# Service difficulty reports: N114DU

A list on [N114DU](https://openairdocs.org/aircraft/N114DU.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 · 63 reports

- [SDR DALA2026032501999](https://openairdocs.org/sdr/DALA2026032501999.md): Duct · blown · Mar 20, 2026 · N114DU · Airbus BD5001A10 · Air Distribution System
  > APU BLEED LEAK MSG WITH ODOR. STEP 1-T/S AND FOUND APU DUCT BLOWN IAW AND WORKCARD 0550-2001. STEP 2 P-TRAK SNIFFER NOT AVAILABLE STEP 3 FOUND SOURCE TO BE APU BLEED DUCT(P.AUTAR 631639) STEP 4 N/A DUE TO SOURCE BEING BLOWN APU DUCT. REMOVED & REPLACED DUCTS P
- [SDR DALA2025052103922](https://openairdocs.org/sdr/DALA2025052103922.md): Light · inoperative · May 18, 2025 · N114DU · Airbus BD5001A10 · Emergency Lighting
  > FOUND 2 EA REAR BARREL EXTERNAL EMERGENCY LIGHTS INOP AND FWD SVC DOOR RH. REMOVED SEAT 1CD PER A220 AMP 25-21-01. REMOVED RH FWD 1CD SIDEWALL PANEL PER A220 AMP 25-29-01. REMOVED RH FWD 1CD DADO PANEL PER A220 AMP 25-29-02. REMOVED LH AFT 28BA SEAT PER A220 A
- [SDR DALA2024102810435](https://openairdocs.org/sdr/DALA2024102810435.md): Proximity Sensor · out of tolerance · Oct 27, 2024 · N114DU · Airbus BD5001A10 · Landing Gear Position and Warning
  > SHIP 8114 - ATB - DUE TO GEAR NOT RETRACTING. CORRECTIVE ACTION: FOUND BOTH PROX SENSORS OUT OF TOLERENCE. RE-RIGGED PROX SENSORS MT157 & MT158. OPS CHECK GOOD. (LP# 4474970)
- [SDR DALA2024102810432](https://openairdocs.org/sdr/DALA2024102810432.md): Doubler · corroded · Oct 24, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION AROUND FASTENERS HOLES OF 2 WASTE BOX DOUBLER FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/004 00468 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 5987
- [SDR DALA2024102810431](https://openairdocs.org/sdr/DALA2024102810431.md): Doubler · corroded · Oct 24, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WASTE BOX DOUBLER HAS MULTIPLE AREAS OF CORROSION AT I/B FWD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/005 00469 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 59
- [SDR DALA2024102810430](https://openairdocs.org/sdr/DALA2024102810430.md): Structure · corroded · Oct 24, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WASTE BOX AREA OF CORROSION AFT OF LIGHT ELECTRICAL CONNECTOR. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/006 00470 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 598701-1
- [SDR DALA2024102810429](https://openairdocs.org/sdr/DALA2024102810429.md): Hinge · corroded · Oct 24, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Door Hinge
  > WASTE SERVICE PANEL I/B HINGE HAS MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/003 00467 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 598701-1
- [SDR DALA2024102810428](https://openairdocs.org/sdr/DALA2024102810428.md): Waste Box · corroded · Oct 24, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WASTE BOX, INTERIOR SIDE HAS MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0509:2090-2023/003 00464 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 598701-14AD R
- [SDR DALA2024102110272](https://openairdocs.org/sdr/DALA2024102110272.md): Longeron · corroded · Oct 15, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Longeron/Stringer
  > WTBF LH LONGERON CORRODED AT FWD END, 2" AFT OF FR 48. REPLACED LONGERON REF A220 ASRP 53-82-55 AND 51-42-21. (LP# 0610773)
