# N302DU: 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: 55070
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: October 22, 2020
- Expires: October 31, 2027
- Mode S code: A3271E
- 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=302DU
- Page: https://openairdocs.org/aircraft/N302DU

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/N302DU/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 N302DU.

## FAA accident and incident reports

None matched to N302DU.

## Service difficulty reports (55, 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 DALA2026070904024](https://openairdocs.org/sdr/DALA2026070904024), Jul 6, 2026: LIGHT. INOPERATIVE. AFT RIGHT SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. R & R REAR RT EXTERNAL EMERGENCY EXIT LIGHT IAW AMP 33-55- 02-03AAA-720A-A. OPS CHKD GOOD. MEL AND PLACARD 
- [SDR DALA2026060903495](https://openairdocs.org/sdr/DALA2026060903495), Jun 7, 2026: TURBINE. DAMAGED. DIV- DIVERTED TO RDU DUE TO #2 ENGINE HIGH N2 VIBRATION. CARRIED OUT BOROSCOPE INSPECTION ON RT ENGINE. FOUND LPT DAMAGE, REQUIRES ENGINE CHANGE. ENGINE REPLACE
- [SDR DALA2026050602889](https://openairdocs.org/sdr/DALA2026050602889), May 5, 2026: PRESSURE SENSOR. FAILED. DIVERTED TO DFW DUE TO LEFT WING ANTI-ICE FAIL. REMOVED AND REPLACED OUTBOARD PRESSURE SENSOR. SECURED SENSE LINE OPS AND LEAK CHECK GOOD. (LP# 8477622, 1577317
- [SDR DALA2026042002484](https://openairdocs.org/sdr/DALA2026042002484), Apr 16, 2026: DOOR FRAME. CORRODED. AFT PASSENGER DOOR SURROUND.FWD FRAME (FR74) HAS 4 FASTENERS HOLES WITH CORROSION .-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/003 0041
- [SDR DALA2026042002483](https://openairdocs.org/sdr/DALA2026042002483), Apr 16, 2026: DOOR FRAME. CORRODED. AFT PASSENGER DOOR SURROUND.AFT FRAME (FR76) HAS 13 FASTENERS HOLES WITH CORROSION .-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/002 004
- [SDR DALA2026041402356](https://openairdocs.org/sdr/DALA2026041402356), Apr 12, 2026: SUPPORT FITTING. CORRODED. WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE LAV E SUPPORT FITTING (REF. A220 ASRP 53-61-43-06AAA-041A-A ITEM 24). COMPLIED WITH ER/A 633268-
- [SDR DALA2026041402357](https://openairdocs.org/sdr/DALA2026041402357), Apr 11, 2026: SKIN. CORRODED. AFT FUSELAGE FRAME 81, JUST FWD OF AFT ACCESSORY COMPARTMENT OPENING, CORROSION FROM CENTER LINE LEFT 18" AROUND DOOR HINGE. SUMMARY SEE NR FOR ADDITIONAL INFOR
- [SDR DALA2026041202312](https://openairdocs.org/sdr/DALA2026041202312), Apr 11, 2026: SEAT TRACK. CORRODED. AFT CABIN-SEAT TRACK LBL43.5 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342701. (LP
- [SDR DALA2026041202311](https://openairdocs.org/sdr/DALA2026041202311), Apr 11, 2026: SEAT TRACK. CORRODED. AFT CABIN-SEAT TRACK RBL23 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REMOVED DAMAGED SEAT TRACK AND INSTALLED REPAIR PARTS, COMPLIED WITH ER/A
- [SDR DALA2026041002298](https://openairdocs.org/sdr/DALA2026041002298), Apr 8, 2026: FLOOR SUPPORT. CORRODED. DURING C2 + 6 YEAR (HCK) CHECK IN MSP, MAINTENANCE FOUND CORROSION COMMON TO THE AFT FUSELAGE FLOOR LAV E SUPPORT AT FR79, LBL 23. REMOVED DAMAGED PARTS, TRIMME
- [SDR DALA2026040802254](https://openairdocs.org/sdr/DALA2026040802254), Apr 7, 2026: SEAT TRACK. CORRODED. AIRCRAFT 8302, AFT CABIN-SEAT TRACK LBL 23 NEAR LAV MOUNT FR 72 HAS CORROSION. (M) REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. CORRECTIVE ACTION: REMOVED DAM
- [SDR DALA2026040702211](https://openairdocs.org/sdr/DALA2026040702211), Apr 5, 2026: FLOOR SUPPORT. CORRODED. WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE FLOOR STRUCTURE AT 2 LOCATIONS BETWEEN FR 76 AND FR 78 JUST AFT OF THE AFT SERVICE DOOR. REMOVED
- [SDR DALA2026040702210](https://openairdocs.org/sdr/DALA2026040702210), Apr 5, 2026: FLOOR SUPPORT. CORRODED. WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE FLOOR STRUCTURE AT 1 LOCATION BETWEEN FR 76 AND FR 78 JUST AFT OF THE AFT PASSENGER DOOR. COMPLI
