# Service difficulty reports: N308DU

A list on [N308DU](https://openairdocs.org/aircraft/N308DU.md).

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

- [SDR DALA2026101405650](https://openairdocs.org/sdr/DALA2026101405650.md): Reu · faulted · Oct 12, 2026 · N308DU · Airbus BD5001A11 · Rudder Control System
  > DIVERTED TO XYX, DUE TO RUDDER FAIL MESSAGE. EMERGENCY DECLARED. REMOVED & REPLACED THE NR 2 AFT REU. (LP# 8954060; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101205600](https://openairdocs.org/sdr/DALA2026101205600.md): Elec Connector · loose · Oct 8, 2026 · N308DU · Airbus BD5001A11 · Landing Gear System Wiring
  > DIVERTED TO FLL DUE TO WEIGHT ON WHEEL FAIL AND RT GEAR DISAGREE. GEAR HANDLE SELECTED DOWN AND NOW HAVE ALL THREE GREEN. FOUND CONNECTOR LOOSE AT MT1678. SAME SECURED. REPLACED MT677 AND MT678 SENSORS. (LP# 8954046, 1852016; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505501](https://openairdocs.org/sdr/DALA2026100505501.md): Light · inoperative · Sep 30, 2026 · N308DU · Airbus BD5001A11 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS, L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. (LP# 8954013; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026100505500](https://openairdocs.org/sdr/DALA2026100505500.md): Light · inoperative · Sep 30, 2026 · N308DU · Airbus BD5001A11 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - LEFT FWD OVER WING EMERGENCY LIGHT INOP. R/R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. (LP# 8964012; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092305318](https://openairdocs.org/sdr/DALA2026092305318.md): Warning Message · illuminated · Sep 22, 2026 · N308DU · Airbus BD5001A11 · Turbine Engine Oil System
  > DECLARED AN EMERGENCY FOR RIGHT ENGINE LOW OIL QUANTITY ADVISORY MESSAGE. NR 2 ENGINE REPLACED. (LP 8186488, 1823569, 8186482; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026073104435](https://openairdocs.org/sdr/DALA2026073104435.md): Skin · corroded · Jul 28, 2026 · N308DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > CORROSION ON AFT WASTE BOX SERVICE PANEL DOOR CUTOUT. COMPLIED WITH ER/A 635796-14 REV ORIGINAL ASSOCIATED ER/A 14-635796 ADDED FOR AC 8308. (LP# 1724261; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026073104434](https://openairdocs.org/sdr/DALA2026073104434.md): Door Frame · corroded · Jul 28, 2026 · N308DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT, LOWER SILL CORRODED AT SECOND PLATE FASTENER FROM AFT. C/W DELTA ER/A 635924-14 REV:ORIGINAL SECTION 1, SECTION II REPETITIVE INSPECTION WITHIN 58,500 TOTAL AIRCRAFT FLIGHT HOURS OR 30,000 TOTAL FLIGHT CYCLES FROM TIME OF MANUFACTURE, WH
- [SDR DALA2026082504827](https://openairdocs.org/sdr/DALA2026082504827.md): Doubler · corroded · Jul 27, 2026 · N308DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > ERA 635796-14: WASTE BOX INTERNAL DOUBLER / FRAME 75-76 CORROSION - SPLICE REPAIR. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN EVERY 1000 FLIGHT HOURS FROM 14,844 TOTAL FLIGHT HOURS AS OF 24JUL26 UNTIL SECTION III IS ACCOMPLISHED. AC
