# Service difficulty reports: N310DU

A list on [N310DU](https://openairdocs.org/aircraft/N310DU.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 · 59 reports

- [SDR DALA2026100705542](https://openairdocs.org/sdr/DALA2026100705542.md): Floor Panel · corroded · Oct 5, 2026 · N310DU · Airbus BD5001A11 · Fuselage Floor Panel
  > R1 DOOR FLOOR PANEL# 222KRF HAS CORROSION. REMOVED AND REPLACED R1 DOOR FLOOR PANEL# 222KRF IAW A220 AMP BD500-A-J53-00-47-12AAA-520A-A AND A220 AMP BD500-A-J53-00-47- 12AAA-720A-A. (LP# 1850064; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100705539](https://openairdocs.org/sdr/DALA2026100705539.md): Floor Support · corroded · Oct 3, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR20, RBL 33 HAS CORROSION. REPLACED FLOOR SUPPORT AT PASSENGER CABIN FR20, RBL33 FOR A SERVICEABLE PART PER ASRP BD500-A-J51-42-21- 00AAA-078A-A. (LP# 1846196; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505498](https://openairdocs.org/sdr/DALA2026100505498.md): Bracket · corroded · Sep 30, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION G4 BRACKET AT LBL 1, FR 76-78 HAS CORROSION (MARKED). C/W ER/A 637185-14 REV ORIGINAL ASSOCIATED ER/A 14-637185 ADDED FOR AC 8310. (LP# 1840747; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505497](https://openairdocs.org/sdr/DALA2026100505497.md): Frame · corroded · Sep 29, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Frame
  > CORROSION, SECTION 48 FRAME HAS EVIDENCE OF CORROSION AT FR 81 STGR 19L. REMOVED AND REPLACED CENTER SECTION FRAME AT FR 81 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG: C01401201 REV:-R. (LP# 1839389; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005435](https://openairdocs.org/sdr/DALA2026093005435.md): Web · corroded · Sep 28, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > AFT OF R2 DOOR, FLOOR STRUCTURE WEB HAS CORROSION AT FR 76-79. REMOVED AND REPLACED FLOOR STRUCTURE WEB AFT OF R2 DOOR BETWEEN FR 76-79 IAW A220 ASRP BD500-A-J51-41-02-00AAA-078A-A AND DWG C01342700 REV T. (LP# 1837447; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005433](https://openairdocs.org/sdr/DALA2026093005433.md): Seat Track · corroded · Sep 26, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > RT INBOARD SEAT TRACK AT RBL 23, FR74 CORRODED. REMOVED AND REPLACED RT INBD SEAT TRACK AT RBL 23 BETWEEN FR 61 TO FR 74 PER DWG PL C01342701 REV-G AND ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP# 1833889; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805392](https://openairdocs.org/sdr/DALA2026092805392.md): Seat Track · corroded · Sep 25, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > OUTBOARD RT SEAT TRACK AT FR 20, RBL 43.5 WAS CORRODED. REMOVED AND REPLACED THE FWD RT SEAT TRACK, FR 20 - 30 IAW DWG PL C02312600, REV K, AND ASRP BD500-A-51-42-20-00AAA-078A-A. (LP 1832414, AIRCRAFT WAS GROUNDED).
