT REPORTED. REMOVE AND REPLACE LH #4 SLAT TRACK AND PINION. SUMMARY. REPLACEMENT WORKED IN CONJUNCTION WITH AMDS W/C 2781- 4002-LH. REMOVED AND REPLACED L/H SLAT TRACK #4 P
- [SDR DALA2024090908858](https://openairdocs.org/sdr/DALA2024090908858), Sep 5, 2024: SLAT TRACK. CORRODED. LH#7 SLAT TRACK UPPER FWD HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORMED HFE
- [SDR DALA2024090908862](https://openairdocs.org/sdr/DALA2024090908862), Sep 4, 2024: SLAT TRACK. CORRODED. LH #8 SLAT TRACK LOWER FWD I/B HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORME
- [SDR DALA2024090908859](https://openairdocs.org/sdr/DALA2024090908859), Sep 4, 2024: SLAT TRACK. CORRODED. LH #7 SLAT TRACK LOWER FWD I/B HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORME
- [SDR DALA2024021302089](https://openairdocs.org/sdr/DALA2024021302089), Feb 10, 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 DALA2024021302088](https://openairdocs.org/sdr/DALA2024021302088), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 
- [SDR DALA2024021302087](https://openairdocs.org/sdr/DALA2024021302087), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 60804
- [SDR DALA2024021302086](https://openairdocs.org/sdr/DALA2024021302086), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 60804
- [SDR DALA2024021302085](https://openairdocs.org/sdr/DALA2024021302085), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD SURFACE IAW ER/A 
- [SDR DALA2024021302084](https://openairdocs.org/sdr/DALA2024021302084), Feb 10, 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 DALA2024021302083](https://openairdocs.org/sdr/DALA2024021302083), Feb 10, 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 DALA2024021302082](https://openairdocs.org/sdr/DALA2024021302082), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 
- [SDR DALA2024021302081](https://openairdocs.org/sdr/DALA2024021302081), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER/A 
- [SDR DALA2024021302080](https://openairdocs.org/sdr/DALA2024021302080), Feb 10, 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 DALA2024021302079](https://openairdocs.org/sdr/DALA2024021302079), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 
- [SDR DALA2024021302078](https://openairdocs.org/sdr/DALA2024021302078), Feb 10, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 

All 62: https://openairdocs.org/aircraft/N307DU/reports.md

## 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

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