# N102DU: 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: 50021
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: August 8, 2020
- Expires: August 31, 2027
- Mode S code: A00C80
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=102DU
- Page: https://openairdocs.org/aircraft/N102DU

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/N102DU/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 N102DU.

## FAA accident and incident reports

None matched to N102DU.

## Service difficulty reports (82, 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 DALA2026091505149](https://openairdocs.org/sdr/DALA2026091505149), Sep 11, 2026: SKIN. CORRODED. WHILE PERFORMING REP INSPECTION PER ER/A 612524-14 REV C. FOUND CORROSION ON SKIN FWD OF WASTE PNL. BLENDED SKIN MINIMUM AMOUNT TO REMOVE CORROSION IAW ASRP 51 
- [SDR DALA2026091605179](https://openairdocs.org/sdr/DALA2026091605179), Sep 10, 2026: SKIN. CORRODED. ER/A 612524-14 SECTION VII TIME LIMITED REPAIR VI WAS ISSUED FOR CORROSION FOUND ON THE FUSELAGE EXTERIOR SURFACE ADJACENT TO THE WASTE SERVICE CUTOUT, DURING S
- [SDR DALA2026052403144](https://openairdocs.org/sdr/DALA2026052403144), May 24, 2026: HYDRAULIC LINE. SHEARED. CREW DECLARED EMERGENCY DUE TO NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE LOSS. FOUND PRESSURE LINE FOR SYS 2 SHEARED. ALSO FOUND LOWER CLOSURE RIB BROKEN. ACC
- [SDR DALA2026050402803](https://openairdocs.org/sdr/DALA2026050402803), Apr 29, 2026: SLIDE. WARNING MESSAGE. LEFT WING SLIDE CAUTION ON LANDING. R & R LEFT OVER WING EMERGENCY EXIT DOOR SLIDE PER 2563-4002 VERIFIED SLIDE INSTALL PIN REMOVED RII COMPLETED. QC 5352 (4840
- [SDR DALA2026042002485](https://openairdocs.org/sdr/DALA2026042002485), Apr 18, 2026: PUMP. FAILED. DECLARED EMERGENCY DUE TO HYD PUMP 2B FAIL. REPLACED HYD PUMP 2B, RT EDP AND RUDDER PCU. R & R CASE DRAIN FILTER, PRESSURE FILTER ELEMENT, HYDRAULIC LINE AND O-
- [SDR DALA2026032301955](https://openairdocs.org/sdr/DALA2026032301955), Mar 23, 2026: REU. FAILED. DIV - TO CLE DUE TO "RUDDER FAIL" WARNING MESSAGE. REPLACED #1 AFT REU. OK FOR SERVICE. (LP# 8384156)
- [SDR DALA2025081105982](https://openairdocs.org/sdr/DALA2025081105982), Aug 9, 2025: HANDLE. UNSECURE. SHIP 8102 - DIV - DUE TO FORWARD CARGO DOOR CAUTION MSG FOLLOWED BY CABIN PRESSURE WARNING. EMERGENCY WAS DECLARED. CORRECTIVE ACTION: FOUND FORWARD CARGO DOOR 
- [SDR DALA2025061304495](https://openairdocs.org/sdr/DALA2025061304495), Jun 9, 2025: SLAT TRACK. DAMAGED. LH SLAT TRACK #6 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER F
- [SDR DALA2025061304494](https://openairdocs.org/sdr/DALA2025061304494), Jun 9, 2025: SLAT TRACK. DAMAGED. LH SLAT TRACK #6 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLI
- [SDR DALA2025061304493](https://openairdocs.org/sdr/DALA2025061304493), Jun 9, 2025: SLAT TRACK. DAMAGED. RH SLAT TRACK #4 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER 
- [SDR DALA2025061304492](https://openairdocs.org/sdr/DALA2025061304492), Jun 9, 2025: SLAT TRACK. DAMAGED. RH SLAT TRACK #4 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHE
- [SDR DALA2025022701551](https://openairdocs.org/sdr/DALA2025022701551), Feb 18, 2025: ENGINE. ODOR. AIRCRAFT 8102, SWEATY SOCK SMELL DURING FINAL APPROCH AND TAXI IN. CORRECTIVE ACTION: C/W WORK CARD 0550-2001 AND WORK CARD 0550-6001. PERFORMED DUCT BURN OUT A
- [SDR DALA2025012900708](https://openairdocs.org/sdr/DALA2025012900708), Jan 22, 2025: ENGINE. ODOR. DIRTY SOCK SMELL ON T/O UNTIL AROUND 50000 FEET, AFTER LANDING DIRTY SOCK SMELL BECAME WORSE/ MORE PRONOUNCED. WORK IAW JIC 0550-2003, 0550-2001, JIC 0550-6001-
- [SDR DALA2024121711786](https://openairdocs.org/sdr/DALA2024121711786), Dec 11, 2024: NOT REPORTED. NOT REPORTED. NR WRITTEN FOR THE CONTINUATION COMMENTS OF ER/A 621981-14 PRI REV 1, STEP 9. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMAT
- [SDR DALA2024121711797](https://openairdocs.org/sdr/DALA2024121711797), Dec 11, 2024: SEAT TRACK. CORRODED. LEFT OUTBOARD AFT END OF SEAT TRACK HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND ON TOP SURFACE AND PITTING OF SEAT TRACK @ FRAME
