# N104DU: C Series Aircraft Ltd Ptnrsp BD-500-1A10

- Status: Valid registration
- Airframe: [C Series Aircraft Ltd Ptnrsp BD-500-1A10](https://openairdocs.org/model/c-series-aircraft-ltd-ptnrsp-bd-500-1a10) (registry code 1400012, 133 seats)
- Data sheets: [TCDS T00008NY](https://openairdocs.org/tcds/T00008NY) (Airbus Canada Limited Partnership) (OpenAirDocs)
- Serial number: 50023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: December 31, 2018
- Expires: December 31, 2028
- Mode S code: A013EE
- 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=104DU
- Page: https://openairdocs.org/aircraft/N104DU

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): 66 in force

### Matched by airframe (C Series Aircraft Ltd Ptnrsp BD-500-1A10)

- [AD 2026-15-14](https://openairdocs.org/ad/2026-15-14): Engine fuel and control · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 3, 2026
- [AD 2026-13-52](https://openairdocs.org/ad/2026-13-52): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 7, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-10-12](https://openairdocs.org/ad/2026-10-12): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-10](https://openairdocs.org/ad/2026-10-10): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-10-07](https://openairdocs.org/ad/2026-10-07): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2026
- [AD 2026-07-04](https://openairdocs.org/ad/2026-07-04): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 11, 2026
- [AD 2026-06-06](https://openairdocs.org/ad/2026-06-06): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 1, 2026
- [AD 2026-07-07](https://openairdocs.org/ad/2026-07-07): Air conditioning system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 17, 2026
- [AD 2026-04-04](https://openairdocs.org/ad/2026-04-04): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 8, 2026
- [AD 2025-20-08](https://openairdocs.org/ad/2025-20-08): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 30, 2025
- [AD 2025-19-07](https://openairdocs.org/ad/2025-19-07): Electrical system installation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 6, 2025
- [AD 2025-19-01](https://openairdocs.org/ad/2025-19-01): Autoflight · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 23, 2025
- [AD 2025-17-01](https://openairdocs.org/ad/2025-17-01): Flight controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 29, 2025
- [AD 2025-16-01](https://openairdocs.org/ad/2025-16-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 18, 2025
- [AD 2025-09-02](https://openairdocs.org/ad/2025-09-02): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 18, 2025
- [AD 2025-06-06](https://openairdocs.org/ad/2025-06-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 2, 2025
- [AD 2025-05-07](https://openairdocs.org/ad/2025-05-07): Standard practices/structures · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 15, 2025
- [AD 2025-02-06](https://openairdocs.org/ad/2025-02-06): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 9, 2025
- [AD 2025-03-05](https://openairdocs.org/ad/2025-03-05): Stabilizers · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Mar 21, 2025
- [AD 2024-24-08](https://openairdocs.org/ad/2024-24-08): Equipment/Furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 13, 2025
- [AD 2024-23-05](https://openairdocs.org/ad/2024-23-05): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 6, 2025
- [AD 2024-22-01](https://openairdocs.org/ad/2024-22-01): Time Limits/Maintenance Checks · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 31, 2024
- [AD 2024-22-04](https://openairdocs.org/ad/2024-22-04): Fuselage · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 17, 2024
- [AD 2024-22-03](https://openairdocs.org/ad/2024-22-03): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 14, 2024
- [AD 2024-15-06](https://openairdocs.org/ad/2024-15-06): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Oct 15, 2024
- [AD 2024-17-04](https://openairdocs.org/ad/2024-17-04): Landing Gear · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 20, 2024
- [AD 2024-12-02](https://openairdocs.org/ad/2024-12-02): Portable Oxygen System · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 13, 2024
- [AD 2024-10-11](https://openairdocs.org/ad/2024-10-11): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 1, 2024
- [AD 2024-10-03](https://openairdocs.org/ad/2024-10-03): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 28, 2024
- [AD 2024-07-11](https://openairdocs.org/ad/2024-07-11): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 6, 2024
- [AD 2024-05-10](https://openairdocs.org/ad/2024-05-10): Electrical Power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-05-08](https://openairdocs.org/ad/2024-05-08): Flight Controls · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective May 22, 2024
- [AD 2024-04-08](https://openairdocs.org/ad/2024-04-08): Electrical power · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 23, 2024
- [AD 2023-24-01](https://openairdocs.org/ad/2023-24-01): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 2, 2024
- [AD 2023-20-01](https://openairdocs.org/ad/2023-20-01): Fire protection · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 9, 2023
- [AD 2023-16-03](https://openairdocs.org/ad/2023-16-03): Pneumatic · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 25, 2023
- [AD 2023-16-02](https://openairdocs.org/ad/2023-16-02): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 22, 2023
- [AD 2023-12-09](https://openairdocs.org/ad/2023-12-09): Flight control system · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Aug 7, 2023
- [AD 2023-14-02](https://openairdocs.org/ad/2023-14-02): Navigation · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jul 27, 2023
- [AD 2023-07-05](https://openairdocs.org/ad/2023-07-05): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10. Effective May 30, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-07-01](https://openairdocs.org/ad/2023-07-01): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Apr 19, 2023
- [AD 2022-26-06](https://openairdocs.org/ad/2022-26-06): Placards and markings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Feb 2, 2023
- [AD 2022-25-19](https://openairdocs.org/ad/2022-25-19): Hardware, Engine Exhaust · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023
- [AD 2022-25-05](https://openairdocs.org/ad/2022-25-05): Wings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jan 23, 2023
- [AD 2022-21-03](https://openairdocs.org/ad/2022-21-03): Fuel · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Dec 14, 2022
- [AD 2022-16-02](https://openairdocs.org/ad/2022-16-02): Doors · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Nov 25, 2022
- [AD 2022-16-08](https://openairdocs.org/ad/2022-16-08): Turbine/turboprop engine · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Sep 1, 2022
- [AD 2022-11-21](https://openairdocs.org/ad/2022-11-21): Equipment/furnishings · Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11. Effective Jun 15, 2022