- [SDR DALA2024101510105](https://openairdocs.org/sdr/DALA2024101510105.md): Skin · corroded · Oct 14, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERIOR OF FUSELAGE JUST FORWARD OF AFT PRESSURE BULKHEAD FRAME 79 BETWEEN STRINGER 36L AND 35L.-M- SEE ATTACHED PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 143-0001:5300-2110/001 00426 ER/A 620821
- [SDR DALA2024101109975](https://openairdocs.org/sdr/DALA2024101109975.md): Frame · cracked · Oct 9, 2024 · N114DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT SERVICE DOOR LOWER SCUFF PLATE HOLE 3 OUTER LOWER HAS CORROSION. PIC ATTACHED. AA 5331-01297-02B. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 094-0001:5331-01297-02B/002 00355 SUMMARY - WP: 630411 - LAVALLE, GARY -
- [SDR DALA2024101109973](https://openairdocs.org/sdr/DALA2024101109973.md): Scuff Plate · corroded · Oct 9, 2024 · N114DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT SERVICE DOOR LOWER SCUFF PLATE HOLE 7 OUTER LOWER HAS CORROSION. PIC ATTACHED. AA 5331-01297-02B. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 094-0001:5331-01297-02B/005 00358 SUMMARY - WP: 630411 -: REMOVED CORRO
- [SDR DALA2024101109972](https://openairdocs.org/sdr/DALA2024101109972.md): Scuff Plate · corroded · Oct 9, 2024 · N114DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT SERVICE DOOR LOWER SCUFF PLATE HOLE 4 OUTER LOWER HAS CORROSION. PIC ATTACHED. AA 5331-01297-02B. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 094-0001:5331-01297-02B/003 00356 SUMMARY - WP: 630411 - LAVALLE, GARY -
- [SDR DALA2024101109971](https://openairdocs.org/sdr/DALA2024101109971.md): Floor Support · corroded · Oct 9, 2024 · N114DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE INTERCOSTAL 12" FORWARD OF FR15 AND AT RBL 28 HAS CORROSION AROUND FASTENER HOLE. -M-. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0474:5311-2016/004 00448 COMPLIED WITH ER/A 620912-14 PRI REV 0, E
- [SDR DALA2024100809788](https://openairdocs.org/sdr/DALA2024100809788.md): Seat Track · corroded · Oct 5, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD PASSENGER AREA SEAT TRACK FR20 TO 4" FWD AND AT RBL 23 CORRODED. SSI: 53-21-43-01. NO BLUE PAINT NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0558:5321-2021/005 00452 REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-11. SUMMARY SEE NR FOR ADDITIONAL
- [SDR DALA2024100809771](https://openairdocs.org/sdr/DALA2024100809771.md): Seat Track · corroded · Oct 4, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 43 IS CORRODED BETWEEN FR69-70 AND 72-74. REF SSI:53-61-43-01, NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5300-2015/002 00458 REPLACED SEAT TRACK PER A220 ASRP 51-4
- [SDR DALA2024100809773](https://openairdocs.org/sdr/DALA2024100809773.md): Seat Track · corroded · Oct 3, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 43 IS CORRODED AT FR70 AND 74. REF SSI:53-61- 43-01, NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5300-2015/005 00461 REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-42-00. (LP# 0590872)
- [SDR DALA2024100809772](https://openairdocs.org/sdr/DALA2024100809772.md): Seat Track · corroded · Oct 3, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 23 IS CORRODED AT FR74. REF SSI:53-61-43-01, NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5300-2015/004 00460 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 53-61-49- 00AAA-041A-A ITEM 2 AND A220 DWG C01342701.
