# Service difficulty reports: N122DU

A list on [N122DU](https://openairdocs.org/aircraft/N122DU.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 · 75 reports

- [SDR DALA2026052503145](https://openairdocs.org/sdr/DALA2026052503145.md): Power Supply · inoperative · May 24, 2026 · N122DU · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHTS / L 4 AND R 4 DOORS EXTERIOR EMERGENCY LIGHTS OUT. REPLACED AFT LT EXTERIOR EMERGENCY LIGHT PER A220 AMM 33-55, OPS CHECK GOOD. REPLACED EPSU (PS5) PER AMM 33-51. OPS CHECK GOOD. (LP 8382986 - AIRCRAF
- [SDR DALA2026032301954](https://openairdocs.org/sdr/DALA2026032301954.md): B-Nut · loose · Mar 23, 2026 · N122DU · Airbus BD5001A10 · Turbine Engine Oil System
  > DIV- IFSD OF NUMBER 1 ENGINE DUE TO OIL LOSS. CREW REPORTED QUANTITY DROPPED TO 9 QUARTS. FLIGHT MADE AN EMERGENCY LANDING IN DSM. TROUBLESHOT AND FOUND #4 BEARING SCAVENGE TUBE B-NUT LOOSE. CLEANED INSPECTED AND REINSTALLED LINE. PERFORMED WINDMILLING INSPECT
- [SDR DALA2025060504286](https://openairdocs.org/sdr/DALA2025060504286.md): Connector · damaged · May 31, 2025 · N122DU · Airbus BD5001A10 · Equipment/Furnishings Wiring
  > WHILE WORKING ODI LOG #7412850, FOUND FWD GALLEY COFFEE MAKER PIN AND CONNECTOR A4070P1 SOCKET 5 BURNED FROM ARCING. SOCKET 5 AT CONNECTOR A4070P1 IS BURNT AND ELEC CONNECTOR AT POSITION 102 IS DAMAGED DUE TO ARCING. (571824). C/W SECTION 1: TIME LIMITED ALTER
- [SDR DALA2025042203167](https://openairdocs.org/sdr/DALA2025042203167.md): Engine · bird ingestion · Apr 21, 2025 · N122DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > SHIP 8122-DIV- DIVERTED TO AUS DUE TO DIRTY SOCK SMELL. CORRECTIVE ACTION: FOUND EVIDENCE OF BIRD STRIKE NBR 1 ENGINE. C/O ODI PREVENTION WORKCARDS. PERFORMED BOROSCOPE INSPECTION NTF. R/R UPPER BRACKET PER A220 AMP 79-11. PERFORMED ENGINE #1 GASPATH WASH PER
- [SDR DALA2025031201907](https://openairdocs.org/sdr/DALA2025031201907.md): Unknown · odor · Mar 11, 2025 · N122DU · Airbus BD5001A10 · Air Distribution System
  > ODOR IN CABIN AND COCKPIT ON DESCENT INTO LGA. C/W "NO GO ODI" PREVENTION FOR SMOKE AND FUMES IN CABIN 1.PERFORMED T/S TO ISOLATE SMOKE AND FUMES IAW A220 W/C 0550- 2001. NO SMOKE AND FUMES DETECTED ALSO PERFORMED ISOLATE SMOKE AND FUMES APU W/C 0550-2002. NO
- [SDR DALA2025030201590](https://openairdocs.org/sdr/DALA2025030201590.md): Door Sill · corroded · Mar 2, 2025 · N122DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8122, AFT CABIN FLOOR- LT AFT MCD LWR SILL CORRODED AT FR 74 & 76. CORRECTIVE ACTION: REMOVED AND REPLACED LT AFT MCD LWR SILL REF A220 ASRP 51-40-00 AND A220 DWG C01342700. (LP 0836350)
- [SDR DALA2025030201592](https://openairdocs.org/sdr/DALA2025030201592.md): Floor Support · corroded · Mar 1, 2025 · N122DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8122, AFT CABIN FLOOR- RT AFT MCD LWR SILL CORRODED AT FR 76. CORRECTIVE ACTION: COMPLIED WITH ER/A 623665-14 PRI REV 0, REV 1, AND FINAL ER/A 623665-14 REV ORIGINAL SECTION 1. (LP 0836262)
- [SDR DALA2025022801566](https://openairdocs.org/sdr/DALA2025022801566.md): Seat Track · corroded · Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8122, SEAT TRACK CORROSION AT LBL 43.50 AROUND FRAME 20. SSI 53-21-43-02. NO PREVIOUS REWORKING NOTED. CORRECTIVE ACTION: REPAIRED PER ER/A 623171-14TR REV ORIGINAL SECTION 1. (LP 0815756)
- [SDR DALA2025022801565](https://openairdocs.org/sdr/DALA2025022801565.md): Seat Track · corroded · Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8122, AFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 RBL 45. CORRECTIVE ACTION: REPLACED DAMAGED SECTION OF SEAT TRACK PER ER/A 623170-14TR REV ORIGINAL. (LP 0815735)
- [SDR DALA2025022801564](https://openairdocs.org/sdr/DALA2025022801564.md): Seat Track · corroded · Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8122, SEAT TRACK CORROSION AT RBL 43.50 AND FRAME 20. REF SSI 53-21-43-02, NO PREVIOUS REWORK NOTED. CORRECTIVE ACTION: REPLACED DAMAGED SECTION OF SEAT TRACK PER ER/A 623174-14TR REV ORIGINAL. (LP 0815760).