- [SDR DALA2026082504823](https://openairdocs.org/sdr/DALA2026082504823.md): Door Sill · corroded · Jul 27, 2026 · N308DU · Airbus BD5001A11 · Fuselage Main, Structure
  > ER/A 635924-14; A220-300/ FUSELAGE / AFT CARGO DOOR CUTOUT / FR 63 TO FR 66/ LOWER SILL / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635924-14, SECTION II REPETITIVE INSPECTION WITHIN 58,500 TOTAL AIRCRAFT FLIGHT HOURS OR 30,000 TOTAL FLIG
- [SDR DALA2026072804362](https://openairdocs.org/sdr/DALA2026072804362.md): Floor Support · not reported · Jul 27, 2026 · N308DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > ON FLOOR SUPPORT AT FR74 LBL 53.5 FWD OF FLOOR PANEL 241MLF. COMPLIED WITH ER/A 635893-14 REV ORIGINAL FOR FABRICATION AND INSTALLED PER A220 ASRP BD50-A-J51-42-06-00AAA-078A-A ASSOCIATED ER/A 14-635893 ADDED FOR AC 8308. (LP# 1723976; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072004246](https://openairdocs.org/sdr/DALA2026072004246.md): Door Frame · corroded · Jul 18, 2026 · N308DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT EQUIPMENT COMPARTMENT DOOR SURROUND STRUCTURE, FRAME 81 BETWEEN DOOR HINGES, FOUND WITH EVIDENCE OF CORROSION. REMOVED AND REPLACED FRAME 81 CENTER SECTION AT AFT EQUIPMENT COMPARTMENT DOOR SURROUND STRUCTURE IAW ASRP BD500-A-J51 -42-20-00AAA-078A-A AND
- [SDR DALA2026072004245](https://openairdocs.org/sdr/DALA2026072004245.md): Seat Track · corroded · Jul 16, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > R/H O/B SEAT TRACK AFT END CORRODED AT FR 74 RBL 43.5 WL151.5. REMOVED AND REPLACED SEAT TRACK RBL 43 FR 60 TO FR74 REF A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV-G. (LP# 1703109; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071604190](https://openairdocs.org/sdr/DALA2026071604190.md): Seat Track · corroded · Jul 14, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 23 WL151.5. REMOVED AND REPLACED L/H I/B SEAT TRACK FROM FR61 TO FR74 LBL 23 WL 151.5 IAW ASRP BD500-A-J51-42-20-00AA-078A-A AND PL C01342701 REV-G. (LP# 1699461; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071504162](https://openairdocs.org/sdr/DALA2026071504162.md): Floor Panel · damaged · Jul 12, 2026 · N308DU · Airbus BD5001A11 · Fuselage Floor Panel
  > POSSIBLE CORROSION AT R2 ENTRY FLOOR PANEL RBL49.5 FR 76 WL 151.5. REMOVED ENTRY FLOOR PANEL DAMAGED AND INSTALLED NEW ENTRY PANEL I.A.W A220 AMP BD500-A-J53-00-47-14AAA-720A-A. (LP# 1696182; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071504161](https://openairdocs.org/sdr/DALA2026071504161.md): Seat Track · corroded · Jul 12, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED RT INBD SEAT TRACK AFT END CORRODED AT FR 74 RBL 23 WL 151.5. REMOVED AND REPLACED RT INBD SEAT TRACK FROM FR 61 TO FR 74 RBL 23 WL 151.5 IAW PL C01342701 REV-G AND ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP# 1696158; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026071504160](https://openairdocs.org/sdr/DALA2026071504160.md): Web · corroded · Jul 12, 2026 · N308DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION AT FLOOR WEB FR76 RBL49.5 WL 151.5. REMOVED SILL, FLOOR (FLOOR WEB) FR 76, RBL 49.5, WL 151.5 AND INSTALLED NEW PART IAW PL C01342700 REV-T AND ASRP