# Service difficulty reports: N101DU

A list on [N101DU](https://openairdocs.org/aircraft/N101DU.md).

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

- [SDR DALA2026090104933](https://openairdocs.org/sdr/DALA2026090104933.md): Control Unit · faulty · Aug 30, 2026 · N101DU · Airbus BD5001A10 · AC Power Distribution System
  > DECLARED EMERGENCY DUE TO 24 ELECTRICAL FAULT - BPCU INOP WITH ASSOCIATED FLAP AND SLAT REDUNDANT LOSS AT CRUISE. REPLACED NR 1 BUS POWER CONTROL UNIT (BPCU). (LP# 8621390)
- [SDR DALA2025011400323](https://openairdocs.org/sdr/DALA2025011400323.md): Valve · leaking · Jan 13, 2025 · N101DU · Airbus BD5001A10 · Waste Disposal System
  > WASTE BALL VALVE LEAKING. REMOVED AND REPLACED WASTE BALL VALVE REF TO A220 AMP 38-31-03. COMPLIED WITH PRI 595069-14 REV 0, REV 01, REV 02, REV 03, AND FINAL ER/A 595069-14AD REV. B. (LP# 0758506)
- [SDR DALA2024102110276](https://openairdocs.org/sdr/DALA2024102110276.md): Light · inoperative · Oct 18, 2024 · N101DU · Airbus BD5001A10 · Emergency Lighting
  > FLIGHT CREW REPORTED EMERGENCY LIGHTS INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AS PER A220 AMP 33-51, OPS CHECK OK. (LP# 6419512)
- [SDR DALA2024100209612](https://openairdocs.org/sdr/DALA2024100209612.md): Warning Message · false activation · Sep 30, 2024 · N101DU · Airbus BD5001A10 · Central Warning
  > SHIP 8101 - ATO - DUE TO "CONFIG RUDDER TRIM" WARNING MESSAGE. CORRECTIVE ACTION: PERFORMED OPERATIONAL AND FUNCTIONAL TEST OF TAKE-OFF CONFIGURATION. (LP# 5812152)
- [SDR DALA2024082908532](https://openairdocs.org/sdr/DALA2024082908532.md): Light · inoperative · Aug 28, 2024 · N101DU · Airbus BD5001A10 · Emergency Lighting
  > 2 OVER WING EMERGENCY EXT LIGHTS INOP. REMOVED AND REPLACED LT FWD AND AFT AND RT FWD OVERWING EMERGENCY LIGHTS PER A220 AMP 33-55. OPS NORMAL. (LP# 6201547)
- [SDR DALA2024040404064](https://openairdocs.org/sdr/DALA2024040404064.md): Skin · cracked · Apr 2, 2024 · N101DU · Airbus BD5001A10 · Wing, Plate/Skin
  > RH WING LEADING EDGE CRACKED AT SLAT TRACK #7 CUT OUT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0684:2021-2065-RH/003 00095 ER/A 616956-14 PRI REV 0 AND FINAL ER/A 616956-14 REV ORIGINAL HAVE BEEN COMPLIED WITH.
- [SDR DALA2024040204034](https://openairdocs.org/sdr/DALA2024040204034.md): Block · broken · Mar 30, 2024 · N101DU · Airbus BD5001A10 · Escape Slide
  > RH OWEED FWD PIVOT BLOCK IS BROKEN AND UNABLE TO BE REPAIRED. REMOVED AND REPLACED RH OWEED SLIDE REF. A220 AMP 25-63-02. SLIDE, PACK, OW OFF 81-2563-9-0008 28045 ON 81-2563-9-0008 28157. (LP# 0268788)
- [SDR DALA2024040204033](https://openairdocs.org/sdr/DALA2024040204033.md): Floor Support · cracked · Mar 28, 2024 · N101DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT: FLOOR SUPPORT BEAM CRACKED AT OTBD END. 5 " AFT OF FR 64. (AFT OF DOOR HINGE). REPAIRED REF PRI 616272-14 REV 0, REV 1 AND ER/A 616272-14 REV O SECTION I. (LP# 0266718)
- [SDR DALA2024032803892](https://openairdocs.org/sdr/DALA2024032803892.md): Floorbeam · cracked · Mar 27, 2024 · N101DU · Airbus BD5001A10 · Fuselage Main, Floor Beam
  > AFT CARGO DOOR CUTOUT: FLOOR SUPPORT BEAM CRACKED AT OTBD END. 5 " FWD OF FR 63. (FWD OF DOOR HINGE). ATA 5311 RII: Y ENTR 00284754 W SUMMARY OF NR#416:ACCOMPLISHED INTER COSTAL REPAIR PER PRI 616270 -14 REV 0 AND REV 1 AND VERIFIED WORK ACCOMPLISHED AND RECOR
- [SDR DALA2024032803891](https://openairdocs.org/sdr/DALA2024032803891.md): Door Frame · corroded · Mar 27, 2024 · N101DU · Airbus BD5001A10 · Fuselage Main, Structure
  > L1 DOOR FR20 FACING FWD FOUND 8 EACH FASTENERS HOLES CORROSION THROUGH NUT-PLATE. REPAIRED PER PRI 616196-14 REV 0, REV 1, REV 2, REV 3, AND ER/A 616196-14 REV O SECTION I. (LP# 0264773)
- [SDR DALA2024032703851](https://openairdocs.org/sdr/DALA2024032703851.md): Skin · cracked · Mar 22, 2024 · N101DU · Airbus BD5001A10 · Wing, Plate/Skin
