# Service difficulty reports: N307DU

A list on [N307DU](https://openairdocs.org/aircraft/N307DU.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 · 62 reports

- [SDR DALA2026092805386](https://openairdocs.org/sdr/DALA2026092805386.md): Bearing · sheared · Sep 22, 2026 · N307DU · Airbus BD5001A11 · Passenger/Crew Doors
  > L1 DOOR STUCK ON ARRIVAL. FOUND INTERLOCK BEARING SHEARED. REMOVED REMAINING PIECES IAW AMP 52-15. INSTALLED NEW INTERLOCK LEVER IAW AMP 52-15. DOOR OPS NORMAL. (LP# 8261220; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080704583](https://openairdocs.org/sdr/DALA2026080704583.md): Fitting · corroded · Aug 6, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR ENTRY WAY BETWEEN FR24 & FR29 FITTINGS 4EA AT ENTRY FOR SUPPORTING FLOOR HAVE CORROSION LEVEL 2 ON TOP SURFACE AND PAINT DETERIORATED. REPLACED THE FITTINGS, IAW ASRP BD500-A-J51-77-00-00AAA-028A-A. (LP 1742285 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080704582](https://openairdocs.org/sdr/DALA2026080704582.md): Bushing · corroded · Aug 6, 2026 · N307DU · Airbus BD5001A11 · Nacelle/Pylon, Main Frame
  > PITTING FOUND ON INNER RACE OF R3 INBOARD BUSHING. REPLACED BUSHING NR 436. (LP 1742279 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080504503](https://openairdocs.org/sdr/DALA2026080504503.md): Threshold · corroded · Aug 3, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FWD LT PASSENGER DOOR THRESHOLD 221 KLF HAS CORROSION IN FASTENER HOLE, FWD OTBD CORNER. R & R SILL ASSEMBLY PANEL 221KLF REF AMP 53-00-47. (LP# 1736819; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080504504](https://openairdocs.org/sdr/DALA2026080504504.md): Skin · cracked · Aug 2, 2026 · N307DU · Airbus BD5001A11 · Wing, Plate/Skin
  > LEFT WING, LE, NR 2 SLAT TRACK CUTOUT CRACKED 0.219, AFT OTBD RADIUS, VERIFIED WITH HFEC IAW AND TP BD500-A-J51-01-08- 01AAA-353A-A. SEE NR FOR ADDITIONAL INFORMATION 001-0697:2021-2065-LH/004 00177 REPAIRED PER ER/A 634994-14TR REV ORIGINAL. (LP# 1734825; A
- [SDR DALA2026080504502](https://openairdocs.org/sdr/DALA2026080504502.md): Doubler · corroded · Aug 2, 2026 · N307DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > WASTE BOX DOUBLER CORROSION AT CUTOUT ON FWD RH CORNER AND AFT EDGE. COMPLIED WITH ER/A 613288-14 REV A PRI REV 0, ER/A 613288-14 REV A PRI REV 1, AND FINAL ER/A 613288-14 REV A. (LP# 1734788: AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080404483](https://openairdocs.org/sdr/DALA2026080404483.md): Scuff Plate · corroded · Jul 31, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > DURING C2 + 6 YEAR (HEAVY) CHECK IN MSP, MTC WAS ACCOMPLISHING AA 5331-01297-01C MOD WHEN THEY REPORTED CORROSION UNDER THE SCUFF PLATE, ON THE SUBJECT (PN C02313004-007 LOWER SILL, C02313004-005 ASSY.) AT SCUFF PLATE ATTACH FASTENER HOLE LOCATIONS 1 AND 9. MA
- [SDR DALA2026073104438](https://openairdocs.org/sdr/DALA2026073104438.md): Floor Support · corroded · Jul 29, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR SUPPORT BEAM FR 76-78, AT RBL 37. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/015 00578 COMPLIED WITH ERA 635283-14 PRI REV 0, 1, 2, AND ERA 635283-14 R
- [SDR DALA2026072804361](https://openairdocs.org/sdr/DALA2026072804361.md): Threshold · no discrepancy · Jul 27, 2026 · N307DU · Airbus BD5001A11 · Standard Practices/Structures
  > REMOVE AFT SERVICE DOOR THRESHOLD PANEL TO FOM. ADDITIONAL INFORMATION 001-0582:5300-2008/006 00536 REMOVED AND REINSTALLED THRESHOLD PANEL 242MRF PER A220 AMP 53-00-47. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-
- [SDR DALA2026071604193](https://openairdocs.org/sdr/DALA2026071604193.md): Seat Track · corroded · Jul 15, 2026 · N307DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AFT MOST CABIN SEAT TRACK RBL 23 SHOWS SIGNS OF CORROSION. COMPLIED WITH ER/A 635190-14 PRI REV 0, ER/A 635190-14 PRI REV 1 AND FINAL ER/A 635190-14 REV ORIGINAL. CORRODED SEAT TRACK SECTION WAS REPLACED. (LP# 1701470; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071604191](https://openairdocs.org/sdr/DALA2026071604191.md): Floorbeam · corroded · Jul 15, 2026 · N307DU · Airbus BD5001A11 · Fuselage Main, Floor Beam