### 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 76: https://openairdocs.org/aircraft/N104DU/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 N104DU.

## FAA accident and incident reports

None matched to N104DU.

## Service difficulty reports (96, 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 DALA2026012300525](https://openairdocs.org/sdr/DALA2026012300525), Jan 19, 2026: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS SYSTEMS. R & R AFT RT LED ASSEMBLY PER AMP 33-55. OPS CK GOOD MEL + PLACARD INSTALLED. (LP# 7904243)
- [SDR DALA2025121209104](https://openairdocs.org/sdr/DALA2025121209104), Dec 9, 2025: UNKNOWN. ODOR. ON APPROACH AT 4000' MSL, BOTH PILOTS NOTICED FUMES ON THE FLT DECK. VERY NOTICEABLE DIRTY SOCK SMELL. NO VISIBLE FUMES. 2 PACKS, SINGLE RIGHT BLEED DUE TO MEL 
- [SDR DALA2025120408875](https://openairdocs.org/sdr/DALA2025120408875), Dec 1, 2025: NONE. NONE. DAMAGE TOLERANCE EVALUATION. ERA 621788-14, REV B, PROVIDES STAGE 2 APPROVAL FOR SECTION IV REPAIR. FOLLOW ON ACTION IS REQUIRED ON THE FUSELAGE SKIN FWD OF FR 
- [SDR DALA2025042403240](https://openairdocs.org/sdr/DALA2025042403240), Apr 20, 2025: SMOKE DETECTOR. FAULTED. FA REPORTED BURNING SMELL IN RIGHT AFT LAV, SMOKE DETECTOR BEEPED TWICE FA CALL LIGHT WENT ON THEN OUT AND SMELL DISSIPATED CONFERRED WITH MAINT CONTROL FOLLOWE
- [SDR DALA2025040802751](https://openairdocs.org/sdr/DALA2025040802751), Apr 3, 2025: UNKNOWN. ODOR. ON TAXI OUT RECEIVED CALL FROM AFT FA'S STATING SMELL OF DIRTY SOCKS COMING FROM AFT AIR VENTS. FORWARD FA SMELLED NOTHING UPFRONT WENT TO BACK AND SMELLED DIRT
- [SDR DALA2025030201591](https://openairdocs.org/sdr/DALA2025030201591), Feb 27, 2025: OUTLET. FAILED. AIRCRAFT 8104, RIGHT AFT LAV WAS REPORTED THAT THE EMERGENCY HORN AND LIGHT REPEATLY TRIPPED. THEY ALSO REPORTED SMELLING A MILD ELECTRICAL ODOR. FOUND OUTLET U
- [SDR DALA2025011300286](https://openairdocs.org/sdr/DALA2025011300286), Jan 10, 2025: SKIN. CORRODED. CORROSION SSI: 53-60-02-03. CORROSION FOUND BETWEEN FR 70 AND FR71 AND BETWEEN STGR 36L AND STGR 35L. REPAIRED PER PRI 622727-14 REV 0,1,2,3 AND ERA 622727-14 R
- [SDR DALA2025100207162](https://openairdocs.org/sdr/DALA2025100207162), Jan 9, 2025: SEAT TRACK. CORRODED. OUTBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK PER ER/A 622672-14 PRI REV. 0, REV. 1, REV. 2, AND FIN
- [SDR DALA2025011300285](https://openairdocs.org/sdr/DALA2025011300285), Jan 9, 2025: SEAT TRACK. CORRODED. REFERENCE AMDS 5300-2015. SSI 53-61-43-01. SEAT TRACK CORROSION NOTED AT RBL 23.0 AT FRAME 61. REMOVED AND REPLACED SEAT TRACK REF. A220 ASRP 51-77-00-28. (LP# 
- [SDR DALA2025011300284](https://openairdocs.org/sdr/DALA2025011300284), Jan 8, 2025: SEAT TRACK. CORRODED. SSI: 53-21-43-01 SEAT TRACK CORROSION RBL 43.5 AT FRAME 20 (M)(P ) LOG-PAGE UPDATED @ 08JAN25 2130 UTC 02 CORR BY SACHS 00583347 MSP 08JAN25 ATA 5346 RII: N ENT
- [SDR DALA2025011300283](https://openairdocs.org/sdr/DALA2025011300283), Jan 8, 2025: DOOR. CORRODED. WHILE ACCOMPLISHING AFT CARGO DOOR CORROSION INSPECTION PER AMDS 5331-01297-02C, FOUND CORROSION AT/AROUND HOLES 1OL, 2OL, 3OL, 4OL, 5OL, 6OL, 7OL, 8OL, 9OL, 10
- [SDR DALA2025011300282](https://openairdocs.org/sdr/DALA2025011300282), Jan 8, 2025: SKIN. CORRODED. FWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION BETWEEN HOLES 5OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATI
- [SDR DALA2025011300281](https://openairdocs.org/sdr/DALA2025011300281), Jan 8, 2025: SKIN. CORRODED. FWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 0.75" ABOVE HOLE 3OL. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2025011300280](https://openairdocs.org/sdr/DALA2025011300280), Jan 8, 2025: DOOR SILL. DAMAGED. FWD RH SERVICE/PASSENGER DOOR, LOWER DOOR SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 045-0001:5331-01297- 01B/002 00260 REPAIRED REF ER/A 622538-14 PRI REV