  > LH LEADING EDGE CUT OUT FOR SLAT TRACK #7 HAS CRACK. REPAIRED CRACK PER PRI 615984-14 REV 0, REV 01, REV 02 AND FINAL ERA 615984-14 REV ORIGINAL.
- [SDR DALA2024032603830](https://openairdocs.org/sdr/DALA2024032603830.md): Roller · worn · Mar 20, 2024 · N101DU · Airbus BD5001A10 · Leading Edge Devices
  > LH WING, #4 SLAT TRACK HAS HEAVY ROLLER WEAR. FWD, UPPER SURFACE. -M- LOG-PAGE UPDATED @ 20MAR24 1416 UTC 02 CORR BY SACHS 00583347 MSP 20MAR24 ATA 5742 RII: N ENTR 00260220 W SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATI
- [SDR DALA2024031203252](https://openairdocs.org/sdr/DALA2024031203252.md): Seat Track · corroded · Mar 11, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD GALLEY: CORROSION IN FLOOR FITTING FR 22 RBL 43. -M-PIC. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:2530-2001/003 00318 REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0239795)
- [SDR DALA2024031203251](https://openairdocs.org/sdr/DALA2024031203251.md): Seat Track · corroded · Mar 11, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD GALLEY: CORROSION IN FLOOR FITTING FR 22 RBL 43. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0240295)
- [SDR DALA2024031203248](https://openairdocs.org/sdr/DALA2024031203248.md): Seat Track · corroded · Mar 9, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 RBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. (LP# 0236714)
- [SDR DALA2024031203247](https://openairdocs.org/sdr/DALA2024031203247.md): Seat Track · corroded · Mar 9, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-00, CIC ACCOMPLISHED ON AMDS 5341-2017. (LP# 0236483)
- [SDR DALA2024031203246](https://openairdocs.org/sdr/DALA2024031203246.md): Seat Track · corroded · Mar 9, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. (LP# 0236475)
- [SDR DALA2024031203249](https://openairdocs.org/sdr/DALA2024031203249.md): Seat Track · corroded · Mar 8, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. -M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:2530-2001/004 00319 REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. (LP# 0236114)
- [SDR DALA2024031203245](https://openairdocs.org/sdr/DALA2024031203245.md): Seat Track · corroded · Mar 8, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LAV FLOOR: CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 43. REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11.(LP# 0236202)
- [SDR DALA2025102107691](https://openairdocs.org/sdr/DALA2025102107691.md): Seat Track · corroded · Mar 7, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 RBL 23. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0234433)
- [SDR DALA2025102107690](https://openairdocs.org/sdr/DALA2025102107690.md): Seat Track · corroded · Mar 7, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN FLOOR FITTING/SEAT TRACK AT FR74 LBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-06 AND DWG C01303000. (LP# 0234426)
- [SDR DALA2025102107689](https://openairdocs.org/sdr/DALA2025102107689.md): Seat Track · corroded · Mar 7, 2024 · N101DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD GALLEY: CORROSION IN FLOOR FITTING AT FR22 RBL 23. REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-42-20. (LP# 0234366)
- [SDR DALA2024030603066](https://openairdocs.org/sdr/DALA2024030603066.md): Threshold · corroded · Mar 3, 2024 · N101DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR: SERVICE ENTRY DOOR THRESHOLD CORRODED AT FWD INBD CORNER FR 17. THRESHOLD REMOVED AND REPLACED PER A220 ASRP 51-41-02. CORROSION LEVEL 2,
- [SDR DALA2024030503039](https://openairdocs.org/sdr/DALA2024030503039.md): Pump · gouged · Mar 1, 2024 · N101DU · Airbus BD5001A10 · Fuel Boost Pump
  > LH WING FUEL SYSTEM - EJECTOR PUMP ASSEMBLY HAS CHAFING AND GOUGING AT COUPLING FLANGE. REF. AMDS 2820-01281-07A, ITEM 12. SEE PIC. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:2820-01281-07A/008 00531 REPLACED
