# Service difficulty reports: N304DU

A list on [N304DU](https://openairdocs.org/aircraft/N304DU.md).

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

Page 1 of 2 · 51 reports

- [SDR DALA2026082704869](https://openairdocs.org/sdr/DALA2026082704869.md): Filter · contaminated · Aug 25, 2026 · N304DU · Airbus BD5001A11 · Air Distribution System
  > DIRTY SOCK ODOR AT AND AFTER TOP OF DEAD, CLEARED AFTER A COUPLE MINS. PERFORMED ISOLATE SMOKE AND FUMES IN COCKPIT AND CABIN WC 0550- 2001. PERFORMED GVI OF ENG 1 AND ENG 2 WITH NTF IAW A220 AMP 72-00. PERFORMED GVI OF APU IAW AMP 49-10 WITH NTF EXTERNALLY (E
- [SDR DALA2026081104628](https://openairdocs.org/sdr/DALA2026081104628.md): Light · inoperative · Aug 10, 2026 · N304DU · Airbus BD5001A11 · Emergency Lighting
  > LEFT FWD FUSELAGE EMERGNECY EXIT LIGHT INOPERATIVE. REPLACED FWD FUSELAGE EMERGENCY EXIT LIGHT IAW AMP 33-55. (LP 9080912 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302989](https://openairdocs.org/sdr/DALA2026051302989.md): Skin · corroded · May 9, 2026 · N304DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT LAV SERVICE DOOR DURING DVI PER ER/A 612058-14 SECTION 2. COMPLIED WITH ER/A# 634152-14 REV-ORIGINAL ASSOCIATED ER/A 14-634152 ADDED FOR AC 8304. (LP# 1585400; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302988](https://openairdocs.org/sdr/DALA2026051302988.md): Skin · corroded · May 9, 2026 · N304DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT LAV SERVICE AREA DURING DVI PER ER/A 612058-14 SECTION 2. COMPLIED WITH ER/A# 634152-14 REV-ORIGINAL ASSOCIATED ER/A 14-634152 ADDED FOR AC 8304. (LP# 1585396; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051403014](https://openairdocs.org/sdr/DALA2026051403014.md): Doubler · corroded · May 6, 2026 · N304DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > ER/A 634152-14; A220-300 / REAR BARREL FUSELAGE WASTE BOX INTERNAL DOUBLER & SERVICE DOOR CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 634152-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 13,074 TOTAL AIRCRAFT FL
- [SDR DALA2026051102960](https://openairdocs.org/sdr/DALA2026051102960.md): Strap · corroded · May 5, 2026 · N304DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > STRUCTURE JUST FORWARD OF RT AFT SERVICE DOOR FLOOR PANEL 242MRF CORRODED AT FR74 OTBD OF RBL 43.5 WL151.5. R & R STRUCTURE (STRAP) FWD OF R/H AFT SERVICE DOOR AT FR 74 OB OF RBL 43.5 WL 151.5 PER A220 ASRP BD500-A-J51- 42-06-00AAA-078A-A AND BOMBARDIER DWG C
- [SDR DALA2026050402801](https://openairdocs.org/sdr/DALA2026050402801.md): Floor Support · corroded · May 1, 2026 · N304DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION AROUND FASTENER HOLE ON FLOORBOARD SUPPORT STRUCTURE R/H SIDE BETWEEN FR 76 AND FR78 APPROX RBL 37.5 SECOND FROM FORWARD FASTENER HOLE. REMOVED AND REPLACED FLOORBOARD SUPPORT STRUCTURE R/H SIDE BETWEEN FR76 AND FR78 APPROX RBL 37.5 I.A.W. A220 ASRP