- [SDR DALA2025011300279](https://openairdocs.org/sdr/DALA2025011300279), Jan 8, 2025: SERVICE DOOR. CORRODED. WHILE ACCOMPLISHING FWD RIGHT SERVICE/PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-01B, FOUND CORROSION AT/AROUND HOLES 4OL, 8OL, SUMMARY SEE NR FOR 
- [SDR DALA2025011300278](https://openairdocs.org/sdr/DALA2025011300278), Jan 8, 2025: SKIN. CORRODED. AFT RIGHT PASSENGER/SERVICE DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 1.5" ABOVE/FWD OF HOLE 12OL. MARKED. SUMMARY SEE NR FOR AD
- [SDR DALA2025011300277](https://openairdocs.org/sdr/DALA2025011300277), Jan 8, 2025: SEAT TRACK. CORRODED. SSI: 53-21-43-01 SEAT TRACK CORROSION LBL 43.5 FORWARD OF FRAME 22 (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION
- [SDR DALA2025011300276](https://openairdocs.org/sdr/DALA2025011300276), Jan 8, 2025: SEAT TRACK. CORRODED. SSI: 53-61-43-02. LEFT INBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR A
- [SDR DALA2025011000227](https://openairdocs.org/sdr/DALA2025011000227), Jan 7, 2025: DOOR SILL. CORRODED. AFT LH PASSENGER DOOR, LOWER DOOR SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297- 02A/003 00249 REPAIRED PER ER/A 622582-14 PRI REV 0, REV 
- [SDR DALA2025011000226](https://openairdocs.org/sdr/DALA2025011000226), Jan 7, 2025: SKIN. CORRODED. WHILE ACCOMPLISHING AFT LEFT PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-02A, FOUND CORROSION AT/AROUND HOLES 12OL. SUMMARY SEE NR FOR ADDITIONAL IN
- [SDR DALA2025011000225](https://openairdocs.org/sdr/DALA2025011000225), Jan 7, 2025: SKIN. CORRODED. WHILE ACCOMPLISHING FWD CARGO DOOR CORROSION INSPECTION PER AMDS 5331-01297-01C, FOUND CORROSION AT/AROUND HOLES 13OL, 14OL, 16OL, 17OL, 18OL, 19OL, 20OL. SUMMA
- [SDR DALA2025010800173](https://openairdocs.org/sdr/DALA2025010800173), Jan 4, 2025: NONE. NONE. RE-INSTALL PREVIOUSLY REMOVED FWD CARGO DOOR UPPER SCUFF PLATE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 046-0001:5
- [SDR DALA2025010600114](https://openairdocs.org/sdr/DALA2025010600114), Jan 3, 2025: SEAT TRACK. CORRODED. RIGHT OUTBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORM
- [SDR DALA2025010612133](https://openairdocs.org/sdr/DALA2025010612133), Dec 31, 2024: DOOR SILL. NOT REPORTED. SSI: 53-21-25-02. FWD CARGO, LOWER SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:5321-2015/001 00261 REMOVED AND REPLACED LOWER SILL AND CORNER STRIK
- [SDR DALA2025010212124](https://openairdocs.org/sdr/DALA2025010212124), Dec 30, 2024: FRAME. CORRODED. AFT EQUIPMENT BAY FRAME 81 (JUST FWD OF ACCESS DOOR 867) AFT FACE HAS CORROSION BETWEEN L36-R36 (FOUND DURING INSPECTION OF ACCESS DOOR 867). SCEPTRE LOG PAGE E
- [SDR DALA2024123112108](https://openairdocs.org/sdr/DALA2024123112108), Dec 27, 2024: SKIN. CRACKED. LEFT WING, #2 SLAT CUTOUT IS CRACKED AT UPPER OUTBOARD CORNER. VERIFIED BY HFEC AT .457 INCHES LONG. MARKED/PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. S
- [SDR DALA2024123112107](https://openairdocs.org/sdr/DALA2024123112107), Dec 27, 2024: SKIN. CRACKED. RIGHT WING, #5 SLAT TRACK CUT OUT HAS A CRACK AT UPPER OUTBOARD CORNER. VERIFIED BY HFEC AT .236 INCHES LONG. MARKED/PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REP
- [SDR DALA2025011300287](https://openairdocs.org/sdr/DALA2025011300287), Oct 22, 2024: SKIN. DENTED. RAMP REPORTS DENT ON UPPER RT FUSELAGE AREA/CANOPY. FND DENT TO BE NEAR FRAME 15, DENT IS 4 3/16" BY 2 3/4" WITH A DEPTH OF .038". OUT OF LIMITS PER A220 ASRP 5