- [SDR DALA2025021801192](https://openairdocs.org/sdr/DALA2025021801192.md): Seat Track · corroded · Feb 14, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 LBL 23. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/003 00424 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-77-00-00 -028A-A AND AIRBUS DRAWING C01342701. (LP# 0811435)
- [SDR DALA2025021101076](https://openairdocs.org/sdr/DALA2025021101076.md): Skin · damaged · Feb 11, 2025 · N122DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LEFT SIDE OF FUSELAGE HAS A SMALL DENT/NICK BETWEEN STR23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0557:2090-2107/002 00406 REPAIRED GOUGE PER ER/A 623625-14 PRI REV 0,REV 1,REV 2, AND ER/A 623625- 14 REV ORIGI
- [SDR DALA2025022701550](https://openairdocs.org/sdr/DALA2025022701550.md): Tail Cone · punctured · Feb 3, 2025 · N122DU · Airbus BD5001A10 · Aerodynamic Fairings
  > AIRCRAFT 8122, WHILE IN HCK VISIT @ MSP MAINTENANCE FOUND A PUNCTURE ON THE (PN C03113040-103) FORWARD UPPER TAIL CONE SKIN. THE PUNCTURE IS LOCATED APPROX. 1.00" AFT OF FR88 AND 3.20" INBD OF STGR1R. THE AREA AROUND THE PUNCTURE ALSO CONTAINS A SMALL DENT REP
- [SDR DALA2025012900704](https://openairdocs.org/sdr/DALA2025012900704.md): Attach Fitting · corroded · Jan 26, 2025 · N122DU · Airbus BD5001A10 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON DOOR THRESHOLD ATTACHMENT LOCATION AFT RH LAV. -P- SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0460:2000-1001/035 00330 REMOVED AND REPLACED DOOR THRESHOLD ATTACHMENT LOCATED AT AFT RH LAV. REF
- [SDR DALA2025012400596](https://openairdocs.org/sdr/DALA2025012400596.md): Seat Track · corroded · Jan 21, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 LBL 43. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/002 00423 REMOVED AND REPLACED SEAT TRACK, REF A220 ASRP 51-77-00. (LP# 0771501)
- [SDR DALA2025012300566](https://openairdocs.org/sdr/DALA2025012300566.md): Seat Track · corroded · Jan 20, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 RBL 23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/004 00425 REMOVED AND REPLACED TRACK PER A220, ASRP 51-77-00. (LP# 0771037)
- [SDR DALA2024102110273](https://openairdocs.org/sdr/DALA2024102110273.md): Link · broken · Oct 15, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT #2 TRACK #4 ATTACHMENT LINK FOUND BROKEN. P/N CO1612553- 001. REMOVED AND REPLACED LH SLAT #2 TRACK #4 ATTACHMENT LINK ON NR008 JOB COMPLETE. (LP# 0610961)
- [SDR DALA2024072607509](https://openairdocs.org/sdr/DALA2024072607509.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0610 UTC. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE PE
- [SDR DALA2024072607508](https://openairdocs.org/sdr/DALA2024072607508.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · 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. LOG-PAGE UPDATED @ 24JUL24 0608 UTC. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE P
- [SDR DALA2024072607507](https://openairdocs.org/sdr/DALA2024072607507.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · 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 FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0606 UTC 02. REPAIRED LH SLAT TRACK NBR 5 LOWER AFT SURFACE
- [SDR DALA2024072607506](https://openairdocs.org/sdr/DALA2024072607506.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 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 @ 24JUL24 0604 UTC 02. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE
- [SDR DALA2024072607505](https://openairdocs.org/sdr/DALA2024072607505.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0601 UTC 02. REPAIRED LH SLAT TRACK NBR 6 UPPER FWD SURFAC
- [SDR DALA2024072607504](https://openairdocs.org/sdr/DALA2024072607504.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0558 UTC 02. REPAIRED LH SLAT TRACK NBR 1 LOWER FWD SURFACE
- [SDR DALA2024072607503](https://openairdocs.org/sdr/DALA2024072607503.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0556 UTC 02. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFAC
- [SDR DALA2024072607502](https://openairdocs.org/sdr/DALA2024072607502.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0551 UTC 02. REPAIRED LH SLAT TRACK NBR 2 LOWER FWD SURFACE
- [SDR DALA2024072607501](https://openairdocs.org/sdr/DALA2024072607501.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0545 UTC 02. REPAIRED LH SLAT TRACK NBR 3 UPPER FWD SURFAC
- [SDR DALA2024072607500](https://openairdocs.org/sdr/DALA2024072607500.md): Slat Track · worn · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT O/B SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0534 UTC 02. MEASURED LH SLAT TRACK NBR 5 UPPER AFT O/B SURF
- [SDR DALA2024072607499](https://openairdocs.org/sdr/DALA2024072607499.md): Slat Track · worn · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD O/B SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0521 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE
- [SDR DALA2024072607498](https://openairdocs.org/sdr/DALA2024072607498.md): Slat Track · worn · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0514 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE PER
- [SDR DALA2024072607497](https://openairdocs.org/sdr/DALA2024072607497.md): Slat Track · worn · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0507 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE PER
