# Service difficulty reports: N116DU

A list on [N116DU](https://openairdocs.org/aircraft/N116DU.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 · 56 reports

- [SDR DALA2025052704035](https://openairdocs.org/sdr/DALA2025052704035.md): Skin · corroded · May 20, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION EXTERNAL SKIN FR 34 + 12" STR 36L-36R (MARKED). COMPLIED WITH ER/A 626424-14 REV ORIGINAL SECTION I. REFERENCE LOG PAGE 0976835 FOR SERVICE LIMIT OF REPAIR. ASSOCIATED ER/A 14-626424 ADDED FOR AC 8116. (LP# 0976879)
- [SDR DALA2025052704032](https://openairdocs.org/sdr/DALA2025052704032.md): Panel · corroded · May 20, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Structure
  > TOILET SERVICE DOOR PAN LOWER AFT EDGE HAS EVIDENCE OF CORROSION FR76 BETWEEN STR 32L 33L. COMPLIED WITH ER/A 601355-14AD REV A ASSOCIATED ER/A 14-601355 ADDED FOR AC 8116. (LP# 0977029)
- [SDR DALA2025052003864](https://openairdocs.org/sdr/DALA2025052003864.md): Floor Support · corroded · May 16, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** INTERCOASTAL BETWEEN FROM 80 AND FR 81 LBL 17 CORROSION FOUND UPPER SURFACE. REMOVED AND REPLACED INTERCOASTAL BETWEEN FR 81 AND FR 80 LBL 17 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG PL C01401201 REV:-R
- [SDR DALA2025052003862](https://openairdocs.org/sdr/DALA2025052003862.md): Pan · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Structure
  > ***CORROSION*** WHILE WORKING MONITOR 2362838 CORROSION WAS FOUND ON EXTERIOR SURFACE OF WASTE BOX LAV PAN. REMOVED REPLACED AND INSTALLED NEW WASTE BOX IAW BOMBARDIER DWG C01342100 REV T AND A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP# 0968350)
- [SDR DALA2025052003861](https://openairdocs.org/sdr/DALA2025052003861.md): Door · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fluid Service Doors
  > ***CORROSION*** WHILE WORKING MONITOR 2362838 CORROSION WAS FOUND ON WASTE SERVICE DOOR INTERIOR SURFACE AROUND LATCHES. REMOVED AND REPLACED WASTE SERVICE DOOR ASSEMBLY PER A220 AMP BD500- A-J52-47-06-05AAA-720A-A. (LP# 0968291)
- [SDR DALA2025052003860](https://openairdocs.org/sdr/DALA2025052003860.md): Floor Support · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** MULTIPLE AREAS ON LBL-3, FR 79-80 (MARKED). REMOVED AND REPLACED INTERCOASTAL BETWEEN FR79-80 LBL 3 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV -R. (LP# 0968267)
- [SDR DALA2025052003859](https://openairdocs.org/sdr/DALA2025052003859.md): Floor Support · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** MULTIPLE AREAS ON AT RBL 3, FR 79-80 (MARKED). REMOVED AND REPLACED INTERCOASTAL BETWEEN FR79-80 RBL 3 PER ASRP A220 BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV -R. (LP# 0968258)
- [SDR DALA2025052003857](https://openairdocs.org/sdr/DALA2025052003857.md): Floor Support · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT EQUIPMENT BAY INTERCOASTAL FR 80-81 RBL 8 HAS CORROSION. REMOVED AND REPLACED INTERCOASTAL ON AFT EQUIPMENT BAY AT FR80-81 RBL 8 PER ASRP A220 BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV -R. (LP# 0967685)
- [SDR DALA2025052003856](https://openairdocs.org/sdr/DALA2025052003856.md): Floor Support · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT EQUIPMENT BAY INTERCOASTAL FR 80-81 LBL 8 HAS CORROSION. REMOVED AND REPLACED INTERCOASTAL ON AFT EQUIPMENT BAY AT FR80- 811 LBL 8 PER ASRP A220 BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV -R. (LP# 0967676)
- [SDR DALA2025052003855](https://openairdocs.org/sdr/DALA2025052003855.md): Door Sill · corroded · May 15, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Structure
  > ***CORROSION*** FWD CARGO COMPARTMENT DOOR LOWER SILL HAS MULTIPLE SPOTS OF CORROSION SSI 53- 21-25-02. REMOVED AND REPLACED LOWER SILL IAW A200 ASRP BD500-A-J51-42-21- 00AAA-078-A, BOMBARDIER DWG C02314100 REG G AND ER/A 626163-14 REV ORG ASSOCIATED ER/A 14-6
- [SDR DALA2025051503770](https://openairdocs.org/sdr/DALA2025051503770.md): Frame · corroded · May 13, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Frame