- [SDR DALA2026050402799](https://openairdocs.org/sdr/DALA2026050402799.md): Floor Panel · corroded · Apr 30, 2026 · N304DU · Airbus BD5001A11 · Fuselage Floor Panel
  > FORWARD ENTRY FLOOR PANEL 221KLF HAS CORROSION ON I/B EDGE. REMOVED AND REPLACED FORWARD ENTRY FLOOR PANEL 221KLF IAW A220 AMP BD500-A-J53-00-47-11AAA-721A-A. (LP# 1570768; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050402798](https://openairdocs.org/sdr/DALA2026050402798.md): Seat Track · corroded · Apr 30, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FORWARD CABIN LEFT INBD SEAT TRACK CORROSION ON FORWARD END LBL 23 FR22 WL151.5. REMOVED AND REPLACED SEAT TRACK FROM FR 20 TO FR30 LBL 23 WL 151.5 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV K. (LP# 1570636; AIRC
- [SDR DALA2026043002751](https://openairdocs.org/sdr/DALA2026043002751.md): Floor Panel · corroded · Apr 29, 2026 · N304DU · Airbus BD5001A11 · Fuselage Floor Panel
  > FORWARD SERVICE FLOOR PANEL 222KRF HAS CORROSION ON AFT I/B CORNER. REMOVED AND REPLACED FWD SERVICE FLOOR PANEL 222KRF IAW A220 AMP BD500-A-J53-00-47-12AAA-720A-A. (LP# 1569041; AIRCRAFT GROUNDED)
- [SDR DALA2026043002750](https://openairdocs.org/sdr/DALA2026043002750.md): Floor Panel · corroded · Apr 27, 2026 · N304DU · Airbus BD5001A11 · Fuselage Floor Panel
  > R/H AFT SERVICE DOOR FLOOR PANEL 242MRF FORWARD EDGE CORRODED. REMOVED DAMAGED FLOOR PANEL 242 MRF FROM RH AFT SERVICE DOOR, AND INSTALLED NEW REPLACEMENT PANEL 242 MRF PART# C01342841-015S, LOT# 5194365-1, IAW-A220-AMP-BD500-A-J53-00-47-14AAA-720A-A & A220-A
- [SDR DALA2026043002749](https://openairdocs.org/sdr/DALA2026043002749.md): Seat Track · corroded · Apr 26, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > R/H I/B SEAT TRACK AFT END CORRODED AT FR 74 RBL 23 WL 151.5. REMOVED AND REPLACED SEAT TRACK R/H I/B, FROM FR60-FR74 RBL 23 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG PL C01342701 REV-G. (LP# 1563944; AIRCRAFT GROUNDED)
- [SDR DALA2026042802690](https://openairdocs.org/sdr/DALA2026042802690.md): Web · corroded · Apr 25, 2026 · N304DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION AROUND FASTENER HOLE ON SUPPORT STRUCTURE R/H SIDE AFT OF FR78 APPROX RBL 49 AFT OF GALLEY WATER LINE. REMOVED AND REPLACED WEB ON FR76 TO FR79, STRINGER 22R, IAW ASRP BD500- A-J51-42-20-00AAA-078A-A. & DWG C01342700 REV-T. (LP# 1562613)
- [SDR DALA2026042802689](https://openairdocs.org/sdr/DALA2026042802689.md): Seat Track · corroded · Apr 23, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 23 WL151.5. REMOVED AND REPLACED LT INBD SEAT TRACK FROM FR 74-FR 61 LBL 23 WL 151.5 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01342701 REV G.
