# N301DU: 2021 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: 55069
- Year built: 2021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 18, 2021
- Certificate issued: March 18, 2021
- Expires: March 31, 2028
- Mode S code: A32367
- 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=301DU
- Page: https://openairdocs.org/aircraft/N301DU

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/N301DU/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 N301DU.

## FAA accident and incident reports

None matched to N301DU.

## 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 DALA2026092205308](https://openairdocs.org/sdr/DALA2026092205308), Sep 16, 2026: DOOR FRAME. CORRODED. DURING H CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-02C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE AFT CARGO DOOR SURROUND ST
- [SDR DALA2026092205307](https://openairdocs.org/sdr/DALA2026092205307), Sep 16, 2026: DOOR FRAME. CORRODED. AFT SERVICE DOOR SURROUND - FR76 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. AC
- [SDR DALA2026092205306](https://openairdocs.org/sdr/DALA2026092205306), Sep 16, 2026: DOOR FRAME. CORRODED. AFT SERVICE DOOR SURROUND - FR74 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. AC
- [SDR DALA2026092205305](https://openairdocs.org/sdr/DALA2026092205305), Sep 16, 2026: SKIN. CORRODED. EVIDENCE OF CORROSION FOUND AT AFT WTB FUSELAGE SKIN, AIRCRAFT CENTERLINE. (M)(P) REF CORROSION SSI: 53-50-02-05. COMPLIED WITH ER/A 636443-14 PRI REV 0, ER/A 6
- [SDR DALA2026092205304](https://openairdocs.org/sdr/DALA2026092205304), Sep 16, 2026: STRINGER. DAMAGED. WHILE REMOVING DAMAGED SKIN IAW PRI 636395-14, STR 36L BETWEEN FR 34-35 DAMAGED BY CUTOFF WHEEL. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV
- [SDR DALA2026092205303](https://openairdocs.org/sdr/DALA2026092205303), Sep 16, 2026: SKIN. CORRODED. CORROSION FOUND ON BOTTOM SKIN AT FWD EDGE OF WTBF, BETWEEN STR36L. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636
- [SDR DALA2026092205302](https://openairdocs.org/sdr/DALA2026092205302), Sep 15, 2026: DOOR SILL. DAMAGED. FWD CARGO DOOR SURROUND STRUCTURE, LWR SILL AREA (AREA COVERED BY SCUFF PLATES), SKIN PANEL, SILL. COMPLIED WITH ER/A 636422-14 PRI REV 0 AND FINAL ER/A 636422-
- [SDR DALA2026092205301](https://openairdocs.org/sdr/DALA2026092205301), Sep 15, 2026: WASTE BOX. CORRODED. WASTE BOX RIGHT SIDE INNER LIP HAS CORROSION. -M- REF. CORROSION SSI: 53-61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A
- [SDR DALA2026092205300](https://openairdocs.org/sdr/DALA2026092205300), Sep 15, 2026: WASTE BOX. CORRODED. WASTE BOX FWD RIGHT CORNER HAS CORROSION MULTIPLE PLACES AND SURROUNDING RIGHT HINGE FITTING. -M- -P- REF. CORROSION SSI: 53- 61-56-02. COMPLIED WITH ER/A 61185
- [SDR DALA2026091605181](https://openairdocs.org/sdr/DALA2026091605181), Sep 8, 2026: LONGERON. CORRODED. ER/A 636601-14 CORROSION REPAIR TO WING TO BODY FAIRING LH LONGERON BETWEEN FR 40 TO FR 48 REQUIRES FOLLOW ON ACTION. ACCOMPLISH 636601-14 SECT II REP INSPECTIO
- [SDR DALA2026091105088](https://openairdocs.org/sdr/DALA2026091105088), Sep 8, 2026: FRAME. CORRODED. CORROSION R/H SIDE FRAME PART # C02382152-102 AT MULTIPLE LOWER PANEL FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0537:2090-2001/007 00307 REM
- [SDR DALA2026091105087](https://openairdocs.org/sdr/DALA2026091105087), Sep 7, 2026: SLIDE. NO TEST. WHILE PERFORMING AMDS 2561-9005-CHECK, THE LH OWEED SLIDE FAILED DEPLOYMENT WITH BOTH NORMAL OPERATION AND BY PULLING THE BACKUP T-HANDLE. SLIDE MPN IS 68332-10
- [SDR DALA2026091005075](https://openairdocs.org/sdr/DALA2026091005075), Sep 6, 2026: SEAT TRACK. CORRODED. FR74 RT INBD SEAT TRACK INSERT CORRODED. SEE INFORMATION 001-0585:5300-2016/004 00428. REMOVED AND REPLACED SEAT TRACK IAW ASRP 51-40-00. (LP# 1799083; AIRCRAFT