- [SDR DALA2026040702209](https://openairdocs.org/sdr/DALA2026040702209), Apr 5, 2026: DOUBLER. CORRODED. WASTE BOX DOUBLER HAS CORROSION ON FWD AND AFT FLANGE. REPAIRED PER PRI 632674-14 REV 0 REV 1 AND FINAL ER/A 632674-14. (LP# 1530122)
- [SDR DALA2026040602178](https://openairdocs.org/sdr/DALA2026040602178), Apr 3, 2026: SEAT TRACK. CORRODED. SEAT TRACK LBL 23 AFT INTERCOSTAL FROM FR 70 TO 71 PILOT HOLES IN NEW SEAT TRACK DO NOT LINE UP WITH INTERCOSTAL HOLES. COMPLIED WITH PRI 633015-14 REV 0 AND SE
- [SDR DALA2026040602174](https://openairdocs.org/sdr/DALA2026040602174), Apr 1, 2026: BLADE. CORRODED. NR 2 ENGINE, RT THRUST REVERSER V-BLADE HAD NUMEROUS SMALL AREAS OF CORROSION OVER ALL SEGMENTS. COMPLIED WITH PRI 632856 REV 00,01,02 AND SECTION I OF ERA 6328
- [SDR DALA2026032501996](https://openairdocs.org/sdr/DALA2026032501996), Mar 23, 2026: SEAT TRACK. CORRODED. AFT CABIN-SEAT TRACK RBL43.5 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. S
- [SDR DALA2026032301951](https://openairdocs.org/sdr/DALA2026032301951), Mar 20, 2026: SEAT TRACK. CORRODED. FWD CABIN - SEAT TRACK RBL 43.5 NEAR FR22 AT CLOSET MOUNT HAS CORROSION -M- REF. SSI 53-21-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2026032301950](https://openairdocs.org/sdr/DALA2026032301950), Mar 20, 2026: SEAT TRACK. CORRODED. FWD CABIN - SEAT TRACK RBL 23.0 NEAR FR22 AT CLOSET MOUNT HAS CORROSION -M- REF. SSI 53-21-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2026041502389](https://openairdocs.org/sdr/DALA2026041502389), Mar 18, 2026: DOUBLER. CORRODED. ER/A 632674-14 SECTION I REPAIR WAS ISSUED TO ADDRESS WASTE BOX COMPARTMENT CORROSION TO INTERNAL DOUBLER AND SKIN. FOLLOW ON ACTIONS ARE REQUIRED.ACCOMPLISH SE
- [SDR DALA2026031901903](https://openairdocs.org/sdr/DALA2026031901903), Mar 18, 2026: SEAL. DAMAGED. /H WING- DURING OK TO INSTALL # 2 SLAT FOUND TELESCOPIC DUCT SEAL DAMAGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION
- [SDR DALA2025081906215](https://openairdocs.org/sdr/DALA2025081906215), Aug 14, 2025: FRAME. NOT REPORTED. FRAME REPLACED ON WORKCARD 5352-01038-08A ASSOCIATED AA 5352-01038 ADDED FOR AC 8302. (LP# 7852131)
- [SDR DALA2025081906214](https://openairdocs.org/sdr/DALA2025081906214), Aug 14, 2025: NONE. NONE. SDR LOG CREATED PER WORKCARD 5352-01038-07A. MFG P/N C02383111-001 REPLACED ON WORKCARD 5352-01038-07A ASSOCIATED AA 5352-01038 ADDED FOR AC 8302. (LP# 7852130)
- [SDR DALA2025060104200](https://openairdocs.org/sdr/DALA2025060104200), May 25, 2025: CIRCUIT CARD. FAULTED. SHIP 8302 - ATO DUE TO FMS SPEED MESSAGE. CAPTAINS V SPEEDS WERE GRAYED OUT AT THROTTLE UP. RETURNED TO GATE. DEFERRED PER MEL 34-61-01A. LATER: REPLACED FMS 1 
- [SDR DALA2025040802745](https://openairdocs.org/sdr/DALA2025040802745), Apr 2, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 PINION TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. C/W ER
- [SDR DALA2025040802744](https://openairdocs.org/sdr/DALA2025040802744), Apr 2, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #4 RACK TOOTH (1 EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. C/W ERA
- [SDR DALA2025040802743](https://openairdocs.org/sdr/DALA2025040802743), Apr 2, 2025: SLAT TRACK. CORRODED. LH SLAT TRACK #6 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 621466-14AD REV B AND P
- [SDR DALA2025021901226](https://openairdocs.org/sdr/DALA2025021901226), Feb 16, 2025: SLIDE. WARNING MESSAGE. WING SLIDE CAUTION MESSAGE (52 WING SLIDE - R OWEE SLIDE INOP). REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT DOOR SLIDE PER W /C 2563-4005.(D.D 830324) ALL R
- [SDR DALA2024101510104](https://openairdocs.org/sdr/DALA2024101510104), Oct 11, 2024: FLANGE. BROKEN. DURING REMOVAL OF WTBF PANEL 195HB FOUND WTBF LONGERON ASSEMBLY NUT PLATE ATTACHMENT FLANGES BROKEN 2 EA P/N: C02383111-001. INSTALLED WTBF LONGERON ASSEMBLY P/