- [SDR DALA2026042302609](https://openairdocs.org/sdr/DALA2026042302609.md): Seat Track · corroded · Apr 22, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 43.5 WL151.5. REMOVED AND REPLACED R/H O/B SEAT TRACK AFT END FR74 RBL 43.5 TO FR 61 RBL 43.5 PER DWG C01342701 REV -G AND A220 ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP# 1557507)
- [SDR DALA2026042302608](https://openairdocs.org/sdr/DALA2026042302608.md): Seat Track · corroded · Apr 20, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FORWARD END RBL 23 FR20 WL151.5. REMOVED AND REPLACED SEAT TRACK FROM FR20 TO FR 30 RBL 23 WL 151.5 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C02312600 REV J. (LP# 1554299)
- [SDR DALA2026042202575](https://openairdocs.org/sdr/DALA2026042202575.md): Floor Panel · corroded · Apr 19, 2026 · N304DU · Airbus BD5001A11 · Fuselage Floor Panel
  > CORROSION LH AFT ENTRY DOOR FLOOR PANEL 241MLF FORWARD EDGE CORRODED. REMOVED AND REPLACED DAMAGED AFT PASSENGER DOOR FLOOR PANEL 241 MLF IAW A220 AMP BD500-A-J53-00-47-13AAA-720A-A. (LP# 1552709)
- [SDR DALA2026042202574](https://openairdocs.org/sdr/DALA2026042202574.md): Seat Track · corroded · Apr 18, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FORWARD CABIN RIGHT O/B SEAT TRACK CORROSION ON FORWARD END RBL 43.5 FR20 WL151.5. REMOVED DAMAGED SEAT TRACK FROM PASSENGER CABIN BETWEEN FR 20 TO FR 30 RBL 43.5 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER PL C02312600 REV-E. (LP# 15
- [SDR DALA2026042002482](https://openairdocs.org/sdr/DALA2026042002482.md): Seat Track · corroded · Apr 17, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FORWARD CABIN LEFT O/B SEAT TRACK CORROSION ON FORWARD END LBL43.5 FR22 WL 151.5. REMOVED AND REPLACED FWD CABIN LEFT O/B SEAT TRACK AT LBL=43.5, FR19+19" TO FR=30+10" PER A220 ASRP BD500-A-J51-42-20-00AAA- 078A-A PAR.3A AND 5.E, DWG= BOMBARDIER PL C
- [SDR DALA2026042002479](https://openairdocs.org/sdr/DALA2026042002479.md): Seat Track · corroded · Apr 17, 2026 · N304DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OTBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 43.5 WL151.5. R & R THE SEAT TRACK FROM FR 61 TO FR 74 LBL 43.5 WL 151.5 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG #C01342701 REV G. (L/P# 1549371)
- [SDR DALA2026012700643](https://openairdocs.org/sdr/DALA2026012700643.md): Pump · faulted · Jan 25, 2026 · N304DU · Airbus BD5001A11 · Aircraft Fuel Distribution System
  > ATB, RETURNED TO IAH AND DECLARED AN EMERGENCY DUE TO FUEL IMBALANCE. R & R RT WING FUEL TANK EJECTOR PUMP. (LP# 8524602)
- [SDR DALA2025051403746](https://openairdocs.org/sdr/DALA2025051403746.md): Skin · damaged · May 8, 2025 · N304DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > DTE, ERA 603429-14 REV A. DAMAGE TOLERANCE EVALUATION REQUIRED. ERA 603429-14 SECTION I IS TIME LIMITED TO 12 MONTHS FROM 1XFEB2 025. FUSELAGE SKIN ON THE SKIN NEAR FR24 AND REPORTED TO BE 1.9". SECTION III IS DTE LIMITED TO 1 YEAR FROM 16FEB25. ADDITIONAL EN
- [SDR DALA2025011400324](https://openairdocs.org/sdr/DALA2025011400324.md): Longeron · cracked · Jan 12, 2025 · N304DU · Airbus BD5001A11 · Aerodynamic Fairings
  > RHS LONGERON CRACKED IN WTB FAIRING R/R WTB RHS LONGERON P/N53-1111-502 PER AMDS WC 5352-01038-01A. (LP# 6421197)
- [SDR DALA2025010800174](https://openairdocs.org/sdr/DALA2025010800174.md): Oil System · overserviced · Jan 5, 2025 · N304DU · Airbus BD5001A11 · Turbine Engine Oil System
  > BLEED AIR SYSTEM "DIRTY SOCK SMELL" DURING TAXI OUT AND CLIMBING IN KSTL AND AGAIN AFTER APU START DURING TAXI IN AT KSLC. PERFORMED STEP 1 OF NO GO ODI PREVENTION. T/S PER AMDS WORK CARD 0550-2001. FOUND NO.1 ENG OVER SERVICED, REMOVED 2 QTS OF ENG OIL PER A2