- [SDR DALA2026090204954](https://openairdocs.org/sdr/DALA2026090204954), Aug 31, 2026: THRESHOLD. CORRODED. LEFT AFT PAX DOOR THRESHOLD PANEL, AFT INBD CORNER WAS CORRODED. REMOVED AND REPLACED THE THRESHOLD PANEL IAW ASRP 51-40-00. (LP# 1786990; AIRCRAFT WAS GROUNDED
- [SDR DALA2026090104932](https://openairdocs.org/sdr/DALA2026090104932), Aug 29, 2026: FRAME. CORRODED. CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783796; AIRCRAFT 
- [SDR DALA2026090104931](https://openairdocs.org/sdr/DALA2026090104931), Aug 29, 2026: FRAME. CORRODED. CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783791; AIRCRAFT 
- [SDR DALA2026082704867](https://openairdocs.org/sdr/DALA2026082704867), Aug 24, 2026: FRAME. CORRODED. CORROSION ON RT SIDE FRAME AT MULTIPLE LOWER PANEL FASTENER AREAS. WORKED WITH NR 303 FOR REMOVAL AND REPLACEMENT OF LONGERON. (LP# 1774104; AIRCRAFT WAS GROUND
- [SDR DALA2025112508590](https://openairdocs.org/sdr/DALA2025112508590), Nov 23, 2025: LONGERON. CRACKED. WORKING AMDS 5352-01038-01A W/P 2967182 STEP 10D FOUND LONGERON P/N C02383111-001 CRACKED MID LENGTH ADJ TO TIE ROD IN THE VICINITY OF LBL 40.0. REMOVED LONGERO
- [SDR DALA2025112508591](https://openairdocs.org/sdr/DALA2025112508591), Nov 22, 2025: CONTROL UNIT. MALFUNCTIONED. R BRAKE FAIL CAUTION MESSAGE OCCURRED AFTER DROPPING LANDING GEAR FOR LANDING. AFTER LANDING, THE RIGHT BRAKE SEEMED TO GRAB WHEN NOT DEPRESSING RIGHT BRAKE PED
- [SDR DALA2025042403228](https://openairdocs.org/sdr/DALA2025042403228), Apr 17, 2025: SLAT TRACK. CORRODED. FOUND RH SLAT TRACK #4 RACK TOOTH #1 AND #2, HAS EVIDENCE OF CORROSION AFT SURFACE AND PREVIOUS REWORK, 5742-01028-02B. LIAISON ENGINEERING REQUIRED BEFORE FURT
- [SDR DALA2025042103106](https://openairdocs.org/sdr/DALA2025042103106), Apr 16, 2025: SLAT TRACK. CORRODED. FOUND LH SLAT TRACK #6 RACK TOOTH #2, HAS EVIDENCE OF CORROSION AFT SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER
- [SDR DALA2025042103105](https://openairdocs.org/sdr/DALA2025042103105), Apr 16, 2025: SLAT TRACK. CORRODED. FOUND LH SLAT TRACK #4 PINION TOOTH #1 AND #2, HAS EVIDENCE OF CORROSION LWR SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFOR
- [SDR DALA2025042103104](https://openairdocs.org/sdr/DALA2025042103104), Apr 16, 2025: SLAT TRACK. CORRODED. FOUND LH SLAT TRACK #6 PINION TOOTH #2, HAS EVIDENCE OF CORROSION LWR SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. PERFORMED HFEC PER STEP 8 OF PRI. REF A22
- [SDR DALA2024101109974](https://openairdocs.org/sdr/DALA2024101109974), Oct 10, 2024: FRAME. CRACKED. CRACK FOUND ON WQTBF FRAME FORWARD OF RH WHEEL BIN REMOVED 194DB PANEL FOR ACCESS. AND REMOVED ONE HI-LOK FASTENER FOR EASE OF MEASURING THE CRACK (412863) ER/A
- [SDR DALA2024100209611](https://openairdocs.org/sdr/DALA2024100209611), Oct 1, 2024: RACK. CORRODED. LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W RII. (LP# 
- [SDR DALA2024100209610](https://openairdocs.org/sdr/DALA2024100209610), Oct 1, 2024: PINION. CORRODED. LG SLAT TRACK#4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W II. (LP# 
- [SDR DALA2024100209609](https://openairdocs.org/sdr/DALA2024100209609), Oct 1, 2024: PINION. CORRODED. RH SLAT TRACK #11 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W RII. (LP# 0586594)
- [SDR DALA2024100209608](https://openairdocs.org/sdr/DALA2024100209608), Oct 1, 2024: PINION. CORRODED. RH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620906-14 REV 0 STEP 7. C/W RII. (LP
- [SDR DALA2024100209607](https://openairdocs.org/sdr/DALA2024100209607), Oct 1, 2024: PINION. CORRODED. RH SLAT TRACK #11 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. PERFORMED NDT PER PRI 620906-14 REV 0 STEP 7. C/W RII. (LP# 0586563)