- [SDR DALA2026092805389](https://openairdocs.org/sdr/DALA2026092805389.md): Seat Track · corroded · Sep 25, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK CORRODED. RBL 43.5, FR 74. R & R THE RT SEAT TRACK, FR 61 - 74 IAW DWG PL C01342701, REV G AND ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP 1831445; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805388](https://openairdocs.org/sdr/DALA2026092805388.md): Support · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > SUPPORT, LAV E HAD CORROSION IN FASTENER HOLES, LBL 11, FR 76-79, WL147. REMOVED AND REPLACED THE LAV SUPPORT IAW ASRP BD500-J51-42-21-00AAA-078A-A, & DWG PL C01342700, REV T. (LP 1830130; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026092805387](https://openairdocs.org/sdr/DALA2026092805387.md): Seat Track · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OTBD SEAT TRACK CORRODED, LBL 43.50, FR 74. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J53-61-49-00AAA -661A-A, ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C01342701, REV G. (LP 1829629; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805385](https://openairdocs.org/sdr/DALA2026092805385.md): Web · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > AFT OF L2 DOOR, FLOOR WEB WAS CORRODED, FR 76 - 79. EVALUATED DAMAGE ON FLOOR WEB AND FOUND OUT OF LIMITS, NO DAMAGE PERMITTED IAW ASRP BD500-A-J51-10-06- 00AAA-028A-A, REMOVED AND REPLACED THE WEB IAW ASRP BD500-A-J51 -40-11-01AAA-652A-A, ASRP BD500-A-J51-
- [SDR DALA2026092805384](https://openairdocs.org/sdr/DALA2026092805384.md): Seat Track · corroded · Sep 23, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > INBOARD RT SEAT TRACK AT FR20, RBL 23 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C02312600, REV K. (LP 1828498; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805383](https://openairdocs.org/sdr/DALA2026092805383.md): Support Beam · corroded · Sep 23, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Structure
  > RIGHT OTBD SUPPORT BEAM CORRODED AT FR 76-78, RBL 36.5, WL 147 IN THE NUT PLATE HOLE. REMOVED AND REPLACED THE SUPPORT BEAM IAW ASRP BD500-A-J51-42-21-00AAA-078A-A. AND DWG PL C01342700 REV-T. (LP 18283474; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026100705541](https://openairdocs.org/sdr/DALA2026100705541.md): Floor Panel · corroded · Sep 22, 2026 · N310DU · Airbus BD5001A11 · Fuselage Floor Panel
  > L1 DOOR FLOOR PANEL# 221KLF HAS CORROSION. REMOVED AND REPLACED L1 DOOR FLOOR PANEL #221KLF IAW A220 AMP BD500-A-J53-00-47-11AAA-720A-A. (LP# 1849920; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805382](https://openairdocs.org/sdr/DALA2026092805382.md): Seat Track · corroded · Sep 22, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK AT LBL 23, FR74, CORRODED. REMOVED AND REPLACED THE SEAT TRACK BTWN LBL 23, FR 74 - 61 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, & DWG C01342701, REV G. (LP 1826399; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026080904592](https://openairdocs.org/sdr/DALA2026080904592.md): Skin · corroded · Aug 8, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > DURING CCK IN MSP, MAINTENANCE WAS ACCOMPLISHING ROUTINE CARD 2021-2025 AND FOUND CORROSION COMMON TO THE AFT WASTE SERVICE DOOR AREA. CORROSION IS COMMON TO THE DOOR AT HINGE ARM ATTACHMENT AND ON THE DOUBLER INBOARD FORWARD AND AFT CORNERS. THE FUSELAGE SKIN
- [SDR DALA2026082504824](https://openairdocs.org/sdr/DALA2026082504824.md): Skin · corroded · Aug 7, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > ER/A 618056-14 REV A ISSUED FOR CORROSION REPAIR TO THE LOWER AF T FUSELAGE SKIN AND WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRED. ERA 618056-14 REV A SECT. IV ACCOMPLISHED IN MSP 07AUG26. SECTION II REPEAT INSPECTIONS ARE REQUIRED @ EVERY 1000FH AFTER SECT.I
- [SDR DALA2025122909486](https://openairdocs.org/sdr/DALA2025122909486.md): O-Ring · contaminated · Dec 28, 2025 · N310DU · Airbus BD5001A11 · Hydraulic System, Main
