# Service difficulty reports: N306DU

A list on [N306DU](https://openairdocs.org/aircraft/N306DU.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 · 98 reports

- [SDR DALA2026081404650](https://openairdocs.org/sdr/DALA2026081404650.md): Seal · leaking · Aug 12, 2026 · N306DU · Airbus BD5001A11 · Turbine Engine Oil System
  > IN FLIGHT LIGHT ODOR DETECTED AROUND ROWS 17,18,19,20. FOUND OIL IN NR 2 ENGINE SPINNER, REPLACED FAN SHAFT COVER SEAL PER A220 AMP 72-15. AMDS W/C'S 0550-2001 AND 0550-2003 COMPLIED WITH. (LP 9615706 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080404485](https://openairdocs.org/sdr/DALA2026080404485.md): Engine · vibration · Aug 3, 2026 · N306DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)
  > DIVERTED TO ATL DUE TO NBR 2 ENGINE VIBES. NR 2 ENG VIBS 1.25 FOR 38 SEC. MAINTENANCE IN PROGRESS.
- [SDR DALA2026070904025](https://openairdocs.org/sdr/DALA2026070904025.md): Strut · fod · Jul 7, 2026 · N306DU · Airbus BD5001A11 · Landing Gear Position and Warning
  > ATB - WOW FAIL ON TAKE OFF. REMOVED LT MLG SHOCK STRUT. FOUND CHEESE CLOTH WRAPPED AROUND BEARING AND SEALS. REMOVED ALL DEBRIS, RE-PACKED LEFT MLG SLIDING TUBE. REPLACED LEFT MLG INBOARD SHOCK STRUT HARNESS. (LP# 8948758, 8948756, 8948760; AIRCRAFT WAS GROUN
- [SDR DALA2026062903853](https://openairdocs.org/sdr/DALA2026062903853.md): Anti-Ice Valve · faulted · Jun 24, 2026 · N306DU · Airbus BD5001A11 · Airfoil Anti/De-ice System
  > DIV - TO SLC DUE TO "R WING A/ICE FAIL" MESSAGE. R & R RT WAI VALVE AND PRESSURE SENSOR HARNESS. (LP# 8948718; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062303731](https://openairdocs.org/sdr/DALA2026062303731.md): Light · inoperative · Jun 20, 2026 · N306DU · Airbus BD5001A11 · Emergency Lighting
  > MULTIPLE EMERGENCY EXIT EXTERIOR LIGHTS OUT. REPLACED EMERGENCY EXTERNAL LIGHTS (FWD RT, AFT LT AND AFT RT) IAW AMP BD500-A-J33-55-02-01AAA-520A-A, BD500-A-J33-55-02- 01AAA-720A-A, BD500-A-J33-55-02-03AAA-520A-A AND BD500-A-J33-55- 00-01AAA-320A-A. OPERATIONAL
- [SDR DALA2026062303730](https://openairdocs.org/sdr/DALA2026062303730.md): Light · inoperative · Jun 19, 2026 · N306DU · Airbus BD5001A11 · Emergency Lighting
  > BOTH LT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE, NEED TO REPLACE. REPLACED BOTH LT OVERWING EXTERNAL EMERGENCY LIGHT IAW AMP BD500-A-J33-55-02-02AAA-720A-A. OP TEST PASSED. (LP# 1655680, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061703626](https://openairdocs.org/sdr/DALA2026061703626.md): Floor Support · corroded · Jun 15, 2026 · N306DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION AT REAR BARREL FLOOR EDGE SUPPORT AT FR 76 RBL 49 WL 147. REMOVED AND REPLACED SILL FLOOR WEB AT STA FR76 RBL 49 WL 147 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342700 REV:-T. (LP# 1648146; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061703625](https://openairdocs.org/sdr/DALA2026061703625.md): Floor Panel · corroded · Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 221 KLF (L1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 221 KLF AT L1 DOOR PER AMP BD500-A-J53 -00-47-12AAA-720A-A. (LP# 1645035; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503586](https://openairdocs.org/sdr/DALA2026061503586.md): Floor Panel · corroded · Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor Panel
  > CORROSION ON FORWARD CABIN FLOOR PANEL 222 KRF (R1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 222 KRF AT R1 DOOR IAW AMP BD500-A-J53 -00-47-12AAA-720A-A. (LP# 1643774; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503585](https://openairdocs.org/sdr/DALA2026061503585.md): Floor Panel · corroded · Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor Panel
  > AFT SERVICE DOOR FLOOR PANEL 242MRF CORRODED ON AFT INBD CORNER. REMOVED AND REPLACED FLOOR PANEL 242MRF AT AFT SERVICE DOOR IAW AMP BD500-A-J53-00-47-14AAA-720A-A. (LP# 1643694; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061503584](https://openairdocs.org/sdr/DALA2026061503584.md): Floor Support · corroded · Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION AT REAR BARREL FLOOR EDGE SUPPORT BETWEEN FR 74 TO FR 76 LBL 49 WL147. REMOVED AND REPLACED FLOOR PANEL SUPPORT FROM FR74 TO FR76 LBL 49 WL 147 IAW A220 AMP BD500-A-J53-00-47-13AAA-720A-A. (LP# 1643683; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026060903489](https://openairdocs.org/sdr/DALA2026060903489.md): Seat Track · corroded · Jun 4, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342722-009S1 LOT 5196527-3 AT REAR BARREL FROM FR 61 TO FR74 LBL 23 WL 147 PER DWG BOMBARDIER PL C01342701 REV- G. AND A220 ASRP BD500-A-J51-42 -20-00