- [SDR DALA2024020101476](https://openairdocs.org/sdr/DALA2024020101476.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 10 LOWER AFT SURFACE PER ER/A 608469 -14AD REV C AND PRI REV
- [SDR DALA2024020101475](https://openairdocs.org/sdr/DALA2024020101475.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 1 LOWER AFT SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101474](https://openairdocs.org/sdr/DALA2024020101474.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H 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 FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 1 UPPER FWD SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101473](https://openairdocs.org/sdr/DALA2024020101473.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H 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 FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 1 UPPER FWD SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101472](https://openairdocs.org/sdr/DALA2024020101472.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 6 UPPER AFT SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101471](https://openairdocs.org/sdr/DALA2024020101471.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 2 UPPER AFT SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101470](https://openairdocs.org/sdr/DALA2024020101470.md): Slat Track · corroded · Jan 30, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H 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 FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 4 UPPER AFT SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101469](https://openairdocs.org/sdr/DALA2024020101469.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 5 UPPER FWD SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101468](https://openairdocs.org/sdr/DALA2024020101468.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK NBR 5 UPPER AFT SURFACE PER ER/A 608469- 14AD REV C AND PRI REV 0
- [SDR DALA2024020101467](https://openairdocs.org/sdr/DALA2024020101467.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF5742-010128-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE PER ERA 608468- 14AD AND PRI REV.0 ASSOCIATE
- [SDR DALA2024020101466](https://openairdocs.org/sdr/DALA2024020101466.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE PER ERA 608468- 14AD REV.B AND PRI REV.0 MAT
- [SDR DALA2024020101465](https://openairdocs.org/sdr/DALA2024020101465.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 3 UPPER AFT SURFACE PER ERA 608468- 14AD REV.B PRI REV 0 MATCHE
- [SDR DALA2024020101464](https://openairdocs.org/sdr/DALA2024020101464.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01018-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 5 LOWER AFT SURFACE PER ERA 608468- 14AD REV.B AND PRI REV.0 MAT
- [SDR DALA2024020101463](https://openairdocs.org/sdr/DALA2024020101463.md): Slat Track · corroded · Jan 29, 2024 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE PER ERA 608468- 14AD REV.B AND PRI REV. 0 AS
- [SDR DALA2023090807368](https://openairdocs.org/sdr/DALA2023090807368.md): Unknown · unknown · Sep 3, 2023 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS CARD 5742-01028-02A- LH WING SLAT TRACK #7 HAS CORROSION ON UPPER AFT AND LOWER AFT SURFACES WITH PREVIOUS REWORK. CEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 048-0001:5742-01028-02A/007 00009 REPAIRED PER PRI
- [SDR DALA2023050503526](https://openairdocs.org/sdr/DALA2023050503526.md): Unknown · unknown · May 1, 2023 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 608468-14AD SECTION I ISSUED FOR CORROSION TO LH SLAT TRACKS. ACCOMPLISHED ERA 608468-14AD REV ORIGINAL SECTION 1. (LP# 2747021)