- [SDR DALA2024121111658](https://openairdocs.org/sdr/DALA2024121111658), Dec 8, 2024: SCUFF PLATE. CORRODED. SERVICE DOOR SCUFF PLATE FASTENER HOLE 4OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M) SUMMARY SEE NR FOR ADDITIONAL INFORMATION 059-0001:5331-012
- [SDR DALA2024121111656](https://openairdocs.org/sdr/DALA2024121111656), Dec 8, 2024: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION @ STA 22 RBL 23 (P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0559:5321-2021/
- [SDR DALA2024121011574](https://openairdocs.org/sdr/DALA2024121011574), Dec 7, 2024: FLOOR PANEL. CORRODED. FWD CABIN FLOOR FWD PASSENGER ENTRY DOOR FR19 FWD INBD CORNER CORRODED.-M-PIC SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0560:5321-2022/001 00448 CMOR: REMOV
- [SDR DALA2024121011573](https://openairdocs.org/sdr/DALA2024121011573), Dec 3, 2024: SCUFF PLATE. CORRODED. FORWARD CARGO DOOR UPPER SCUFF PLATE FASTENER HOLE 6OU HAS CORROSION AROUND THE SURROUNDING AREA. (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SE
- [SDR DALA2024120311422](https://openairdocs.org/sdr/DALA2024120311422), Nov 27, 2024: DRAIN MAST. CORRODED. CORROSION FOUND ON FUSELAGE AT MATING SURFACE OF AFT HEATED DRAIN MAST. CEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001
- [SDR DALA2024120311421](https://openairdocs.org/sdr/DALA2024120311421), Nov 26, 2024: MECHANISM. INOPERATIVE. DURING TESTING FOUND LH OVERWING SLIDE DEPLOYMENT MODE SELECT MECHANISM IS NOT OPERATING CORRECTLY IN THE ARMED POSITION. SCEPTRE LOG PAGE ENTERED FOR SDR REPOR
- [SDR DALA2024112511190](https://openairdocs.org/sdr/DALA2024112511190), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 9OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY
- [SDR DALA2024112511188](https://openairdocs.org/sdr/DALA2024112511188), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 10OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M) W SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMA
- [SDR DALA2024112511187](https://openairdocs.org/sdr/DALA2024112511187), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 8OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMAR
- [SDR DALA2024112511186](https://openairdocs.org/sdr/DALA2024112511186), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 4OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMAR
- [SDR DALA2024112511185](https://openairdocs.org/sdr/DALA2024112511185), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 3OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMAR
- [SDR DALA2024112511184](https://openairdocs.org/sdr/DALA2024112511184), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 2OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMAR
- [SDR DALA2024112511183](https://openairdocs.org/sdr/DALA2024112511183), Nov 21, 2024: SCUFF PLATE. CORRODED. AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 11OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMAR
- [SDR DALA2024111110822](https://openairdocs.org/sdr/DALA2024111110822), Nov 8, 2024: SEAT TRACK. CORRODED. FWD FUSELAGE SEAT TRACK CORROSION @ STA 22 RBL 43.5 (P). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0559:5321-2021/001 00402 REMOVED AND REPLACED SEAT TRACK 
- [SDR DALA2024111110821](https://openairdocs.org/sdr/DALA2024111110821), Nov 8, 2024: SEAT TRACK. CORRODED. RIGHT OUTBOARD AFT END OF SEAT TRACK (UNDER AFT RIGHT LAV) HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND PITTING ON TOP SURFACE OF
- [SDR DALA2024111110820](https://openairdocs.org/sdr/DALA2024111110820), Nov 8, 2024: SEAT TRACK. CORRODED. RIGHT INBOARD AFT END OF SEAT TRACK (UNDER AFT RIGHT LAV) HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION ON TOP SURFACE OF SEAT TRACK F
- [SDR DALA2024111110818](https://openairdocs.org/sdr/DALA2024111110818), Nov 8, 2024: SEAT TRACK. CORRODED. RIGHT OUTBOARD AFT END OF SEAT TRACK HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND ON TOP SURFACE AND PITTING OF SEAT TRACK @ FRAM