  > ***CORROSION*** ON FR81, AREA FWD OF AFT EQUIPMENT BAY ACCESS DOOR, BTW LBL16 TO RBL6. REMOVED AND REPLACED FRAME ON FR81 BETWEEN STRINGER 18L TO 17R PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01409001 REV -D. (LP# 0964104)
- [SDR DALA2025051503769](https://openairdocs.org/sdr/DALA2025051503769.md): Floor Support · corroded · May 13, 2025 · N116DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** INTERCOASTAL BETWEEN FROM 80 AND FR 81 RBL 17 CORROSION FOUND UPPER SURFACE. REMOVED AND REPLACED INTERCOASTAL BETWEEN FROM FR80 AND FR81 RBL 17 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV- R. (LP# 0964096)
- [SDR DALA2025051403743](https://openairdocs.org/sdr/DALA2025051403743.md): Floor Panel · corroded · May 10, 2025 · N116DU · Airbus BD5001A10 · Fuselage Floor Panel
  > ***CORROSION*** ON FSD ENTRY FLOOR PANEL 222KRF, INBOARD AND AFT EDGES. REMOVED ENTRY FLOOR PANEL 222KRF AND INSTALLED A NEW ENTRY FLOOR PANEL PER A220 AMP BD500-A-J53-00-47-12AAA-720A-A AND A220 AMP BD500-A-J53-00-47-12AAA-520A-A. (LP# 0958911)
- [SDR DALA2025051303712](https://openairdocs.org/sdr/DALA2025051303712.md): Frame · corroded · May 8, 2025 · N116DU · Airbus BD5001A10 · Fuselage Main, Frame
  > CORROSION, MULTIPLE AREAS ON FR80, STR 15L- 19L (MARKED). REMOVED AND REPLACED FRAME SECTION ON FR80 STR 15L TO 19L PER A220 ASRP BD500-A-J51-42-21-00AA-078A-A AND BOMBARDIER DWG C01409001 REV-D. REMOVED AND REPLACED FRAME SECTION ON FR80 STR 15L TO 19L PER A2
- [SDR DALA2025050603474](https://openairdocs.org/sdr/DALA2025050603474.md): Seat Track · corroded · May 2, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON FWD END OF SEAT TRACK @ FR20, RBL43, WL151. REMOVED CORROSION AND EVALUATED OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK AT RBL 43 WL 151 FROM FR20 TO 30+9" IAW A220 ASRP BD500-A-51-42-21-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV E. (L
- [SDR DALA2025050603472](https://openairdocs.org/sdr/DALA2025050603472.md): Seat Track · corroded · May 2, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON PASSENGER SEAT TRACK AT FR 74 LBL 23 WL 147 ( MARKED). SSI 53-61-43-02. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 61 TO FR 74, LBL 23, WL 147 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG: C01342701, REV: G. (LP# 0944447)
- [SDR DALA2025050603471](https://openairdocs.org/sdr/DALA2025050603471.md): Cargo Track · corroded · May 2, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON PASSENGER SEAT TRACK AT FR 74 RBL 43.5 WL 147 (MARKED). SSI 53-61-43-02. REMOVED AND REPLACED SEAT TRACK AT RBL 43.5 BTW FR 62 AND FR 74 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV G. C CRUZ 2553675U 01/MAY
- [SDR DALA2025050103371](https://openairdocs.org/sdr/DALA2025050103371.md): Seat Track · corroded · Apr 29, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON PASSENGER SEAT TRACK AT FR 74 RBL 23 WL 147 ( MARKED). SSI 53-61-43-02. REMOVED AND REPLACED SEAT TRACK FROM FR 61 TO FR 74 RBL 23 WL 147 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG BOMBARDIER PL C01342701 REV E. (LP# 0939741)
- [SDR DALA2025050103370](https://openairdocs.org/sdr/DALA2025050103370.md): Floor Panel · corroded · Apr 28, 2025 · N116DU · Airbus BD5001A10 · Fuselage Floor Panel
  > ***CORROSION*** ON FPD ENTRY FLOOR PANEL 221 KLF, INBOARD AND AFT EDGES. REMOVED DAMAGED FWD PASSENGER ENTRY FLOOR PANEL 221 KLF AND REPLACED (INSTALLED) PER A220 AMP BD500-A-J53-00-47-11AAA-720A-A STEP 1. (LP# 0938167)
- [SDR DALA2025043003328](https://openairdocs.org/sdr/DALA2025043003328.md): Seat Track · corroded · Apr 26, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON FWD END OF SEAT TRACK @ FR20, RBL23, WL151. REMOVED AND REPLACED SEAT TRACK BETWEEN FR19+9" TO FR 30+9" RBL 23 WL 151 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV E. (LP# 0934712)
- [SDR DALA2025043003329](https://openairdocs.org/sdr/DALA2025043003329.md): Seat Track · corroded · Apr 25, 2025 · N116DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON PASSENGER SEAT TRACK AT FR 74 LBL 43.5 WL 147 (MARKED). REMOVED AND REPLACED SEAT TRACK FROM FR 61 TO FR 74 BETWEEN LBL 43.5 WL 147 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG PL C01342701 REV G. (LP# 0934722)