- [SDR DALA2024072607496](https://openairdocs.org/sdr/DALA2024072607496.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER 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 @ 24JUL24 0447 UTC 02. REPAIRED LH SLAT TRACK NBR 7 UPPER AFT SURFAC
- [SDR DALA2024072607495](https://openairdocs.org/sdr/DALA2024072607495.md): Slat Track · corroded · Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0439 UTC 02. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD SURFAC
- [SDR DALA2024050204866](https://openairdocs.org/sdr/DALA2024050204866.md): Relay · faulted · May 1, 2024 · N122DU · Airbus BD5001A10 · Landing Gear Position and Warning
  > SHIP 8122 - GEAR - AFTER SELECTING GEAR DOWN, RECEIVED "GEAR FAIL" CAUTION MESSAGE WITH 3 GREEN DOWN AND LOCKED INDICATIONS. CORRECTIVE ACTION: R/R LANDING GEAR RELAY K6. (LP# 5846460)
- [SDR DALA2024042604719](https://openairdocs.org/sdr/DALA2024042604719.md): Slat Track · corroded · Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD 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 1 UPPER FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085
- [SDR DALA2024042604718](https://openairdocs.org/sdr/DALA2024042604718.md): Slat Track · corroded · Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD 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 4 UPPER FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085
- [SDR DALA2024042604717](https://openairdocs.org/sdr/DALA2024042604717.md): Slat Track · corroded · Apr 24, 2024 · N122DU · Airbus BD5001A10 · 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 FLIGHT. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085
- [SDR DALA2024042604716](https://openairdocs.org/sdr/DALA2024042604716.md): Slat Track · corroded · Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD 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 FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085
- [SDR DALA2024042604715](https://openairdocs.org/sdr/DALA2024042604715.md): Slat Track · corroded · Apr 23, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608598- 14AD REV C AND PRI 608598-1
- [SDR DALA2024013001390](https://openairdocs.org/sdr/DALA2024013001390.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H 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 FLT. REPAIRED LH SLAT TRACK NBR 8 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0, 1 M
- [SDR DALA2024013001389](https://openairdocs.org/sdr/DALA2024013001389.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 8 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 8 LOWER FWD I/B SIDE PER ERA 608595- 14AD REV C & PRI REV
- [SDR DALA2024013001388](https://openairdocs.org/sdr/DALA2024013001388.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 7 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 LOWER FWD I/B SIDE PER ERA 608595- 14AD REV C & PRI 0.1
- [SDR DALA2024013001387](https://openairdocs.org/sdr/DALA2024013001387.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 10 LOWER FWD OUTBOARD SIDE 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 10 LOWER FWD O/B SIDE PER ERA 608595- 14AD REV C & PRI 0
- [SDR DALA2024013001386](https://openairdocs.org/sdr/DALA2024013001386.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 UPPER AFT OUTBOARD SIDE 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 10 UPPER AFT O/B SIDE PER ERA 608595- 17AD REV C & PRI RE
- [SDR DALA2024013001385](https://openairdocs.org/sdr/DALA2024013001385.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 10 UPPER FWD 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 10 UPPER FWD SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1
- [SDR DALA2024013001384](https://openairdocs.org/sdr/DALA2024013001384.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OR CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1 MAT
- [SDR DALA2024013001382](https://openairdocs.org/sdr/DALA2024013001382.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 3 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1 MA
- [SDR DALA2024013001379](https://openairdocs.org/sdr/DALA2024013001379.md): Slat Track · corroded · Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OR CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 3 LOWER FWD O/B SIDE PER ERA 608595- 14AD REV C & PRI 0.1
- [SDR DALA2024013001377](https://openairdocs.org/sdr/DALA2024013001377.md): Slat Track · corroded · Jan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR MARKS IN TWO SEPARATE LOCATIONS AND PREVIOUS REWORK REF 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 4 LOWER AFT SURFACE PER ERA 608595-
- [SDR DALA2024012901269](https://openairdocs.org/sdr/DALA2024012901269.md): Slat Track · corroded · Jan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 5 UPPER AFT OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 5 UPPER AFT OUTBOARD SIDE PER ER/A 608595-14AD REV C AND
- [SDR DALA2024012901268](https://openairdocs.org/sdr/DALA2024012901268.md): Slat Track · corroded · Jan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FWD INBOARD SIDE HAS EVIDENCE OF A WEAR MARK AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 6 LOWER FWD INBOARD SIDE PER ER/A 608595-14AD REV C AND

Next page: https://openairdocs.org/aircraft/N122DU/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 = 'N122DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N122DU/reports

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