- [SDR DALA2024040904235](https://openairdocs.org/sdr/DALA2024040904235), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024040904234](https://openairdocs.org/sdr/DALA2024040904234), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 PINION HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 PINION IN 2 LOCATION I
- [SDR DALA2024040904233](https://openairdocs.org/sdr/DALA2024040904233), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-011028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/
- [SDR DALA2024040904232](https://openairdocs.org/sdr/DALA2024040904232), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A
- [SDR DALA2024040904231](https://openairdocs.org/sdr/DALA2024040904231), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A
- [SDR DALA2024040904230](https://openairdocs.org/sdr/DALA2024040904230), Apr 6, 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 DALA2024040904229](https://openairdocs.org/sdr/DALA2024040904229), Apr 6, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 FWD RACK TEETH HAVE EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-011028-02B. REPAIRED RH SLAT TRACK NBR 4 FWD RACK TEE
- [SDR DALA2024040904228](https://openairdocs.org/sdr/DALA2024040904228), Apr 6, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD S
- [SDR DALA2024040904227](https://openairdocs.org/sdr/DALA2024040904227), Apr 6, 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 DALA2024040904226](https://openairdocs.org/sdr/DALA2024040904226), Apr 6, 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 DALA2024040904225](https://openairdocs.org/sdr/DALA2024040904225), Apr 6, 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 DALA2024040904224](https://openairdocs.org/sdr/DALA2024040904224), Apr 6, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 PINION HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 PINION IN 2 LOCATIONS 
- [SDR DALA2024040904223](https://openairdocs.org/sdr/DALA2024040904223), Apr 6, 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 DALA2024040904222](https://openairdocs.org/sdr/DALA2024040904222), Apr 6, 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 FWD SURFACE IAW ER/A 60886
- [SDR DALA2024040904221](https://openairdocs.org/sdr/DALA2024040904221), Apr 6, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024040204035](https://openairdocs.org/sdr/DALA2024040204035), Mar 27, 2024: BRAKE ASSY. FAILED. SHIP 8301 - MISC / DE - DUE TO "RT BRAKE DEGRADED" ADVISORY MESSAGE. CORRECTIVE ACTION: R/R #3 AND #4 MLG BRAKE ASSEMBLIES. R/R #4 EMCU. (LP# 5798435, 5798432)
- [SDR DALA2024012601200](https://openairdocs.org/sdr/DALA2024012601200), Jan 25, 2024: SEAT TRACK. CORRODED. SEAT TRACK, LBL 23 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/108 00207 COMPL
- [SDR DALA2024012601207](https://openairdocs.org/sdr/DALA2024012601207), Jan 24, 2024: COVER. UNKNOWN. THE AFT FLOOR MOUNT COVERS FOR LAV C ARE RAISED.SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/065 000
- [SDR DALA2024012601199](https://openairdocs.org/sdr/DALA2024012601199), Jan 24, 2024: SEAT TRACK. CORRODED. SEAT TRACK, RBL 43.5 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/106 00205 COM
- [SDR DALA2024012601198](https://openairdocs.org/sdr/DALA2024012601198), Jan 24, 2024: SEAT TRACK. CORRODED. SEAT TRACK, RBL 23 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/107 00206 COMPL
- [SDR DALA2024012601197](https://openairdocs.org/sdr/DALA2024012601197), Jan 24, 2024: SEAT TRACK. CORRODED. SEAT TRACK, LBL 43.5 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/109 00208 COM

All 62: https://openairdocs.org/aircraft/N301DU/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
- The Pratt & Whitney PW1521G SERIE engine: https://openairdocs.org/engine/pratt-whitney-pw1521g-serie.md

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