- [SDR DALA2025032502214](https://openairdocs.org/sdr/DALA2025032502214.md): Oven · odor · Mar 20, 2025 · N116DU · Airbus BD5001A10 · Buffet/Galleys
  > FUMES SMELLED ON FLIGHT DECK AND FWD GALLEY AFTER APU STARTED. DISSIPATED AFTER C/L C/W. C/W AMDS W/C 0550-2001(362513) NO FUMES OR SMELL NOTED. C/W W/ C0550-2003- NO ITEMS. C/W A220 EFIM ELIMINATION OF RESIDUAL ODORS 2HR. ENG RUNS- NO ODORS. OK FOR SVC, REF.
- [SDR DALA2025021301122](https://openairdocs.org/sdr/DALA2025021301122.md): Slat Track · corroded · Feb 12, 2025 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 TEETH (1 EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ER/A 62458-14AD REV ORIGINAL AND PRI 624258-14AD REV 0 MATCHES. (LP# 0808277)
- [SDR DALA2024082208372](https://openairdocs.org/sdr/DALA2024082208372.md): Warning Message · illuminated · Aug 22, 2024 · N116DU · Airbus BD5001A10 · Landing Gear Brake System
  > SHIP 8116 - MISC - DECLARED EMERGENCY DUE TO "BRAKE ON" CAUTION MESSAGE. CORRECTIVE ACTION: DOWNLOADED NON-VOLATILE MEMORY FROM THE BRAKE DATA CONCENTRATOR UNITS (BDCU) AND REPLACED ELECTRIC MOTOR CONTROL UNIT (EMCU) 3. (LP# 5741338)
- [SDR DALA2024062406366](https://openairdocs.org/sdr/DALA2024062406366.md): Slat Track · damaged · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 9 LOWER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP# 04083
- [SDR DALA2024062406365](https://openairdocs.org/sdr/DALA2024062406365.md): Slat Track · damaged · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 7 LOWER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP# 04083
- [SDR DALA2024062406364](https://openairdocs.org/sdr/DALA2024062406364.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD IN 2 LOCATIONS HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD IN 2 LOCATIONS PER ER/A 606807-14AD REV C AND PRI REV 0 M
- [SDR DALA2024062406363](https://openairdocs.org/sdr/DALA2024062406363.md): Slat Track · corroded · Jun 23, 2024 · N116DU · 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 REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP#
- [SDR DALA2024062406362](https://openairdocs.org/sdr/DALA2024062406362.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP#
- [SDR DALA2024062406361](https://openairdocs.org/sdr/DALA2024062406361.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE SURFACE PER ER/A 606807-14AD REV C AND PRI REV
- [SDR DALA2024062406360](https://openairdocs.org/sdr/DALA2024062406360.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE PER ER/A 606806- 14AD, REV C AND PRI REV 0 MATCH
- [SDR DALA2024062406359](https://openairdocs.org/sdr/DALA2024062406359.md): Slat Track · corroded · Jun 23, 2024 · N116DU · 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 REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP#
- [SDR DALA2024062406358](https://openairdocs.org/sdr/DALA2024062406358.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 1 LOWER AFT SURFACE PER ER/A 606806-14AD, REV C AND PRI REV 0 MATCHE
- [SDR DALA2024062406357](https://openairdocs.org/sdr/DALA2024062406357.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 8 LOWER FWD SURFACE PER ER/A 606806-14AD, REV C AND PRI REV 0 MATCHE
- [SDR DALA2024062406356](https://openairdocs.org/sdr/DALA2024062406356.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP# 0408316)
- [SDR DALA2024062406355](https://openairdocs.org/sdr/DALA2024062406355.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE PER ER/A 606806-14AD, REV C AND PRI REV 0 MATCHE
- [SDR DALA2024062406354](https://openairdocs.org/sdr/DALA2024062406354.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 LOWER AFT SURFACE PER ER/A 606807-14AD REV C AND PRI REV 0 MATCHED. (LP# 040831
- [SDR DALA2024062406353](https://openairdocs.org/sdr/DALA2024062406353.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD SURFACE PER ER/A 606806- 14AD, REV C AND PRI REV 0 MATCH