BD500-A-J51-42-06-00AAA-078A-A. (LP# 1695726; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071304118](https://openairdocs.org/sdr/DALA2026071304118.md): Seat Track · corroded · Jul 10, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CABIN RIGHT O/B SEAT TRACK CORROSION ON FORWARD END RBL 43.5 FR20 WL151.5. REMOVED AND REPLACED FWD CABIN RIGHT SEAT TRACK AT FR 20 TO FR 30 RBL 43.5 WL 151.5 IAW ASRP BD500-A-J51-42-20-00AAA- 078A-A AND DWG C02312600 REV K. (LP# 1692647; AIRCRAFT WAS
- [SDR DALA2026071304115](https://openairdocs.org/sdr/DALA2026071304115.md): Seat Track · corroded · Jul 9, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CABIN L/H O/B SEAT TRACK CORRODED. REMOVED AND REPLACED FWD CABIN L/H SEAT TRACK LBL 43.5 FR 20 TO FR 30 WL 151.5 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600-REV K. (LP# 1690653; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070904023](https://openairdocs.org/sdr/DALA2026070904023.md): Seat Track · corroded · Jul 6, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CABIN RIGHT INBD SEAT TRACK CORROSION ON FWD END RBL 23, FR 20, WL 151.5. REMOVED DAMAGED SEAT TRACK BTWN FR 20 TO FR 34 RBL 23 WL 151.5 AND REPLACED IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C02312600 REV-K. (LP# 1684958; AIRCRAFT WAS GROU
- [SDR DALA2026070904022](https://openairdocs.org/sdr/DALA2026070904022.md): Seat Track · corroded · Jul 6, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CABIN LT INBD SEAT TRACK CORRODED ON FWD END LBL 23, FR 20, WL 151.5. REMOVED DAMAGED SEAT TRACK BTWN FR 20 TO FR 30 LBL 23 WL 151.5 AND REPLACED IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG PL C02312600 REV-K. (LP# 1684947; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070904021](https://openairdocs.org/sdr/DALA2026070904021.md): Seat Track · corroded · Jul 5, 2026 · N308DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OTBD SEAT TRACK AFT END CORRODED AT FR 74, LBL 43.5, WL 151.5. REMOVED & REPLACED THE SEAT TRACK FROM FR 60+13" TO FR 74+6" LBL 43.5, WL 151.5 IAW PL C01342701 REV-G. (LP 1683247; AIRCRAFT WAS GROUNDED)
- [SDR DALA2025122309355](https://openairdocs.org/sdr/DALA2025122309355.md): Shutoff Valve · faulted · Dec 17, 2025 · N308DU · Airbus BD5001A11 · Pneumatic System
  > MISC - DECLARED EMERGENCY DUE TO "R BLEED FAIL" AND "ALPHA LIMIT" MESSAGES WHILE IN ICING. REPLACED THE HIGH PRESSURE SHUT OFF VALVE. (LP# 7694666)
- [SDR DALA2025121209102](https://openairdocs.org/sdr/DALA2025121209102.md): Fan · dirty · Dec 8, 2025 · N308DU · Airbus BD5001A11 · Air Distribution Fan
  > AT CRUISE A BUZZING SOUND FOLLOWED BY A BRIEF BURNT PLASTIC SMELL OCCURRED. BOTH SOUND AND SMELL IN THE AFT GALLEY WENT AWAY AFTER ALL GALLEY ELECTRICAL WAS TURNED OFF. FOUND DUSTY FAN INLET GRILL IN AFT GALLEY. NO BUZZING SOUND OR OTHER ISSUE PRESENT AFTER CL
- [SDR DALA2025061304497](https://openairdocs.org/sdr/DALA2025061304497.md): Skin · dented · Jun 10, 2025 · N308DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > ERA 602806AD REV E FUSELAGE / LH NOSE SKIN / FR 2 TO FR 3 / DENT ERA REVISED TO REV D TO ADD STAGE III DTE RESULTS. FOLLOW ON ACTION REQUIRED. SECTION V INSPECTION ADDED AT REV 3. SECTION V ADDED AND REQUIRED TO BE ACCOMPLISHED EVERY 58500 FH OR 30000 FC FROM