- [SDR DALA2024110110583](https://openairdocs.org/sdr/DALA2024110110583), Oct 29, 2024: SLAT TRACK. NO DISCREPANCY. RIGHT WING SLAT TRACK 6 REQUIRES NDT TO BLENDED AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 184-0001:5742-01028-
- [SDR DALA2024110110581](https://openairdocs.org/sdr/DALA2024110110581), Oct 29, 2024: SLAT TRACK. NO DISCREPANCY. RIGHT WING SLAT TRACK 9 REQUIRES NDT TO BLENDED AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 184-0001:5742-01028-
- [SDR DALA2024110110580](https://openairdocs.org/sdr/DALA2024110110580), Oct 29, 2024: SLAT TRACK. NO DISCREPANCY. RIGHT WING SLAT TRACK 4 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED F
- [SDR DALA2024110110579](https://openairdocs.org/sdr/DALA2024110110579), Oct 29, 2024: SLAT TRACK. NO DISCREPANCY. RIGHT WING SLAT TRACK 3 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED F
- [SDR DALA2024110110578](https://openairdocs.org/sdr/DALA2024110110578), Oct 29, 2024: SLAT TRACK. NO DISCREPANCY. SLAT TRACK 2 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED FINDINGS ON 
- [SDR DALA2024061106015](https://openairdocs.org/sdr/DALA2024061106015), Jun 6, 2024: SLAT TRACK. WORN. RH SLAT TRACK NBR 5 UPPER AFT I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER AFT I/B SIDE IAW ER/A 60
- [SDR DALA2024061106014](https://openairdocs.org/sdr/DALA2024061106014), Jun 6, 2024: SLAT TRACK. WORN. RH SLAT TRACK NBR 5 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER FWD O/B SIDE IAW ERA 608
- [SDR DALA2024061106013](https://openairdocs.org/sdr/DALA2024061106013), Jun 6, 2024: SLAT TRACK. WORN. RH SLAT TRACK NBR 5 LOWER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER FWD I/B SIDE IAW ER/A 60
- [SDR DALA2024061106012](https://openairdocs.org/sdr/DALA2024061106012), Jun 6, 2024: SLAT TRACK. WORN. R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 6082
- [SDR DALA2024061106011](https://openairdocs.org/sdr/DALA2024061106011), Jun 6, 2024: SLAT TRACK. WORN. R/H SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF WEAR IN TWO LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED R/H SLAT TRACK NBR 11 LOWER AFT S
- [SDR DALA2024061106010](https://openairdocs.org/sdr/DALA2024061106010), Jun 6, 2024: SLAT TRACK. WORN. R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED R/H SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 608
- [SDR DALA2024061106009](https://openairdocs.org/sdr/DALA2024061106009), Jun 6, 2024: SLAT TRACK. CRACKED. CLOSING PLATES, SLAT NO.2 TRACK NO.4 CRACKED. REPLACED CLOSING PLATE, SLAT#2, TRACK#4, IAW A220 AMP BD500- A-J57-42-39-02AAA-720A-A. UP TO STEP#2 STANDING BY FO
- [SDR DALA2024061106008](https://openairdocs.org/sdr/DALA2024061106008), Jun 6, 2024: SLAT TRACK. WORN. RH SLAT TRACK NBR 5 UPPER AFT O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER AFT O/B SIDE IAW ER/A 60
- [SDR DALA2024061106007](https://openairdocs.org/sdr/DALA2024061106007), Jun 6, 2024: SLAT TRACK. CORRODED. R/H SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/
- [SDR DALA2024061106006](https://openairdocs.org/sdr/DALA2024061106006), Jun 6, 2024: SLAT TRACK. CORRODED. R/H 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 DALA2024061106005](https://openairdocs.org/sdr/DALA2024061106005), Jun 6, 2024: SLAT TRACK. WORN. RH SLAT TRACK NBR 4 UPPER AFT O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. RH SLAT TRACK#4 REPLACED. REF NR 001 FOR CORRECTIVE ACTION.
- [SDR DALA2024061106004](https://openairdocs.org/sdr/DALA2024061106004), Jun 6, 2024: SLAT TRACK. WORN. R/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. RH SLAT TRACK #4 REPLACED. REF NR 001 FOR CORRECTIVE ACTION.
- [SDR DALA2024061106003](https://openairdocs.org/sdr/DALA2024061106003), Jun 6, 2024: SLAT TRACK. WORN. R/H SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. RH SLAT TRACK #4 REPLACED. REF NR001 FOR CORRECTIVE ACTION. 

All 82: https://openairdocs.org/aircraft/N102DU/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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