  > AIRCRAFT 8310, FA'S REPORTED A CHEMICAL SMELLING SMOKE IN AFT GALLEY. THE SMOKE AND SMELL WENT TO THE EMERGENCY ROW AND EVENTUALLY THE CABIN. FA'S DONNED MASK. FOUND EVIDENCE OF HYD CONTAMINATION FROM EDP SUPPLY LINE NR 2 MID FUSALAGE TORQUED LINE IAW AMP 29
- [SDR DALA2025091806866](https://openairdocs.org/sdr/DALA2025091806866.md): Transceiver · failed · Sep 13, 2025 · N310DU · Airbus BD5001A11 · Weather Radar System
  > ATB DUE TO WEATHER RADAR FAIL ADVISORY. REMOVED AND REPLACED WEATHER RADAR ANTENNA, OPS CHECK GOOD ACFT OK FOR SERVICE. (LP 7876389)
- [SDR DALA2025081906210](https://openairdocs.org/sdr/DALA2025081906210.md): Lever · overrotated · Aug 13, 2025 · N310DU · Airbus BD5001A11 · Passenger/Crew Doors
  > DUE TO DELAY TAKEN FOR AFT LEFT DOOR EOAM MODE SELECT LEVER BEING FOUND IN THE OVER-CENTERED POSITION PLZ SETUP TO CHECK THE RIGGING OF THE EOAM TRIGGER PER A220 AMP 52- 12-08-01.CHECKED R/G OF L2 DOOR EOAM TRIGGER PER A220 AMP 52-12-08. FOUND OUT OF RIG. RIGG
- [SDR DALA2025042403238](https://openairdocs.org/sdr/DALA2025042403238.md): Engine · faulted · Apr 22, 2025 · N310DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)
  > 75 R ENGINE FAULT - BAV INOP IN FLIGHT BETWEEN 11,000 AND LANDING. BRIEF OILY SMELL @ 11,000FT, MSG CONTINUED TILL AFTER LANDING. T/S PER A220 EFIM FAULT CODE 7526F0020. FAULT DID NOT RETURN DURING HIGH POWER ENG RUN. NO 30 DAY HISTORY. T/S PER WC 0550- 2001.
- [SDR DALA2024121711790](https://openairdocs.org/sdr/DALA2024121711790.md): Slat Track · no discrepancy · Dec 11, 2024 · N310DU · Airbus BD5001A11 · Standard Practices/Structures
  > RH SLAT TRACK NBR 8 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02B. PERFORMED EDDY CURRENT INSPECTION R/H SLAT TRACK #8 UPPER FWD SURFACE PER A220 ANDTP 51-01-20. NO CRACKS NOTED. (LP# 0704956)
- [SDR DALA2024121711787](https://openairdocs.org/sdr/DALA2024121711787.md): Slat Track · no discrepancy · Dec 11, 2024 · N310DU · Airbus BD5001A11 · Standard Practices/Structures
  > LH SLAT TRACK NBR 1 UPPER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION L/H #1 SLAT TRACK UPPER AFT SURFACE PER A220 ANDTP 51-01-20. NO CRACKS NOTED. (LP# 0704911)
- [SDR DALA2024121711791](https://openairdocs.org/sdr/DALA2024121711791.md): Slat Track · no discrepancy · Dec 10, 2024 · N310DU · Airbus BD5001A11 · Standard Practices/Structures
  > RH SLAT TRACK NBR 2 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02B. PERFORMED EDDY CURRENT INSPECTION R/H #2 SLAT TRACK UPPER SURFACE PER A220 ANDTP 51-01-20. NO CRACKS NOTED. (LP# 0704980)
- [SDR DALA2024121711789](https://openairdocs.org/sdr/DALA2024121711789.md): Slat Track · no discrepancy · Dec 10, 2024 · N310DU · Airbus BD5001A11 · Standard Practices/Structures
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION L/H #4 SLAT TRACK UPPER AFT SURFACE PER A220 ANDTP 51-01-20. NO CRACKS NOTED. (LP# 0704949)
- [SDR DALA2024121711788](https://openairdocs.org/sdr/DALA2024121711788.md): Slat Track · no discrepancy · Dec 10, 2024 · N310DU · Airbus BD5001A11 · Standard Practices/Structures
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01029-02A. PERFORMED EDDY CURRENT INSPECTION R/H #5 SLAT TRACK UPPER SURFACE PER A220 ANDTP 51-01-20. NO CRACKS NOTED. (LP# 0704935)
- [SDR DALA2024090408719](https://openairdocs.org/sdr/DALA2024090408719.md): Coffeemaker · odor · Aug 30, 2024 · N310DU · Airbus BD5001A11 · Buffet/Galleys
  > GALLEY AND LAST 4 ROWS OF CABIN. TURNED OFF GALLEY HEATER/FAN, OVENS AND ELECTRICAL OUTLETS. SMELL DID NOT DISSIPATE. REMOVED SCREWS FOR AFT GALLEY CEILING PANEL(868406) R/R CENTER CEILING PANELS FROM ROW 25 TO AFT GALLEY AND CEILING PANELS IN AFT GALLEY. INSP
- [SDR DALA2024082808516](https://openairdocs.org/sdr/DALA2024082808516.md): Throttle · failed · Aug 24, 2024 · N310DU · Airbus BD5001A11 · Landing Gear Brake System
  > DIV - TO LAX DUE TO "AUTOBRAKE FAIL" MESSAGE ON APPROACH. CORRECTIVE ACTION: DEFERRED AUTOBRAKE SYSTEM TO MEL 32-43-15; R/R THROTTLE QUADRANT ASSEMBLY.