- [SDR DALA2025052804102](https://openairdocs.org/sdr/DALA2025052804102.md): Line · leaking · May 27, 2025 · N308DU · Airbus BD5001A11 · Turbine Engine Oil System
  > SHIP 8308-DIV- DIVERTED TO PIT DUE TO RIGHT ENGINE LOW OIL QUANTITY. TIGHTENED #4 SCAVENGE LINE AND REPLACED OIL COOLER. (LP# 7523368)
- [SDR DALA2025051503774](https://openairdocs.org/sdr/DALA2025051503774.md): Longeron · cracked · May 15, 2025 · N308DU · Airbus BD5001A11 · Aerodynamic Fairings
  > DURING WTB FAIRING INSP TASK CARD 5352-01038-01B-AD RELATED. STEP 4. LONGERON P/N C02383111-002 @ RBL40 OB SIDE ABOUT 2 FEET FROM FWD EDGE CRACK APPROX 3" LONG. LOCKED OUT RAD ALT 1, 2 AND 3 PER A220 AMP 34-44. REMOVED RAD ALT ANTENNA 3 PER A220 AMP 34-44. REM
- [SDR DALA2024032803888](https://openairdocs.org/sdr/DALA2024032803888.md): Slat Track · corroded · Mar 26, 2024 · N308DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 608452- 14AD REV D AND PRI 608452-14AD REV 0 MATCHED. (LP# 0263649)
- [SDR DALA2024032803887](https://openairdocs.org/sdr/DALA2024032803887.md): Slat Track · corroded · Mar 26, 2024 · N308DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 608452- 14AD REV D AND PRI 608452-14AD REV 0 MATCHED. (LP# 0263646)
- [SDR DALA2024032803886](https://openairdocs.org/sdr/DALA2024032803886.md): Slat Track · corroded · Mar 26, 2024 · N308DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608452- 14AD REV D AND PRI 608452-14AD REV 0 MATCHED. (LP# 0263644)
- [SDR DALA2024032803885](https://openairdocs.org/sdr/DALA2024032803885.md): Slat Track · corroded · Mar 26, 2024 · N308DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742=01028-02A. REPAIRED LH SLAT TRACK NUMBER 8 LOWER AFT SURFACE IAW ER/A 608452-14AD REV D AND PRI 608452-14AD REV D MATCHED ASSOCIATED AA 5742-01028 ADDED FOR AC 8308
- [SDR DALA2024032803884](https://openairdocs.org/sdr/DALA2024032803884.md): Slat Track · corroded · Mar 25, 2024 · N308DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608543- 14AD REV D AND PRI 608453-14AD REV 0 MATCHED. (LP# 0262237)
- [SDR DALA2024032803883](https://openairdocs.org/sdr/DALA2024032803883.md): Slat Track · corroded · Mar 25, 2024 · N308DU · 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 608543- 14AD REV D AND PRI 608453-14AD REV 0 MATCHED. (LP# 0262234)
- [SDR DALA2024032803882](https://openairdocs.org/sdr/DALA2024032803882.md): Slat Track · corroded · Mar 25, 2024 · N308DU · 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 608543- 14AD REV D AND PRI 608453-14AD REV 0 MATCHED. (LP# 0262228)
- [SDR DALA2024020101478](https://openairdocs.org/sdr/DALA2024020101478.md): Tank · full · Jan 31, 2024 · N308DU · Bombdr BD1001A10 · Waste Disposal System
  > SHIP 8308 - DIV - TO MSP DUE TO ALL LAVATORIES INOPERATIVE. LAVATORY TANK IS SHOWING FULL. CORRECTIVE ACTION: SERVICED LAVATORIES. (LP# 0179650)
- [SDR DALA2023120109881](https://openairdocs.org/sdr/DALA2023120109881.md): Unknown · unknown · Nov 30, 2023 · N308DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR - AREA COVERED BY THE LOWER SCUFF PLATE HAS CORROSION AROUND FAST ENER LOCATIONS MARKED. PIC. SEE N/R 33. COMPLIED WITH ER/A 613852-14 PRI REV 0, ER/A 613852-14 PRI REV 1 AND FINAL ER/A 613852-14 REV ORIGINAL. SEE N/R 33. (LP# 0088413)