- [SDR DALA2024100309652](https://openairdocs.org/sdr/DALA2024100309652.md): Seat Track · corroded · Oct 2, 2024 · N114DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 23 IS CORRODED BETWEEN FR71-74. REF SSI:53-61- 43-01, NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5300-2015/003 00459 REMOVED AND REPLACED TRACK REF A220 ASRP 51-42-
- [SDR DALA2025040302525](https://openairdocs.org/sdr/DALA2025040302525.md): Door Frame · corroded · Oct 1, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT EQUIPMENT DOOR FWD FRAME FR81 ON AFT SIDE HAS CORROSION ON VERTICAL FLANGE. REMOVED AND REPLACED FRAME 81 LOWER CENTER SECTION, REF BOMBARDIER DWG C01401201. REMOVED AND REPLACED FRAME 81 LOWER CENTER SECTION, REF BOMBARDIER DWG C01401201. SCEPTRE LOG PAGE
- [SDR DALA2024092509405](https://openairdocs.org/sdr/DALA2024092509405.md): Scuff Plate · corroded · Sep 23, 2024 · N114DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8114, AFT SERVICE DOOR LOWER SCUFF PLATE HOLE 5 OUTER LOWER HAS CORROSION. PIC ATTACHED. AA 5331-01297-02B. CORRECTIVE ACTION: REMOVED CORROSION BY COUNTERSINKING TO DIAMETER OF 0.346 INCHES PER TASK CARD 5331-01297-02B. (LP 0572469)
- [SDR DALA2024071207062](https://openairdocs.org/sdr/DALA2024071207062.md): Longeron · cracked · Jul 9, 2024 · N114DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WHILE WORKING W/C 5352-01038-01A FOUND R/H LONGERON AT RBL40 4" CRACK AT TIE ROD. PULLED R/A C/B FOR RA 1/2/3. REMOVED PANEL 195GB AND REMOVED R/H LONGERON PER A220 AMM 53-82.(548551) REINSTALLED LONGERON PER WORKCARD 53-52-01038-07B. R/A ANTENNAS RECONNECTED
- [SDR DALA2024022702739](https://openairdocs.org/sdr/DALA2024022702739.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 UPPER AFT OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 UPPER AFT OB SIDE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219859)
- [SDR DALA2024022702738](https://openairdocs.org/sdr/DALA2024022702738.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 LOWER FWD IB SIDE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219855)
- [SDR DALA2024022702737](https://openairdocs.org/sdr/DALA2024022702737.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219854)
- [SDR DALA2024022702736](https://openairdocs.org/sdr/DALA2024022702736.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 UPPER FWD SURFACE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219853)
- [SDR DALA2024022702735](https://openairdocs.org/sdr/DALA2024022702735.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 UPPER AFT SURFACE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219849)
- [SDR DALA2024022702734](https://openairdocs.org/sdr/DALA2024022702734.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER AFT SURFACE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219848)
- [SDR DALA2024022702733](https://openairdocs.org/sdr/DALA2024022702733.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219846)
- [SDR DALA2024022702732](https://openairdocs.org/sdr/DALA2024022702732.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED. (LP# 0219844)
- [SDR DALA2024022702731](https://openairdocs.org/sdr/DALA2024022702731.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD I/B SIDE IAW ER/A 607380- 14AD REV D AND PRI 607380-14AD REV 0 MATCHED.