- [SDR DALA2024091609031](https://openairdocs.org/sdr/DALA2024091609031.md): Slat Track · corroded · Sep 11, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #2 LOWER AFT HAS EVIDENCE OF CORROSION. LH SLAT TRACK #2 CORROSION BLENDED PER AMDS #5742-01028-02A PERFORMED EDDY CURRENT INSPECTION IAW BD500-A-J51-01-20-01-AAA- 353A-A NO DEFECT NOTED. (LP# 0551121)
- [SDR DALA2024032803881](https://openairdocs.org/sdr/DALA2024032803881.md): Slat Track · worn · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 PINION 2 EA TEETH HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 PINION TEETH (2EA) IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260682)
- [SDR DALA2024032803880](https://openairdocs.org/sdr/DALA2024032803880.md): Slat Track · worn · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 RACK 2 EA LOWER TEETH HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 RACK TEETH (2EA) IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260676)
- [SDR DALA2024032803879](https://openairdocs.org/sdr/DALA2024032803879.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260672)
- [SDR DALA2024032803878](https://openairdocs.org/sdr/DALA2024032803878.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260271)
- [SDR DALA2024032803877](https://openairdocs.org/sdr/DALA2024032803877.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260665)
- [SDR DALA2024032803876](https://openairdocs.org/sdr/DALA2024032803876.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260660)
- [SDR DALA2024032803875](https://openairdocs.org/sdr/DALA2024032803875.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260658)
- [SDR DALA2024032803874](https://openairdocs.org/sdr/DALA2024032803874.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260657)
- [SDR DALA2024032803873](https://openairdocs.org/sdr/DALA2024032803873.md): Slat Track · corroded · Mar 25, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 607881- 14AD REV C AND PRI 607881-14AD REV 0 MATCHED. (LP# 0260656)
- [SDR DALA2024032803872](https://openairdocs.org/sdr/DALA2024032803872.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LOWER I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 LOWER FWD I/B SIDE IAW ER/A 607882 -14AD REV D AND PRI 607882-14AD REV 0 MATCHED ASSOCIATED AA 5742-01028 ADDED FOR AC 8304 A
- [SDR DALA2024032803871](https://openairdocs.org/sdr/DALA2024032803871.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 10 LOWER FWD I/B SIDE IAW ER/A 607882 -14AD REV D AND PRI
- [SDR DALA2024032803870](https://openairdocs.org/sdr/DALA2024032803870.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 9 LOWER FWD I/B SIDE IAW RE/A 607882- 14AD REV D AND PRI 60
- [SDR DALA2024032803869](https://openairdocs.org/sdr/DALA2024032803869.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 607882- 14AD REV D AND PRI 6078
- [SDR DALA2024032803868](https://openairdocs.org/sdr/DALA2024032803868.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 607882- 14AD REV D AND PRI 607882-14
- [SDR DALA2024032803867](https://openairdocs.org/sdr/DALA2024032803867.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 607882- 14AD REV D AND PRI 60788
- [SDR DALA2024032803866](https://openairdocs.org/sdr/DALA2024032803866.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 607882- 14AD REV D PRI 60788
- [SDR DALA2024032803865](https://openairdocs.org/sdr/DALA2024032803865.md): Slat Track · corroded · Mar 24, 2024 · N304DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE, IAW ER/A 607882- 14AD REV D AND PRI 607882-14AD REV 0 MATCHED ASSOCIATED AA 5742-01028 ADDED FOR AC 8304 AS
- [SDR DALA2023092607909](https://openairdocs.org/sdr/DALA2023092607909.md): Unknown · unknown · Sep 19, 2023 · N304DU · Bombdr BD1001A10 · Fuselage Main, Structure
  > ERA 612058-14 SECTION I ISSUED FOR CORROSION REPAIR TO AFT WASTE SERVICE INTERNAL DOUBLER. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II EVERY 1000 FH FROM SECTION I UNTIL SECTION III ACCOMPLISHMENT. SECTION III IS REQUIRED PRIOR TO 10000 FH FROM SECTION I.