- [SDR DALA2024082208373](https://openairdocs.org/sdr/DALA2024082208373), Aug 22, 2024: CONTROL LEVER. STIFF. FA REPORTS 1 LEFT DOOR ARM/DISARM LEVER IS STIFF AND GETS STUCK BEFORE REACHING FULL DISARM MODE. DURING OPS CHK OF 1L REF 52-11-00, TASK 320A-A ON 3RD ATTEMPT 
- [SDR DALA2025050103375](https://openairdocs.org/sdr/DALA2025050103375), Jul 20, 2024: SKIN. ERODED. R/H HORIZONTAL STABILIZER TIP EROSION PROTECTIVE MATERIAL REQUIRES REPAIR. INSPECTED RH HORIZONTAL TIP IN AREA WHERE EROSION TAPE WAS DAMAGE AND FOUND NO UNDERL
- [SDR DALA2024030503038](https://openairdocs.org/sdr/DALA2024030503038), Feb 29, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SU
- [SDR DALA2024030503037](https://openairdocs.org/sdr/DALA2024030503037), Feb 29, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 UPPER FWD SURFACE IAW ER/A 
- [SDR DALA2024030503036](https://openairdocs.org/sdr/DALA2024030503036), Feb 29, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 UPPER FWD SURFACE IAW ER/A 
- [SDR DALA2024030503035](https://openairdocs.org/sdr/DALA2024030503035), Feb 29, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER
- [SDR DALA2024030503034](https://openairdocs.org/sdr/DALA2024030503034), Feb 29, 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 DALA2024030503033](https://openairdocs.org/sdr/DALA2024030503033), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 10 UPPER AFT OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 UPPER AFT OB SIDE IAW ER/
- [SDR DALA2024030503032](https://openairdocs.org/sdr/DALA2024030503032), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 9 LOWER FWD OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LOWER FWD OB SIDE IAW ER/A 
- [SDR DALA2024030503031](https://openairdocs.org/sdr/DALA2024030503031), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER
- [SDR DALA2024030503030](https://openairdocs.org/sdr/DALA2024030503030), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE IAW ER
- [SDR DALA2024030503029](https://openairdocs.org/sdr/DALA2024030503029), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 LOWER AFT SURFACE IAW ER/A 
- [SDR DALA2024030503028](https://openairdocs.org/sdr/DALA2024030503028), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SU
- [SDR DALA2024030503027](https://openairdocs.org/sdr/DALA2024030503027), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IN 2 LOCATION
- [SDR DALA2024030503026](https://openairdocs.org/sdr/DALA2024030503026), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER
- [SDR DALA2024030503025](https://openairdocs.org/sdr/DALA2024030503025), Feb 29, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER
- [SDR DALA2023091407549](https://openairdocs.org/sdr/DALA2023091407549), Sep 9, 2023: UNKNOWN. UNKNOWN. R1 DOOR HAS DENT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 128-0002:0500-2004/002 00314 REPAIRED PER PRI 610830-14 
- [SDR DALA2023090807370](https://openairdocs.org/sdr/DALA2023090807370), Sep 7, 2023: UNKNOWN. UNKNOWN. ER/A 610830-14 REV A ISSUED FOR SECTION IV PERMANENT REPAIR ACCOMPLISHMENT. FOLLOW ON ACTION (DTE) IS REQUIRED. DTE IS REQUIRED. ER/A 610830-14 REV A SECTION IV
- [SDR DALA2023081506635](https://openairdocs.org/sdr/DALA2023081506635), Aug 10, 2023: UNKNOWN. UNKNOWN. FORWARD CARGO COMPARTMENT DOOR SCUFF PLATE, INSIDE AFT POCKET AREA HAS 2 EA. FASTENER HOLES WITH EVIDENCE OF CORROSION. 'M'. SCEPTRE LOG PAGE ENTERED FOR SDR RE
- [SDR DALA2024041304395](https://openairdocs.org/sdr/DALA2024041304395), Aug 9, 2023: SCUFF PLATE. CORRODED. AIRCRAFT 8302, DURING C CHECK IN MSP MTC REPORTED CORROSION UNDER THE SCUFF PLATES SILL, POST BLENDING THE MINIMUM REPORTED THICKNESS WAS LOWER THAN REQUIRED. C
- [SDR DALA2023050903641](https://openairdocs.org/sdr/DALA2023050903641), May 5, 2023: UNKNOWN. UNKNOWN. SHIP 8302 - ATB - DUE TO AFT CARGO DOOR CAUTION MESSAGE. CORRECTIVE ACTION: FOUND DOOR HANDLE RED FLAG DISPLAYED. CYCLED MULTIPLE TIMES DOOR HANDLE REMAINED FLU

All 55: https://openairdocs.org/aircraft/N302DU/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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