- [SDR DALA2026060903488](https://openairdocs.org/sdr/DALA2026060903488.md): Seat Track · corroded · Jun 4, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342723-0095 LOT 5194663-1 OF REAR BARREL FROM FR61 TO FR74 PER DWG BOMBARDIER PL C01342701 REV-G AND A220 ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP# 16
- [SDR DALA2026053003280](https://openairdocs.org/sdr/DALA2026053003280.md): Seat Track · corroded · May 29, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 43.5 WL147. REPLACED SEAT TRACK AT LBL=43.5, WL=147 BTW FR=60 TO FR=75 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A PAR. 3, 5 AND BOMBARDIER DWG= C01342701 REV= G. (LP 1620113 - AIRCRAFT WAS GROU
- [SDR DALA2026053003279](https://openairdocs.org/sdr/DALA2026053003279.md): Seat Track · corroded · May 29, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 43.5 FR 20 WL 147. REPLACED SEAT TRACK RBL 43.5 FR20 - FR30 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV - K. (LP 1620095 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052703196](https://openairdocs.org/sdr/DALA2026052703196.md): Seat Track · corroded · May 26, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 43.5 WL147. REPLACED SEAT TRACK RBL 43.5 FR61 - FR74 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV G. (LP 1614438 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052703195](https://openairdocs.org/sdr/DALA2026052703195.md): Seat Track · corroded · May 26, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 23 FR 20 WL 147. REPLACED FWD CABIN RIGHT SIDE SEAT TRACK RBL23 BTW FR19 TO FR31 WL 147 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A PAR. 3 AND 5 AND DWG BOMBARDIER C02312600 REV: K. (LP 1614290 - AIRCRAFT WAS GR
- [SDR DALA2026011400342](https://openairdocs.org/sdr/DALA2026011400342.md): Slide · warning message · Jan 12, 2026 · N306DU · Airbus BD5001A11 · Escape Slide
  > ON FINAL APPROACH, WING SLIDE CAUTION COME ON INTERMITTENTLY. DOORS PAGE SHOWED LEFT SLIDE YELLOW DOOR INDICATION IN AFT. INTERMITTENT INDICATION CONTINUED ON THE GROUND. REMOVED AND REPLACED L/H OVERWING SLIDE IN REF. WITH AMDS W/C # 2563-4002. OK FOR SVC. RI
- [SDR DALA2025111708376](https://openairdocs.org/sdr/DALA2025111708376.md): Skin · punctured · Nov 14, 2025 · N306DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE, AFT OF DOOR 1L. ACCESSED TO DAMAGE IS FWD BB, SUBMITTED DIMENSIONS OF DAMAGE TO ENGINEERING. ALL REPAIR WORK COMPLETED IAW ER/A 630504-14 REV. A. RII'S COMPLIED WITH. FWD CARGO SIDEWALL PANEL INSTALLED IAW AMP 50-11. ASSOCIATED ER/A 14-63
- [SDR DALA2025070204957](https://openairdocs.org/sdr/DALA2025070204957.md): Engine · odor · Jun 25, 2025 · N306DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)
  > DIRTY SOCK SMELL IN AFT GALLEY DURING DESCENT. T/S PER AMDS W/C 0550-2001. FOUND OIL ODOR COMING FROM LT ENG DURING HIGH POWER OP (+80% N1). C/W AMDS W/C 0550-6001. C/W MEL 36-12-00A, REF LOG # 7382643. ERA 613840-14TR SEC. II (WATER WASH) REQ WITHIN 5 CALENDA
- [SDR DALA2025052003863](https://openairdocs.org/sdr/DALA2025052003863.md): Slat Track · corroded · May 16, 2025 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #4 RACK TEETH 1 AND 2 HAS EVIDENCE OF CORROSION WITH EVIDENCE OF PREVIOUS REWORK. LIAISON ENGINEERING SUPPORT WILL BE REQ BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 620728-14AD REV B AND PRI 620728-14AD REV O MATCHES. (LP# 0969341)
- [SDR DALA2025010800175](https://openairdocs.org/sdr/DALA2025010800175.md): Unknown · odor · Jan 5, 2025 · N306DU · Airbus BD5001A11 · Air Distribution System
  > ON DESCENT THROUGH 8000 FT WE SMELLED A STRONG ODOR SIMILAR TO OIL BURNING FOR APPROXIMATELY TWO MINUTES IN BOTH THE FLIGHT DECK AND CABIN. NO SMOKE WAS PRESENT. BOTH ENGINES AND ALL SYSTEMS WERE OPERATING NORMAL. APU WAS OFF. LEFT OIL QUANTITY 26.5, RIGHT 25.