- [SDR DALA2024091909195](https://openairdocs.org/sdr/DALA2024091909195), Sep 9, 2024: BLEED AIR SYS. ODOR. BLEED AIR SYSTEMS - ENGINE **DISPATCHER SELECT EXTENSION** MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG RE DEFERRAL REQUIRED.- -DURING T/O ROLL HAD STRONG ODOR AS
- [SDR DALA2024091709115](https://openairdocs.org/sdr/DALA2024091709115), Sep 8, 2024: UNKNOWN. ODOR. DIRTY SOCK SMELL - BEGAN ON TAKEOFF ROLL, LASTED ABOUT 5 MINUTES THEN DISSIPATED UNTIL FINAL APPROACH AND TAXI-IN. WHEN THE DIRTY SOCK ODOR WAS NOTICEABLE AGAIN
- [SDR DALA2024052305450](https://openairdocs.org/sdr/DALA2024052305450), May 22, 2024: WASTE BOX. CORRODED. MON ERA 596162-14AD CORROSION IN WASTE BOX. WHILE PERFORMING REPEAT INSPECTION II OF ERA 596162-14AD REV ORIGINAL NOTED CORROSION ON EXTERNAL SKIN AND IN RH LOW
- [SDR DALA2024031803421](https://openairdocs.org/sdr/DALA2024031803421), Mar 16, 2024: LENS. MISSING. ON SVC CHK, PORTION CHECKING EMERGENCY ESCAPE PATH LIGHTING FOUND R1 DOOR ILLUMINATION LIGHT LENS MISSING. REPLACED MISSING R1 DOOR GENERAL ILLUMINATION ESCAPE 
- [SDR DALA2024013001383](https://openairdocs.org/sdr/DALA2024013001383), Jan 28, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 UPPER AFT INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE 
- [SDR DALA2024013001381](https://openairdocs.org/sdr/DALA2024013001381), Jan 28, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE 
- [SDR DALA2024013001380](https://openairdocs.org/sdr/DALA2024013001380), Jan 28, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 5 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024013001378](https://openairdocs.org/sdr/DALA2024013001378), Jan 28, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF A WEAR MARK AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FUR
- [SDR DALA2024013001376](https://openairdocs.org/sdr/DALA2024013001376), Jan 28, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024013001375](https://openairdocs.org/sdr/DALA2024013001375), Jan 27, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024013001374](https://openairdocs.org/sdr/DALA2024013001374), Jan 27, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER FWD INBOUND SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE 
- [SDR DALA2024013001373](https://openairdocs.org/sdr/DALA2024013001373), Jan 27, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE
- [SDR DALA2024013001372](https://openairdocs.org/sdr/DALA2024013001372), Jan 27, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 6 UPPER AFT INBOARD SIDE HAS EVIDENCE OF WEAR MARK AND PREVIOUS REWORK REF REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEF
- [SDR DALA2024013001371](https://openairdocs.org/sdr/DALA2024013001371), Jan 27, 2024: SLAT TRACK. CORRODED. LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901265](https://openairdocs.org/sdr/DALA2024012901265), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901264](https://openairdocs.org/sdr/DALA2024012901264), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 7 INBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE F
- [SDR DALA2024012901263](https://openairdocs.org/sdr/DALA2024012901263), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901262](https://openairdocs.org/sdr/DALA2024012901262), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901261](https://openairdocs.org/sdr/DALA2024012901261), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901260](https://openairdocs.org/sdr/DALA2024012901260), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH
- [SDR DALA2024012901259](https://openairdocs.org/sdr/DALA2024012901259), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURT
- [SDR DALA2024012901272](https://openairdocs.org/sdr/DALA2024012901272), Jan 27, 2024: SLAT TRACK. CORRODED. RH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTH

All 96: https://openairdocs.org/aircraft/N104DU/reports.md

## STCs that may be installed (OpenAirDocs) (15)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (C Series Aircraft Ltd Ptnrsp BD-500-1A10)

- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST02570LA](https://openairdocs.org/stc/ST02570LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST11389DS](https://openairdocs.org/stc/ST11389DS): Installation of Delta Comfort Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04792NY](https://openairdocs.org/stc/ST04792NY): Update of Intelsat 2Ku. Delta Engineering Corporation
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST04483AT](https://openairdocs.org/stc/ST04483AT): Installation of the Avionics Support Group Constant Friction Mount (cfMount) with Cradle. Avionics Support Group Inc
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST03972NY](https://openairdocs.org/stc/ST03972NY): Installation of Honeywell Satcom SBB Upgrade and WiFi Network Activation. UMLAUT ENGINEERING GMBH
- [STC ST04073NY](https://openairdocs.org/stc/ST04073NY): Installation of navAero Electronic Flight Bag provisions. Delta Engineering Corporation
- [STC ST00149IB](https://openairdocs.org/stc/ST00149IB) (historical): Installation of a Cabin air exhaust muffler, to reduce this noise to a more comfortable level by installing a valve cap and sound damping system. DOA21 LIMITED

## Related

- Other C Series Aircraft Ltd Ptnrsp BD-500-1A10 aircraft: https://openairdocs.org/model/c-series-aircraft-ltd-ptnrsp-bd-500-1a10/aircraft.md

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