  > LEFT PASSENGER FLOOR HAS CORROSION AT ATTACHMENT HOLE LOCATED FR76 LBL 52.5. REMOVED AND REPLACED FLOOR BEAM REF DWG C01342759 REV D AND A220 ASRP 51-42-00. (LP# 1700264; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071604192](https://openairdocs.org/sdr/DALA2026071604192.md): Attach Fitting · corroded · Jul 14, 2026 · N307DU · Airbus BD5001A11 · Nacelle/Pylon, Attach Fittings
  > CORROSION FOUND ON RH OUTER UPPER FORWARD PYLON ATTACH FITTINGS R7 AND R8. REMOVED AND REPLACED BEARINGS PER BOMBARDIER DWG C01627010 -B. (LP# 1700103; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071604189](https://openairdocs.org/sdr/DALA2026071604189.md): Floor Support · corroded · Jul 14, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, RBL 53. REPLACED EDGE SUPPORT MEMBER PER ASRP 51-42-06. (LP# 1699452; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071604187](https://openairdocs.org/sdr/DALA2026071604187.md): Fitting · corroded · Jul 13, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR FITTING HAS CORROSION NEAR FR 74 UNDER DOOR THRESHOLD PANEL. REMOVED AND REPLACED PER ASRP 51-77-00-00-028. CORROSION IS LEVEL 2. (LP 1697908; AIRCRAFT IS GROUNDED)
- [SDR DALA2026071504163](https://openairdocs.org/sdr/DALA2026071504163.md): Floor Support · corroded · Jul 11, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, LBL 54.5. -M- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/004 00567 REPLACED SUPPORT MPN C01342782-103 PER ASRP 51-42-06. (LP# 1694108; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026071304117](https://openairdocs.org/sdr/DALA2026071304117.md): Seat Track · corroded · Jul 9, 2026 · N307DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AFT MOST CABIN SEAT TRACK RBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-20. (LP# 1690284; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071304113](https://openairdocs.org/sdr/DALA2026071304113.md): Seat Track · corroded · Jul 8, 2026 · N307DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RBL 23 SHOWS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2022/002 00260 SEAT TRACK REPLACED PER A220 ASRP 51-42-20 AND A220 DWG C02312600. (LP# 1689355; AIRCRAFT WAS GR
- [SDR DALA2026071304112](https://openairdocs.org/sdr/DALA2026071304112.md): Floorbeam · corroded · Jul 8, 2026 · N307DU · Airbus BD5001A11 · Fuselage Main, Floor Beam
  > PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR EDGE SUPPORT MEMBER AT FR 74, LBL 49. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/005 00568 REPLACED SUPPORT MPN C01342782-103 PER A220 ASRP 51-42-06. (
- [SDR DALA2026071004050](https://openairdocs.org/sdr/DALA2026071004050.md): Threshold · corroded · Jul 7, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR THRESHOLD, CORROSION FOUND AT AFT INBD CORNER. DRILLED NEW THRESHOLD, REF ASRP BD500-A-J51-77-00-00AAA-028A-A. INSTALLATION TO BE ACCOMPLISHED ON NR 490. (LP# 1686829; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071004049](https://openairdocs.org/sdr/DALA2026071004049.md): Threshold · corroded · Jul 7, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR THRESHOLD - CORROSION FOUND AT FWD INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/017 00584 COMPLETE: DRILLED NEW THRESHOLD, REF A220 ASRP BD500-A-J51-77-00-00AAA-028A-A. I
- [SDR DALA2026070703958](https://openairdocs.org/sdr/DALA2026070703958.md): Door Sill · corroded · Jun 30, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FWD RT SERVICE DOOR, FWD THRESHOLD ATTACHMENT HOLE HAS LIGHT CORROSION. SILL ASSEMBLY REPLACED IAW ASRP 53-21-24 AND DRAWINGS C02312000 AND C02316000. (LP# 1674914; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070703956](https://openairdocs.org/sdr/DALA2026070703956.md): Seat Track · corroded · Jun 28, 2026 · N307DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK LBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK REF. A220 ASRP 51-77-00. (LP# 1670327; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070703955](https://openairdocs.org/sdr/DALA2026070703955.md): Seat Track · corroded · Jun 28, 2026 · N307DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RBL 43.5 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW ASRP BD500- A-J51-42-00-00AAA-028A-A AND DWG C02312600. (LP# 1670326; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070703953](https://openairdocs.org/sdr/DALA2026070703953.md): Bearing · corroded · Jun 27, 2026 · N307DU · Airbus BD5001A11 · Nacelle/Pylon, Main Frame