- [SDR DALA2023120109883](https://openairdocs.org/sdr/DALA2023120109883.md): Unknown · unknown · Nov 29, 2023 · N308DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AFT LEFT PASSENGER DOOR - SEVERAL SCUFF PLATE FASTENER HOLES HAVE LIGHT CORROSION ON THE SURFACE AND IN THE BORES. - M - SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0257:5360-2023/001 00048 COMPLIED WITH ER/A 613855-14 PRI REV 0, ER/A 613855-14 PRI REV 1 AND
- [SDR DALA2023120109882](https://openairdocs.org/sdr/DALA2023120109882.md): Unknown · unknown · Nov 29, 2023 · N308DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AFT RIGHT SERVICE DOOR HAS MULTIPLE SPOTS OF CORROSION ON LOWER THRESHOLD. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0261:5360-2024/001 00014 REPAIRED PER PRI 613853-14 REV 0, PRI 613853-14 REV 1, AND ERA 613853-14 REV O SEC 1. (LP# 0087637)
- [SDR DALA2023101008327](https://openairdocs.org/sdr/DALA2023101008327.md): Unknown · unknown · Oct 5, 2023 · N308DU · Bombdr BD1001A10 · Fuselage Structure (General)
  > DURING WALK-AROUND ON SERVICE CHECK, CORROSION FOUND ON WASTE BOX DOUBLER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:0514-2001/004 00017 REPAIRED PER PRI 612578-14 REV 0, 1, 2, AND ER/A 612578-14 REV ORIGINA
- [SDR DALA2024041304394](https://openairdocs.org/sdr/DALA2024041304394.md): Doubler · corroded · Oct 3, 2023 · N308DU · Airbus BD5001A11 · Wing, Plate/Skin
  > AIRCRAFT 8308, DURING SLAT TRACK INSPECTION IN MSP, THE C01342310-109 INTERNAL WASTE DOUBLER WAS FOUND CORRODED IN THE FORWARD INBD CORNER. CORRECTIVE ACTION: REPAIRED PER ER/A 612578-14. FABRICATED A SKIN REPAIR DOUBLER AND TRIPLER, INSTALL SKIN REPAIR DOUBLE
- [SDR DALA2023050103363](https://openairdocs.org/sdr/DALA2023050103363.md): Unknown · unknown · Apr 30, 2023 · N308DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 608452-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VIS IT. FOLLOW ON ACTION IS REQUIRED. LH WING SLAT TRACKS 1-11 ARE AFFECTED.ACCOMPLISH ERA 608452-14AD SECTION II EVERY 850 FH AFTER SECTION I. ERA 608452-14AD SECTION IIS TIME LIMITED TO 8500 FH. ER
- [SDR DALA2023050103362](https://openairdocs.org/sdr/DALA2023050103362.md): Unknown · unknown · Apr 30, 2023 · N308DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 608453-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VIS IT. FOLLOW ON ACTION IS REQUIRED. RH WING SLAT TRACKS 1-11 ARE AFFECTED.ACCOMPLISH ERA 608453-14AD SECTION II EVERY 850 FH AFTER SECTION I. ERA 608453-14AD SECTION IIS TIME LIMITED TO 8500 FH. ER
- [SDR DALA2023040302539](https://openairdocs.org/sdr/DALA2023040302539.md): Unknown · unknown · Mar 31, 2023 · N308DU · Bombdr BD1001A10 · Air Conditioning System
  > MUSTY ODOR NOTICED ON CLIMB OUT STRONGEST 4000 SML-FL180, THEN IT SEEMED TO DISSIPATE. PER MTC REQUEST PERFORMED BORESCOPE INSPECTION OF THE LPC PER A220 AMP 72-31-00-00AAA-312A-A AND HPC PER A220 AMP 72-35-00- 00AAA-312A ON NBR 1 AND 2 ENGINES FOR SIGNS OF OI