- [SDR DALA2024022702730](https://openairdocs.org/sdr/DALA2024022702730.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 10 UPPER FWD SURFACE IAW ER/A 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218539)
- [SDR DALA2024022702729](https://openairdocs.org/sdr/DALA2024022702729.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 26FEB24 0147 UTC 02 CORR BY COBB 01831429 IAH 26FEB24 ATA 5742 RII: N
- [SDR DALA2024022702728](https://openairdocs.org/sdr/DALA2024022702728.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · 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 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218536)
- [SDR DALA2024022702727](https://openairdocs.org/sdr/DALA2024022702727.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · 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 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP3 0218535)
- [SDR DALA2024022702726](https://openairdocs.org/sdr/DALA2024022702726.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 LOWER AFT SURFACE IAW ER/A 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218532)
- [SDR DALA2024022702725](https://openairdocs.org/sdr/DALA2024022702725.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218530)
- [SDR DALA2024022702724](https://openairdocs.org/sdr/DALA2024022702724.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · 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 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218528)
- [SDR DALA2024022702723](https://openairdocs.org/sdr/DALA2024022702723.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · 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 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218521)
- [SDR DALA2024022702722](https://openairdocs.org/sdr/DALA2024022702722.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IN 2 LOCATIONS IAW ER/A 607379-14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218514)
- [SDR DALA2024022702721](https://openairdocs.org/sdr/DALA2024022702721.md): Slat Track · corroded · Feb 26, 2024 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 LOWER AFT SURFACE IAW ER/A 607379- 14AD REV D AND PRI 607379-14AD REV 0 MATCHED. (LP# 0218510)
- [SDR DALA2024021302104](https://openairdocs.org/sdr/DALA2024021302104.md): Slide · faulty · Feb 9, 2024 · N114DU · Airbus BD5001A10 · Escape Slide
  > WING SLIDE CAUTION - RT WING SLIDE. T/S PER A220 EFIM SOLUTION # 2-29570. R/R RT OWEED SLIDE PER WORKCARD 2563-4005. NO ACTIVE FAULTS AT THIS TIME. NO "M" PROCEDURES TO REVERSE, PLACARDS REMOVED. OK FOR SVC. RII C/W 855718 (LP# 4885170)
- [SDR DALA2023121810325](https://openairdocs.org/sdr/DALA2023121810325.md): Unknown · unknown · Dec 15, 2023 · N114DU · Airbus BD5001A10 · Aircraft Fuel System
  > SHIP 8114 - DIV - TO BWI DUE TO "FUEL COLLECTOR LO LVL" MESSAGE. CORRECTIVE ACTION: R/R LT REMOTE DATA CONCENTRATOR. (LP# 4279272)
- [SDR DALA2023120710015](https://openairdocs.org/sdr/DALA2023120710015.md): Unknown · unknown · Dec 7, 2023 · N114DU · Airbus BD5001A10 · Emergency Lighting
  > FOUND FWD SERVICE DOOR EMERGENCY OVERHEAD LIGHT LENS MISSING DURING SVC CHK. REPLACED FSD OVERHEAD EMERGENCY LIGHT LENS PER A220 AMP 52-02. (LP# 4279250)
- [SDR DALA2023091807652](https://openairdocs.org/sdr/DALA2023091807652.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #11 HAS DAMAGE ON LOWER AFT SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/006 00009 ACCOMPLISHED ER/A 607380-14AD REV B PRI REV 0 AND F
- [SDR DALA2023091807651](https://openairdocs.org/sdr/DALA2023091807651.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #8 HAS CORROSION ON LOWER SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/005 00008 ACCOMPLISHED ER/A 607380-14AD REV B PRI REV 0 AND FIN
- [SDR DALA2023091807650](https://openairdocs.org/sdr/DALA2023091807650.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #5 HAS CORROSION ON UPPER AND LOWER SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/004 00007 ACCOMPLISHED ER/A 607380-14AD REV B PRI REV
- [SDR DALA2023091807649](https://openairdocs.org/sdr/DALA2023091807649.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #4 HAS CORROSION ON UPPER SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/003 00006 ACCOMPLISHED ER/A 607380-14AD REV B PRI REV 0 AND FIN
- [SDR DALA2023091807648](https://openairdocs.org/sdr/DALA2023091807648.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #3 HAS DAMAGE ON LOWER AFT SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/002 00005 ACCOMPLISHED ER/A 607380-14AD REV B PRI REV 0 AND FI
- [SDR DALA2023091807647](https://openairdocs.org/sdr/DALA2023091807647.md): Unknown · unknown · Sep 16, 2023 · N114DU · Airbus BD5001A10 · Leading Edge Devices
  > LT WING SLAT TRACK #1 HAS CORROSION AND DAMAGE ON LOWER AFT SURFACE WITH EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/001 00004 ACCOMPLISHED ER/A 607380-14AD REV B PR

Next page: https://openairdocs.org/aircraft/N114DU/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 = 'N114DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N114DU/reports

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