  > CORROSION FOUND ON NR 1 ENGINE PYLON UPPER FORWARD SPHERICAL BEARINGS R7 AND R8. REMOVED AND REPLACED BEARINGS IAW DWG C01627010 -B. (LP# 1669886; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070703952](https://openairdocs.org/sdr/DALA2026070703952.md): Bearing · damaged · Jun 27, 2026 · N307DU · Airbus BD5001A11 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE PYLON BOX BEAM R7. REMOVED AND REPLACED THE BEARINGS IAW DWG C01701332. (LP# 1669877; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062303732](https://openairdocs.org/sdr/DALA2026062303732.md): Threshold · corroded · Jun 20, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > LEFT PASSENGER DOOR THRESHOLD, CORROSION FOUND IN ATTACHMENT HOLE AT FR 74 LBL 54.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0196:2531-4003/027 00595. REMOVED AND REPLACED FLOOR FITTING IAW ASRP 51-42-20. (L
- [SDR DALA2026062303735](https://openairdocs.org/sdr/DALA2026062303735.md): Floor Support · corroded · Jun 20, 2026 · N307DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > PER MTX REQUESTED OI, FOUND CORROSION ON FLOOR SUPPORT FR 76-78, AT LBL 37. REMOVED AND REPLACED FLOOR SUPPORT PER ASRP 51-77-00. (LP# 1656729; AIRCRAFT WAS GROUNDED)
- [SDR DALA2025122309351](https://openairdocs.org/sdr/DALA2025122309351.md): Longeron · cracked · Dec 21, 2025 · N307DU · Airbus BD5001A11 · Fuselage Main, Longeron/Stringer
  > LONGERON AT RBL 40.0 CRACKED AT FWD END APPROX 18"LONG AT RADIUS BETWEEN VERT & OUTER FLANGES. AD RELATED, WC 5352-01038-01B. REMOVED AND REPLACED LONGERON @ RBL 40.0 PER A220 ASRP 51-77-00. (LP# 1362563)
- [SDR DALA2025051303717](https://openairdocs.org/sdr/DALA2025051303717.md): Pinion · corroded · May 9, 2025 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #11 MEASUREMENTS WERE OUT-OF-LIMITS. ENGINEERING REQUESTS TO REMOVE AND REPLACE PINION P/N: C01612526-001. REMOVED SLAT PINION #11 IAW A220 AMP 27-81-09 P/N: C01612526-001 S/N: 501940 J. HARMON 2420359. OK TO INSTALL SLAT PINION #11 REF A220 27-8
- [SDR DALA2025051303716](https://openairdocs.org/sdr/DALA2025051303716.md): Slat Track · corroded · May 9, 2025 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #11, RACK TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION AFT PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622237-14AD REV A AND PRI 622237-14AD REV 1 MATCHES. (LP# 0957161)
- [SDR DALA2025051303715](https://openairdocs.org/sdr/DALA2025051303715.md): Pinion · corroded · May 9, 2025 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH PINION #11, TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION LWR PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622237-14AD REV A AND PRI 622237-14AD REV 1 MATCHES. (LP# 0957159)
- [SDR DALA2025051303714](https://openairdocs.org/sdr/DALA2025051303714.md): Pinion · corroded · May 9, 2025 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH PINION #4, TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION LWR & PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622237-14AD REV A AND PRI 622237-14AD REV 1 MATCHES. (LP# 0957156)
- [SDR DALA2025051303713](https://openairdocs.org/sdr/DALA2025051303713.md): Slat Track · corroded · May 9, 2025 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #4, RACK TOOTH #1 AND 2 HAS EVIDENCE OF CORROSION AFT PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622237-14AD REV A AND PRI 622237-14AD REV 1 MATCHES. (LP# 0957151)