- [SDR DALA2023050503525](https://openairdocs.org/sdr/DALA2023050503525.md): Unknown · unknown · May 1, 2023 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 608469-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VIS IT. FOLLOW ON ACTION IS REQUIRED. THIS AFFECTS RH WING SLAT TRAC KS 4-9. ACCOMPLISHED ER/A 608469-14AD REV. ORIGINAL SECTION 1. (LP# 2747030)
- [SDR DALA2023032102110](https://openairdocs.org/sdr/DALA2023032102110.md): Unknown · unknown · Mar 17, 2023 · N101DU · Bombdr BD1001A10 · Air Conditioning System
  > AFTER STARTING ENG #2, FA REPORTED BURNING SMELL AND THIN SMOKE IN MID AND FWD CABIN. SMELL AND SMOKE DISSIPATED AFTER SHUTTING DOWN. THE ENGINE. EXPERIENCED SIGNIFICANT WIND SHIFT DURING ENGINE START FROM R-QTR HW TO R-QTR TW. C/W WITH AMDS WORK CARD 0550-200
- [SDR DALA2023013000751](https://openairdocs.org/sdr/DALA2023013000751.md): Oil System · overserviced · Jan 26, 2023 · N101DU · Bombdr BD1001A10 · APU Oil System
  > DURING AND JUST AFTER TOUCHDOWN ALL CABIN FA'S REPORTED ELECTRICAL ODOR AND MINOR HAZE OVER COMFORT PLUS SEATS. ODOR AND HAZE DISSIPATED AFTER AIRCRAFT WAS PARKED. C/W NO GO ODI STEP 1, ISOLATED SOURCE PER J/C 0550-2001. FOUND APU OIL OVERSERVICED. PERFORMED S
- [SDR DALA2022060904028](https://openairdocs.org/sdr/DALA2022060904028.md): None · none · Nov 2, 2021 · N101DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/Rib
  > ERA 594987-14 SECTION I ACCOMPLISHED DURING CCK IN MSP NOV2021. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 594987-14 SECTION II REPEAT INSPECTION EVERY 850 FH AFTER SECTION I UNTIL 8500 FH AFTER SECTION I. THE 8500 FH RE STRCTION IS TRACKED PER ERA SECTION I
- [SDR DALA2025011400326](https://openairdocs.org/sdr/DALA2025011400326.md): None · none · Oct 27, 2021 · N101DU · Airbus BD5001A10 · Standard Practices/Structures
  > **AD RELATED** - LOWER AFT FUSELAGE / WASTE WATER SURROUND STRUCTURE / FR75-76 / CORROSION. ERA 595069-14AD ISSUED AND IS CURRENT. FOLLOW ON ACTION REQUIRED SECT. ACCOMPLISHED @ C CHK VISIT MSP OCT2021. SECT. II TBA WITHIN 8500FH AFTER SECT. I. AD RELATED, NO
- [SDR DALA2022091606166](https://openairdocs.org/sdr/DALA2022091606166.md): None · none · Sep 28, 2021 · N101DU · Bombdr BD1001A10 · Leading Edge Devices
  > A220 LH WING NO. 3 SLAT (MPN C01612004-001 / MSN 50038) WAS IMPACTED BY A STAND CREATING A DENT ON THE TOP SKIN. THE SUBJECT NO. 3 SLAT HAS BEEN REPAIRED PER ER/A 593408-14 REV. ORIGINAL, SECTION I. FOLLOW ON ACTION IS REQUIRED. ER/A 593408-14 REV. ORIGINAL SE
- [SDR DALA2020080302688](https://openairdocs.org/sdr/DALA2020080302688.md): Warning Message · false activation · Aug 2, 2020 · N101DU · Bombdr BD1001A10 · Engine Fuel and Control
  > L ENG FUEL LO PRESS CAUTION MESSAGE INFLIGHT. RAN THROUGH QRH, AFTER 1 MINUTE MESSAGE DISSAPEARED. T/S PER A220 SOLUTION 2-33317, R/R LT ENG FEED PRESSURE SWITCH, ALL CK GOOD. INSPECTED WIRING TO SWITCH NO DEFECTS FOUND. RAN 3 TIMES NO FAULTS PRESENT. A/C OK
- [SDR DALA2020011600352](https://openairdocs.org/sdr/DALA2020011600352.md): Longeron · cracked · Jan 14, 2020 · N101DU · Airbus BD5001A10 · Aerodynamic Fairings
  > FOUND RT WTBF INTERNAL LONGERON ASSY P/N C02383111-002 CRACKED VERTICAL. REMOVED DAMAGED AREA PER ERA 583765-14 SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 584302-14 REV ORIG - REF LOG 1428537.
- [SDR DALA2020011600351](https://openairdocs.org/sdr/DALA2020011600351.md): Longeron · cracked · Jan 14, 2020 · N101DU · Airbus BD5001A10 · Aerodynamic Fairings
  > FOUND LT WTBF INTERNAL LONGERON ASSY P/N 602383111-001 CRACKED VERTICALLY. REMOVED DAMAGED AREA PER ERA 583765-14 RI SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 584302-14 REV ORIG - REF LOG 1428537.

## 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 = 'N101DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N101DU/reports

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