# Service difficulty reports: N105DU

A list on [N105DU](https://openairdocs.org/aircraft/N105DU.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DALA2026021701091](https://openairdocs.org/sdr/DALA2026021701091.md): Plug · leaking · Feb 14, 2026 · N105DU · Airbus BD5001A10 · Turbine Engine Reduction Gear
  > AIRCRAFT DIVERTED TO ORD DUE TO LT ENGINE LOSS OF OIL QTY WITH PRESSURE DEGRADING. INSTALLED NEW GEARBOX DRAIN PLUG AND NEW HELICOIL INSERT. (LP 7651170).
- [SDR DALA2025062504756](https://openairdocs.org/sdr/DALA2025062504756.md): Scuff Plate · corroded · Jun 21, 2025 · N105DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT SILL BEAM HAS CORROSION AROUND 3(EA) THRESHOLD SCUFF PLATE ATTACH FASTENER HOLES. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0500:5321-2015/001 00094 REPAIRED PER PRI ER/A 626500-14 REV 0
- [SDR DALA2025062504766](https://openairdocs.org/sdr/DALA2025062504766.md): Threshold · corroded · Jun 21, 2025 · N105DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > THE AFT PASSENGER DOOR THRESHOLD HAS CORROSION AROUND THE FORWARD SCUFF PLATE ATTACH FASTENER HOLE. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0527:5360-2023/002 00172 REPAIRED PER ER/A 626969-14 PRI REV. 0 AND FINAL ER/A 626969-14 REV. ORIGINAL SECTION 1 P
- [SDR DALA2025062404722](https://openairdocs.org/sdr/DALA2025062404722.md): Door · corroded · Jun 20, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Powerplant Attach Fittings
  > FORWARD LEDGE OF LAV SERVICE DOOR OPENING HAS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0519:5300-2019/002 00191 REPAIRED PER ER/A PRI 609317-14 REV 0, REV. 1, REV. 2, AND FINAL ER/A 609317 -1
- [SDR DALA2025100207161](https://openairdocs.org/sdr/DALA2025100207161.md): Skin · corroded · Jun 19, 2025 · N105DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION IN TWO AREAS ADJACENT TO THE FORWARD CARGO COMPARTMENT LOWER SCUFF PLATE ATTACH FASTENER HOLE 12OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 049-0001:5331-01297- 01C/003 00130 REPAIRED PER ER/A PRI 626491-14 REV. 0, REV. 1, REV. 2,
- [SDR DALA2025062404717](https://openairdocs.org/sdr/DALA2025062404717.md): Threshold · corroded · Jun 19, 2025 · N105DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT SERVICE DOOR THRESHOLD/ENTRY SILL HAS CORROSION AROUND FASTENER HOLE AT AFT I/B CORNER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0576:5300-2016/001 00358 REMOVED AND REPLACED ENTRY SILL PER A220 AMP 53-00-47. (LP# 1034435)
- [SDR DALA2025062404727](https://openairdocs.org/sdr/DALA2025062404727.md): Threshold · corroded · Jun 19, 2025 · N105DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT PASSENGER DOOR THRESHOLD/ENTRY SILL HAS CORROSION AT AFT I/B CORNER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0576:5300-2016/003 00360 REPLACED THRESHOLD PANEL REF. A220 AMP 53-00-47. (LP# 1034399)
- [SDR DALA2025100207160](https://openairdocs.org/sdr/DALA2025100207160.md): Skin · corroded · Jun 14, 2025 · N105DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION ADJACENT TO THE FORWARD PASSENGER DOOR SCUFF PLATE ATTACH FASTENER HOLE 8OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 050-0001:5331-01297- 01A/001 00140 REPAIRED REF PRI 626486-14 REV 0, REV 1, REV 2 AND COMPLIED WITH ER/A 626486-1
- [SDR DALA2025061804587](https://openairdocs.org/sdr/DALA2025061804587.md): Skin · dented · Jun 14, 2025 · N105DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > DENT FOUND ON UPPER FUSELAGE SKIN JUST AFT OF FR 53, AND JUST OUTBOARD OF STRINGER L3. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0568:5350-2009/002 00381 REPAIRED PER PRI 626580-14 REV 0, 1, 2. SCEPTRE LOG PAGE E