- [SDR DALA2023031401871](https://openairdocs.org/sdr/DALA2023031401871.md): None · none · Mar 10, 2023 · N308DU · Bombdr BD1001A10 · Fuselage Main, Plate/Skin
  > ER/A 602806-14 REV B ISSUED FOR SECTION III PERMANENT REPAIR ACCOMPLISHMENT. FOLLOW ON ACTION (DTE) IS REQUIRED. DTE IS REQUIRED. ER/A 602806-14 REV B SECTION III APPROVAL IS LIMITED TO 12 MONTHS. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRE
- [SDR DALA2026021701089](https://openairdocs.org/sdr/DALA2026021701089.md): Frame · dented · Feb 24, 2023 · N308DU · Airbus BD5001A11 · Fuselage Main, Frame
  > ON WALKAROUND, FOUND TWO DENTS ON THE FRAMES OF AFT OF RADOME ON RT SIDE OF FUSELAGE. REPAIRED PER ER/A 606387-14 REV A, PRI REV.1, WAITING ON ABC RVSM SKIN CONTOUR RESULTS AND FINAL ER/A. ( 00127702 10FEB26 07:45 UTC) (ETS WIP) MECHANIC: ACCOMPLISHED ERA 60
- [SDR DALA2026021701088](https://openairdocs.org/sdr/DALA2026021701088.md): Frame · dented · Feb 24, 2023 · N308DU · Airbus BD5001A11 · Fuselage Main, Frame
  > TWO DENTS ON FRAMES AFT OF RADOME ON RT SIDE OF FUSELAGE. C/W ERA 606387-14, REV ORIG, SECTION 1, OMITTED STEP 4 FOR TIME. ER/A PERMANENT REPAIR MUST BE DONE PRIOR TO CLOSING LOG 23 FEB, 2023 FLT 2477, REP 850 TER 8500 APPROVED PER DAL P.S. 900-5-1 NO 4. ACCO
- [SDR DALA2023011000185](https://openairdocs.org/sdr/DALA2023011000185.md): Unknown · odor · Jan 5, 2023 · N308DU · Bombdr BD1001A10 · Air Distribution System
  > CAPTAIN REPORTED DURING LANDING DIRTY SOCK SMELL IN COCKPIT. PERFORMED STEP 1 O FNO GO ODI. AFT GALLEY & BOTH AFT LAVS APPEARED TO HAVE DIRTY SOCK SMELL OTHER THAN COCKPIT. C/W JIC O550-2001. NO ODOR SMELL NOTED. C/W LT & RT ENGINES SOLUTION ID #1-8449 & 1-8
- [SDR DALA2022021500955](https://openairdocs.org/sdr/DALA2022021500955.md): None · none · Feb 11, 2022 · N308DU · Bombdr BD1001A10 · Fuel Control/Turbine Engines
  > SHIP 8308 -DIV- FLIGHT DIVERTED TO JFK DUE TO R ENG OPER DEGRADED MESSAGE DISPLAYED SHORTLY AFTER TAKE-OFF. PER QRH LANDED AT NEAREST SUITABLE AIRPORT. CORRECTIVE ACTION: PERFORMED EEC SYSTEM TEST PER A220 AMP 73-21, TEST NORMAL AND FAULTS CLEARED. DOWNLOADED
- [SDR DALA2022012600532](https://openairdocs.org/sdr/DALA2022012600532.md): Controller · faulted · Jan 25, 2022 · N308DU · Airbus BD5001A11 · Turbine Engine Compressor Section
  > ON T/O ROLL LOUD BANG. WITH LOUD BURNING SMELL. NOTICED THE RELIGHT ICON OVER THE #1 ENGINE, APU OFF, ENGINE A/I ON. SMELL WENT AWAY AFTER ABOUT 3 MINS. PERFORMED BORO OF #1 ENG HPC PER AMP 72-35-00 & LPT STAGES 1-3 PER AMP 72-53-00. NO DEFECTS NOTED. C/W POST
- [SDR DALA2021100506089](https://openairdocs.org/sdr/DALA2021100506089.md): None · none · Oct 4, 2021 · N308DU · Airbus BD5001A10 · Engine Indicating System
  > SHIP 8308 -ATB- DUE TO RECEIVING AN ENG VIBE MESSAGE AND A MASTER CAUTION LIGHT SEVERAL TIMES AFTER TAKEOFF. PER QRH EFFECTED ENGINE TO BE OPERATED AT REDUCED THRUST, RETURNED TO DFW. CORRECTIVE ACTION: INSPECTED THE MCD'S AND FOUND METAL ON THE #3 BEARING COM

## 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 = 'N308DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N308DU/reports

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