- [SDR DALA2023062005008](https://openairdocs.org/sdr/DALA2023062005008.md): Unknown · unknown · Jun 16, 2023 · N304DU · Bombdr BD1001A10 · Passenger/Crew Doors
  > THE LH OWEED IS DISARMED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 004-0001:2818602/005 00032 RE-ARMED LH OWEED PER A220 AMP 52-21-00. (LP# 2820006)
- [SDR DALA2023062005007](https://openairdocs.org/sdr/DALA2023062005007.md): Unknown · unknown · Jun 16, 2023 · N304DU · Bombdr BD1001A10 · Passenger/Crew Doors
  > THE RH OWEED IS DISARMED.SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 004-0001:2818602/004 00031 RE-ARMED RH OWEED PER A220 AMP 52-21-00. (LP# 2819981)
- [SDR DALA2023041703028](https://openairdocs.org/sdr/DALA2023041703028.md): Unknown · unknown · Apr 12, 2023 · N304DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 607881-14AD SECTION I ISSUED FOR CORROSION TO RH SLAT TRACKS FOLLOW ON ACTION REQUIRED. ACCOMPLISHED ERA 607881-14AD REV O SECTION I FOR R/H SLAT TRACK CORROSION BLENDING. (TIME LIMITED REPAIR) RII STEP 3 WAS COMPLIED WITH ON LOG 2716878 AND N/R 22. (LP# 2
- [SDR DALA2023041703027](https://openairdocs.org/sdr/DALA2023041703027.md): Unknown · unknown · Apr 12, 2023 · N304DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 607882-14AD SECTION I ISSUED FOR CORROSION TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED.ACCOMPLISHED ERA 607882-14AD REV O SECTION I FOR L/H SLAT TRACK CORROSION BLENDING. (TIME LIMITED REPAIR) RII STEP 3 WAS COMPLIED WITH ON LOG 2716782 AND N/R 20. (LP# 27
- [SDR DALA2022111407328](https://openairdocs.org/sdr/DALA2022111407328.md): None · none · Nov 9, 2022 · N304DU · Bombdr BD1001A10 · Standard Practices/Structures
  > ERA 603429-14 SECTION I ISSUED FOR LIGHTNING STRIKE DOUBLER REPAIR AT FR24, STR9R FOLLOWING FERRY FLIGHT FROM SLC PER ERA 603446-14. FOLLOW ON ACTION IS REQUIRED. SECTION I REPAIR LIMITED TO 8000 FH FROM TIME OF ACCOMPLISHMENT. SECTION II IS TBD AND ERA REVISI
- [SDR DALA2022092706331](https://openairdocs.org/sdr/DALA2022092706331.md): None · none · Sep 23, 2022 · N304DU · Bombdr BD1001A10 · Flight Compartment Windows
  > SHIP 8304 -ATB- DUE TO FIRST OFFICERS WINDOW SHATTERING. CORRECTIVE ACTION: R/R FO WINDSHIELD AND WINDSHIELD TEMPERATURE CONTROLLER, WIPC 2 A326. (LP# 9063599)
- [SDR DALA2020121804143](https://openairdocs.org/sdr/DALA2020121804143.md): Bottle · low pressure · Dec 17, 2020 · N304DU · Airbus BD5001A11 · Emergency Equipment
  > R1 DOOR EMERGENCY ASSIST INDICATING IN THE YELLOW BAND. SERVICED R1 DOOR EOAM DOOR ASSIST CYLINDER, PER A2220 AMP BD500-A-J52-45-08-01AAA-214 A-A. SAFETY PIN REMOVED AND STOWED.

Next page: https://openairdocs.org/aircraft/N304DU/reports.md?page=2

## 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 = 'N304DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N304DU/reports

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