- [SDR DALA2025061704570](https://openairdocs.org/sdr/DALA2025061704570.md): Seat Track · corroded · Jun 13, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 RBL 43.5. SSI: 53-21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0562:5321-2021/002 00320 REMOVED AND REPLACED SEAT TRACK RBL43.5 FRAME 19.5-30.5 REF ASRP 51-
- [SDR DALA2025100207159](https://openairdocs.org/sdr/DALA2025100207159.md): Skin · corroded · Jun 11, 2025 · N105DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION AT THE FORWARD SERVICE SCUFF PLATE ATTACH FASTENER HOLE 15OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 020-0001:5331-01297- 01B/001 00134 COMPLY WITH PRI 626480-14 REV 0, 1 AND ERA 626480-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIO
- [SDR DALA2025061004419](https://openairdocs.org/sdr/DALA2025061004419.md): Bearing · gouged · Jun 7, 2025 · N105DU · Airbus BD5001A10 · Main Landing Gear Strut/Axle/Truck
  > R/H MLG ASSEMBLY, AFT SPHERICAL BEARING GOUGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 211-0002:3210-4001-RH/001 00496 REMOVED AND REPLACED SPHERICAL BEARING REF A220 AMP 32-11-03. RH MLG ASSEMBLY INSTALLATION AND
- [SDR DALA2025061004418](https://openairdocs.org/sdr/DALA2025061004418.md): Seat Track · corroded · Jun 6, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 22. SSI: 53- 61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0562:5321-2021/007 00326 SPLICED SEAT TRACK PE
- [SDR DALA2025060204205](https://openairdocs.org/sdr/DALA2025060204205.md): Seat Track · corroded · Jun 1, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8105, AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 43.5. SSI: 53-61-43-01. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A220 ASRP 51-77-00. (LP 0999871)
- [SDR DALA2025053004149](https://openairdocs.org/sdr/DALA2025053004149.md): Threshold · corroded · May 29, 2025 · N105DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8105, FWD SERVICE DOOR THRESHOLD, AFT I/B CORNER AND EDGE HAVE CORROSION. CORRECTIVE ACTION: REPLACED THRESHOLD PANEL REF. A220 AMP 53-00-47. (LP 0993886)
- [SDR DALA2025052704043](https://openairdocs.org/sdr/DALA2025052704043.md): Seat Track · corroded · May 25, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 RBL 22. SSI:53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. BLENDED AND CHECKED LIMITS PER A220 ASRP 53-21-49-00-661. BLENDS OUT OF LIMITS. REPLACED PER A220 ASRP 51-77-00 AND A220 DWG C02312600. (
- [SDR DALA2025052704050](https://openairdocs.org/sdr/DALA2025052704050.md): Seat Track · corroded · May 23, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 22 LBL 43.5. SSI: 53-21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0562:5321-2021/004 00323 REPLACED SEAT TRACK REF A220 ASRP 51-77-00. SUMMARY SEE NR FOR AD
- [SDR DALA2025052704049](https://openairdocs.org/sdr/DALA2025052704049.md): Seat Track · corroded · May 23, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 43.5. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. ( M) (P). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0562:5321-2021/008 00327. REPLACED SEAT TRACK REF A220 ASRP 51-77-00. SUMMARY S
- [SDR DALA2025052704048](https://openairdocs.org/sdr/DALA2025052704048.md): Seat Track · corroded · May 23, 2025 · N105DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 22. SSI: 53- 61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0562:5321-2021/006 00325 REPLACED SEAT TRACK REF A220 ASRP 51-77-00. SUMMARY SEE NR FOR AD
- [SDR DALA2025051403745](https://openairdocs.org/sdr/DALA2025051403745.md): Light · not reported · May 10, 2025 · N105DU · Airbus BD5001A10 · Emergency Lighting