- [SDR DALA2024093009542](https://openairdocs.org/sdr/DALA2024093009542.md): Valve · locked · Sep 28, 2024 · N306DU · Airbus BD5001A11 · Cabin Temperature Control System
  > SHIP 8306 - ATB - DUE TO TRIM AIR INDICATION WITH TRIM AIR VALVE LOCKED CLOSED. CORRECTIVE ACTION: REMOVED AND REPLACED TRIM AIR PRESSURE REGULATING VALVE. OPS CHECK OK. (LP 6049314)
- [SDR DALA2024021302039](https://openairdocs.org/sdr/DALA2024021302039.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2107 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302038](https://openairdocs.org/sdr/DALA2024021302038.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LOWER FORWARD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2054 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5
- [SDR DALA2024021302037](https://openairdocs.org/sdr/DALA2024021302037.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2050 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742
- [SDR DALA2024021302036](https://openairdocs.org/sdr/DALA2024021302036.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2047 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII
- [SDR DALA2024021302035](https://openairdocs.org/sdr/DALA2024021302035.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > L/H SLAT TRACK NBR 1 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2044 UTC 02 CORR BY SPURLIN 02405497
- [SDR DALA2024021302034](https://openairdocs.org/sdr/DALA2024021302034.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2040 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742 R
- [SDR DALA2024021302033](https://openairdocs.org/sdr/DALA2024021302033.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2036 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302032](https://openairdocs.org/sdr/DALA2024021302032.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2016 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302031](https://openairdocs.org/sdr/DALA2024021302031.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2003 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302030](https://openairdocs.org/sdr/DALA2024021302030.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH 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 FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1912 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302029](https://openairdocs.org/sdr/DALA2024021302029.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1852 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302028](https://openairdocs.org/sdr/DALA2024021302028.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1833 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII
- [SDR DALA2024021302027](https://openairdocs.org/sdr/DALA2024021302027.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1816 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RI
- [SDR DALA2024021302026](https://openairdocs.org/sdr/DALA2024021302026.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1756 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RI
- [SDR DALA2024021302025](https://openairdocs.org/sdr/DALA2024021302025.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > 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 FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1713 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021302024](https://openairdocs.org/sdr/DALA2024021302024.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER FORWARD O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1653 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RI
- [SDR DALA2024021302023](https://openairdocs.org/sdr/DALA2024021302023.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1624 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RI
- [SDR DALA2024021302022](https://openairdocs.org/sdr/DALA2024021302022.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1558 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII
- [SDR DALA2024021201919](https://openairdocs.org/sdr/DALA2024021201919.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2101 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 02453691 W
- [SDR DALA2024021201918](https://openairdocs.org/sdr/DALA2024021201918.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2052 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 0245369
- [SDR DALA2024021201917](https://openairdocs.org/sdr/DALA2024021201917.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2049 UTC 02 CORR BY SPURLIN 02405497
- [SDR DALA2024021201916](https://openairdocs.org/sdr/DALA2024021201916.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2045 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 018
- [SDR DALA2024021201915](https://openairdocs.org/sdr/DALA2024021201915.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2042 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021201914](https://openairdocs.org/sdr/DALA2024021201914.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2039 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742
- [SDR DALA2024021201913](https://openairdocs.org/sdr/DALA2024021201913.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2031 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N
- [SDR DALA2024021201912](https://openairdocs.org/sdr/DALA2024021201912.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2009 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII
- [SDR DALA2024021201911](https://openairdocs.org/sdr/DALA2024021201911.md): Slat Track · corroded · Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1925 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N

Next page: https://openairdocs.org/aircraft/N306DU/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 = 'N306DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N306DU/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