- [SDR DALA2025031902076](https://openairdocs.org/sdr/DALA2025031902076.md): Longeron · broken · Mar 16, 2025 · N307DU · Airbus BD5001A11 · Fuselage Main, Structure
  > FOUND 1 EA LONGERON ASSEMBLY P/N: C02383111-001 BROKEN. REMOVED AND REPLACED LONGERON P/N: C02383111-001 IAW AMDS W/C 5352-01038-05A. (LP# 0860849)
- [SDR DALA2024091208944](https://openairdocs.org/sdr/DALA2024091208944.md): Slat Track · not reported · Sep 7, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > REMOVE AND REPLACE LH #4 SLAT TRACK AND PINION. SUMMARY. REPLACEMENT WORKED IN CONJUNCTION WITH AMDS W/C 2781- 4002-LH. REMOVED AND REPLACED L/H SLAT TRACK #4 P/N OFF: C01612072-005 S/N OFF: AS1616 P/N ON: C01612074-007 S/N ON AS008635 FTN 705M0E IAW A220 AMP
- [SDR DALA2024090908858](https://openairdocs.org/sdr/DALA2024090908858.md): Slat Track · corroded · Sep 5, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH#7 SLAT TRACK UPPER FWD HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORMED HFEC OF BLENDED AREA ON TRACK, NO DEFECTS NOTED ALL WORK DONE IAW ANDTP BD500-A-J51-01-20-01AAA-353A-A
- [SDR DALA2024090908862](https://openairdocs.org/sdr/DALA2024090908862.md): Slat Track · corroded · Sep 4, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH #8 SLAT TRACK LOWER FWD I/B HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORMED HFEC OF BLENDED AREA ON TRACK, NO DEFECTS NOTED ALL WORK DONE IAW ANDTP BD500-A-J51-01-20-01AAA-35
- [SDR DALA2024090908859](https://openairdocs.org/sdr/DALA2024090908859.md): Slat Track · corroded · Sep 4, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > LH #7 SLAT TRACK LOWER FWD I/B HAS EVIDENCE OF CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A. REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. PERFORMED HFEC OF BLENDED AREA ON TRACK, NO DEFECTS NOTED ALL WORK DONE IAW ANDTP BD500-A-J51-01-20-01AAA-35
- [SDR DALA2024021302089](https://openairdocs.org/sdr/DALA2024021302089.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195022)
- [SDR DALA2024021302088](https://openairdocs.org/sdr/DALA2024021302088.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195020)
- [SDR DALA2024021302087](https://openairdocs.org/sdr/DALA2024021302087.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195018)
- [SDR DALA2024021302086](https://openairdocs.org/sdr/DALA2024021302086.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195017)
- [SDR DALA2024021302085](https://openairdocs.org/sdr/DALA2024021302085.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195014)
- [SDR DALA2024021302084](https://openairdocs.org/sdr/DALA2024021302084.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195011)
- [SDR DALA2024021302083](https://openairdocs.org/sdr/DALA2024021302083.md): Slat Track · corroded · Feb 10, 2024 · N307DU · 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 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195010)
- [SDR DALA2024021302082](https://openairdocs.org/sdr/DALA2024021302082.md): Slat Track · corroded · Feb 10, 2024 · N307DU · 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 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195007)
- [SDR DALA2024021302081](https://openairdocs.org/sdr/DALA2024021302081.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195006)
- [SDR DALA2024021302080](https://openairdocs.org/sdr/DALA2024021302080.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195005)
- [SDR DALA2024021302079](https://openairdocs.org/sdr/DALA2024021302079.md): Slat Track · corroded · Feb 10, 2024 · N307DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195004)
- [SDR DALA2024021302078](https://openairdocs.org/sdr/DALA2024021302078.md): Slat Track · corroded · Feb 10, 2024 · N307DU · 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 608047- 14AD REV C AND PRI 608047-14AD REV 0 MATCHED. (LP# 0195002)

Next page: https://openairdocs.org/aircraft/N307DU/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 = 'N307DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N307DU/reports

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