  > L/H REAR BARREL EXTERNAL EMERGENCY LIGHT INOP. REMOVED AND INSTALLED SERVICEABLE L/H REAR EXTERNAL EMERGENCY LIGHT PER A220 AMP 33-55-02, OPS TEST GOOD. (LP# 4323881)
- [SDR DALA2023091807656](https://openairdocs.org/sdr/DALA2023091807656.md): Unknown · unknown · Sep 16, 2023 · N105DU · Bombdr BD1001A10 · Landing Gear Brake System
  > SHIP 8105 - MISC/DE - DUE TO "BRAKE ON" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED ELECTRICAL MOTOR CONTROL UNIT (EMCU) #4. (LP# 4492648)
- [SDR DALA2023091807653](https://openairdocs.org/sdr/DALA2023091807653.md): Unknown · unknown · Sep 12, 2023 · N105DU · Bombdr BD1001A10 · Extinguishing System
  > SHIP 8105 - DIV - TO MKE DUE TO "CARGO BTL FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: CARGO BOTTLE PLACED ON MEL; R/R HRD FIRE BOTTLE. (LP# 4492632)
- [SDR DALA2023080806471](https://openairdocs.org/sdr/DALA2023080806471.md): Unknown · unknown · Aug 3, 2023 · N105DU · Bombdr BD1001A10 · Leading Edge Devices
  > LEFT WING #2 SLAT TRACK HAS CORROSION ON LOWER SURFACE AFT ROLLER AREA. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 004-0001:5742-01028-02A/002 00004 ACCOMPLISHED ER/A 608177-14AD REV A
- [SDR DALA2023080806470](https://openairdocs.org/sdr/DALA2023080806470.md): Unknown · unknown · Aug 3, 2023 · N105DU · Bombdr BD1001A10 · Leading Edge Devices
  > LEFT WING #1 SLAT TRACK HAS CORROSION ON LOWER SURFACE AFT ROLLER AREA. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 004-0001:5742-01028-02A/001 00003 ACCOMPLISHED ER/A 608177-14AD REV A
- [SDR DALA2023060704631](https://openairdocs.org/sdr/DALA2023060704631.md): Unknown · unknown · Jun 6, 2023 · N105DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON WASTE BOX DOOR MOUNTING SURFACE RH SIDE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 069-0001:3832-01114-01/001 00005 ACCOMPLISHED ALL WORK PER ER/A 609317-14 PRI REV. 0, ER/A 609317 -14 PRI REV. 01,
- [SDR DALA2023020300861](https://openairdocs.org/sdr/DALA2023020300861.md): Not Entered · not entered · Jan 31, 2023 · N105DU · Bombdr BD1001A10 · Passenger Compartment Windows
  > SHIP 8105 - DIV - DUE TO SUSPECTED CRACK IN WINDOW AT SEAT 20A. CORRECTIVE ACTION: MAINTENANCE INSPECTED WINDOW AND REPORTED NO TROUBLE FOUND. FLIGHT CONTINUED ON TO SLC. (LP# 9851122)
- [SDR DALA2022042803007](https://openairdocs.org/sdr/DALA2022042803007.md): A/C Pack · overheated · Apr 25, 2022 · N105DU · Bombdr BD1001A10 · Cabin Cooling System
  > ON DESCENT, THROUGH 180, AFTER TURN COWL-ANTI ICE OFF WITH ENGINES AT IDLE-BURNING OIL SCENT IN THE COCKPIT. ENGINE OFF IDLE SCENT WENT AWAY. ON TAXI IN AFTER SHUTTING DOWN R ENG SCENT ALSO WENT AWAY. F/A DID NOT REPORT ANY UNUSUAL ODORS IN THE CABIN. LT PACK
- [SDR DALA2022020400722](https://openairdocs.org/sdr/DALA2022020400722.md): None · none · Jan 28, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STAB #3 RIB ELEVATOR HINGE CRACKED. ADDITIONAL INFORMATION 001-0293:2090-2039-RH/001 00148 ACCOMPLISHED PRI 596551-14, REV. 0; 596551-14, REV. 1; 596551-14, REV. 1.1; 596551-14, REV. 2; 596551-14, REV. 3 AND ERA 596551- 14, REV. ORIGINAL. ASSOC
- [SDR DALA2022020400721](https://openairdocs.org/sdr/DALA2022020400721.md): None · none · Jan 28, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > #2 HORIZONTAL STAB ELEVATOR RIB HINGE IS CRACKED. ADDITIONAL INFORMATION 001-0293:2090-2039-RH/002 00152 ACCOMPLISHED PRI 596562-14, REV. 0; 596562-14, REV. 1; 596562-14, REV. 2 AND ERA 596562-14, REV. ORIGINAL. (LP# 2102394)
- [SDR DALA2022020400720](https://openairdocs.org/sdr/DALA2022020400720.md): None · none · Jan 28, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STABILIZER #2 RIB ELEVATOR HINGE CRACKED. ADDITIONAL INFORMATION 001-0291:2090-2039-LH/001 00147 ACCOMPLISHED PRI 596563-14, REV. 0; 596563-14, REV. 1 AND ERA 596563-14, REV. ORIGINAL. (LP# 2102249)