- [SDR DALA2024062406352](https://openairdocs.org/sdr/DALA2024062406352.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE PER ER/A 606806-14AD, REV C AND PRI REV 0 MATCHE
- [SDR DALA2024062406351](https://openairdocs.org/sdr/DALA2024062406351.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NB2 UPPER AFT SURFACE PER ER/A 606806- 14AD, REV C AND PRI REV 0 MATCHED
- [SDR DALA2024062406350](https://openairdocs.org/sdr/DALA2024062406350.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 1 UPPER AFT SURFACE PER ER/A 606807- 14AD REV C AND PRI REV 0 MATCHED. (LP# 04083
- [SDR DALA2024062406349](https://openairdocs.org/sdr/DALA2024062406349.md): Slat Track · corroded · Jun 23, 2024 · N116DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE PER ER/A 606806- 14AD, REV C AND PRI REV 0 MATCH
- [SDR DALA2023092607921](https://openairdocs.org/sdr/DALA2023092607921.md): Unknown · unknown · Sep 20, 2023 · N116DU · Bombdr BD1001A10 · Engine Bleed Air System
  > SHIP 8116 MISC/DE - AT TOP OF DECENT FL310, CREW RECEIVED LEFT BLEED FAIL, AT FL150, CREW RECEIVED LEFT WING ANT-ICE FAIL IN ICING CONDITIONS. AND AT FL100 AIRCRAFT WAS STRUCK BY LIGHTNING. EMERGENCY WAS DECLARED. CORRECTIVE ACTION: T/S PER FAULT CODE 3611F000
- [SDR DALA2023031401868](https://openairdocs.org/sdr/DALA2023031401868.md): None · none · Mar 12, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH WING: SLAT TRACK #8 HAS CORROSION ON BOTTOM. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 080-0001:5742-01028-02B/006 00021 CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 5742-0102
- [SDR DALA2023031401867](https://openairdocs.org/sdr/DALA2023031401867.md): None · none · Mar 12, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH WING: SLAT TRACK #6 HAS CORROSION ON BOTTOM. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 080-0001:5742-01028-02B/004 00019 CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 5742-0102
- [SDR DALA2023031401866](https://openairdocs.org/sdr/DALA2023031401866.md): None · none · Mar 11, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH WING: SLAT TRACK #5 HAS CORROSION ON BOTTOM. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 080-0001:5742-01028-02B/003 00018 CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 5742-0102
- [SDR DALA2023031401870](https://openairdocs.org/sdr/DALA2023031401870.md): None · none · Mar 10, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH WING: SLAT TRACK #11 HAS CORROSION ON BOTTOM. NO EVIDENCE OF PREVIOUS REWORK. CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 057-0001:5742 -01028-02A. MAX MATERIAL REMOVED IS.002 ORIGINAL THICKNESS TAPERS FROM.232 TO.230 SEE AMDS FOR MORE INFORMATION
- [SDR DALA2023031401865](https://openairdocs.org/sdr/DALA2023031401865.md): None · none · Mar 9, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH WING: SLAT TRACK #9 HAS CORROSION ON BOTTOM TOP. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 079-0001:5742-01028-02A/004 00011 CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 057-0
- [SDR DALA2023031401864](https://openairdocs.org/sdr/DALA2023031401864.md): None · none · Mar 9, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH WING: SLAT TRACK #4 HAS CORROSION ON GEAR. NO EVIDENCE OF PREVIOUS REWORK. SEE N/R 12 WORK PACKAGE #P103854220230228 FOR DETAILS. CLEANED AND INSPECTED SLAT TRACK #4 GEAR PER AMDS CARD 057-0001:5742- 01028-02A. (LP#2662650).
- [SDR DALA2023031401863](https://openairdocs.org/sdr/DALA2023031401863.md): None · none · Mar 9, 2023 · N116DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH WING: SLAT TRACK #6 HAS CORROSION ON TOP AND BOTTOM. NO EVIDENCE OF PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 079-0001:5742-01028-02A/002 00009 CLEANED AND REPAIRED CORROSION AREAS PER AMDS CARD 0

Next page: https://openairdocs.org/aircraft/N116DU/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 = 'N116DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N116DU/reports

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