- [SDR DALA2022012800579](https://openairdocs.org/sdr/DALA2022012800579.md): None · none · Jan 26, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > ON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 4 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 007 00239 COMPLETED INSTALL OF REPAIR PER A220 ASRP 51-71-59. (LP# 2099959)
- [SDR DALA2022012800578](https://openairdocs.org/sdr/DALA2022012800578.md): None · none · Jan 26, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > ON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 2 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 006 00238 COMPLETED INSTALL OF REPAIR PER A220 ASRP 51-71-59. (LP# 2099956)
- [SDR DALA2022012800580](https://openairdocs.org/sdr/DALA2022012800580.md): None · none · Jan 24, 2022 · N105DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > ER/A 596551-14 SECTION I ACCOMPLISHED FOR REPAIR OF THE RH HORIZONTAL STABILIZER, TRAILING EDGE, HINGE RIB #3. THE REPAIR WAS ACCOMPLISHED DURING 'C' CHECK IN MSP, NR # 148. ANALYSIS (DTA). ADDITIONAL ENGINEERING APPROVAL, ER/A REVISION, IS REQUIRED FOR CONTIN
- [SDR DALA2021112307195](https://openairdocs.org/sdr/DALA2021112307195.md): Blades · contaminated · Nov 21, 2021 · N105DU · Bombdr BD1001A10 · Engine (Turbine/Turboprop)
  > DIRTY/MUSTY SMELL ON T.O. AND CLIMB IN COCKPIT AND AFT CABIN, SMELL CAME BACK ON DSCT FROM 15,000 TILL GATE ARRIVAL. OPENED #1 ENGINE FOR BORO, REMOVED BORO PLUGS LPC-2, HPC-1, HPC- 2, TIC, LPC-3, LPT-1, LPT-2 AND N1 SPEED PROBE. REF: AMP TASK BD500-A-J29-00-0
- [SDR DALA2021112307197](https://openairdocs.org/sdr/DALA2021112307197.md): Engine · odor · Nov 17, 2021 · N105DU · Bombdr BD1001A10 · Air Conditioning System
  > ONCE AIRBORNE AFTER T/O A/C HAD A MUST SOCK SMELL. IT WAS NOTICEABLE NOT STRONG. ODOR STARTED TO FADE ONCE POWER WAS REDUCED TO CLIMB POWER. SLIGHT SMELL AFTER LANDING. BEGAN WORKING WC# 0550-2001 TO ISOLATE SMOKE FUMES. RH ENGINE GENERATES SMELL IN CABIN AT H
- [SDR DALA2021082404997](https://openairdocs.org/sdr/DALA2021082404997.md): Reu · failed · Aug 23, 2021 · N105DU · Bombdr BD1001A10 · Rudder Control System
  > SHIP 8105 - DIV - TO PDX DUE TO FLIGHT CONTROL FAULT/ REU INTERNAL MESSAGE AND FOLLOWED BY RUDDER FAIL MESSAGE. CORRECTIVE ACTION: REPLACED AFT REU-1. (LP# 7998164)
- [SDR DALA2020061802472](https://openairdocs.org/sdr/DALA2020061802472.md): Computer · malfunctioned · Jun 17, 2020 · N105DU · Bombdr BD1001A10 · Central Computers
  > SHIP 8105 - ATB/DE - DUE TO NUMEROUS FAULT WARNINGS ASSOCIATED WITH FAILURE OF THE DCM IN CONTROL TO INCLUDE EMERG DESCENT ANNUNCIATED. CORRECTIVE ACTION: TROUBLESHOOTING INDICATED DCM 2A AT FAULT. CARD REPLACED, FDR AND NVM DATA PROVIDED TO ABC FOR FINAL DETE
- [SDR DALA2019061103510](https://openairdocs.org/sdr/DALA2019061103510.md): Sign · missing · Jun 8, 2019 · N105DU · Bombdr BD1001A10 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT SIGN MISSING. REPLACED LT OVERWING EXIT SIGN LENS REF A220 AMP 33-54-01. OK FOR SERVICE. (LP# 5707337)
- [SDR DALA2019042202545](https://openairdocs.org/sdr/DALA2019042202545.md): None · none · Apr 15, 2019 · N105DU · Bombdr BD1001A10 · Communications System
  > ACCOMPLISH ER/A 577289-14 TO INSTALL NEW CMS SOFTWARE. (REF. SERVICE BULLETIN BD500-441007 ISSUE NO. 1 AND SERVICE BULLETIN RDAK5151014-44-1S). (LP# 1031395)

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N105DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N105DU/reports

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