- [SDR DALA2024052805554](https://openairdocs.org/sdr/DALA2024052805554.md): Door · corroded · May 24, 2024 · N310DU · Airbus BD5001A11 · Fluid Service Doors
  > LAV SERVICE PANEL - ACCESS DOOR HAS CORROSION AT INBD HINGE ATTACHMENT AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0254:2021-2025/003 00220 REMOVED AND INSTALLED NEW DOOR ASSEMBLY PER A220 AMM 52-47-06. (LP#
- [SDR DALA2024052805553](https://openairdocs.org/sdr/DALA2024052805553.md): Waste Box · corroded · May 24, 2024 · N310DU · Airbus BD5001A11 · Fuselage Main, Structure
  > LAV SERVICE PANEL - WASTE BOX HAS CORROSION ON LOWER FLANGE AREA AT AFT INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0254:2021-2025/001 00218 COMPLIED WITH PRI 618056-14 REV 0, 1, 2, 3, AND ER/A 618056-
- [SDR DALA2024052805552](https://openairdocs.org/sdr/DALA2024052805552.md): Waste Box · corroded · May 24, 2024 · N310DU · Airbus BD5001A11 · Fuselage Main, Structure
  > LAV SERVICE PANEL - WASTE BOX HAS CORROSION ON LOWER AND UPPER FLANGE AREAS AT FWD INBD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0254:2021-2025/002 00219 COMPLIED WITH PRI 618056-14 REV 0, 1, 2, 3, AND E
- [SDR DALA2024051505239](https://openairdocs.org/sdr/DALA2024051505239.md): Isolator · worn · May 15, 2024 · N310DU · Airbus BD5001A11 · Wing Main, Frame Structure
  > WORN ISOLATOR ITEM #11 WORN TO LIMITS ON LH WING RIB 6. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 100-0001:2820-01281-05A/009 00244 REMOVED AND REPLACED ISOLATOR PER AMDS 2820-01281-05A-LH. (LP# 0343015)
- [SDR DALA2024051505238](https://openairdocs.org/sdr/DALA2024051505238.md): Canister · gouged · May 14, 2024 · N310DU · Airbus BD5001A11 · Fuel Storage
  > RH WING FUEL TANK - AC BOOST PUMP CANISTER (P/N 9C207-1) IS GOUGED ON PIPE CONNECTION FLANGE. SEE PICS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 101-0001:2820-01281-05B/001 00225 REMOVED AND REPLACED BOOST PUMP REF
- [SDR DALA2024051505237](https://openairdocs.org/sdr/DALA2024051505237.md): Tee Fitting · worn · May 14, 2024 · N310DU · Airbus BD5001A11 · Fuel Storage
  > ON TEE ASSEMBLY LC1325-01AE (ITEM 9) CHECK VALVES WERE WORN BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 101-0001:2820-01281-05B/005 00241 REMOVED AND REPLACED CHECK VALVES PER AMDS 2820-01281-05B-RH. (LP
- [SDR DALA2024051505236](https://openairdocs.org/sdr/DALA2024051505236.md): Tee Fitting · gouged · May 14, 2024 · N310DU · Airbus BD5001A11 · Fuel Storage
  > TEE ASSEMBLY LC1325-01AE (ITEM 9) GOUGED AT FLANGE END BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 101-0001:2820-01281-05B/004 00240 REMOVED AND REPLACED TEE ASSEMBLY PER AMDS 2820-01281-05B-RH. (LP# 034
- [SDR DALA2024020701652](https://openairdocs.org/sdr/DALA2024020701652.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185848)
- [SDR DALA2024020701651](https://openairdocs.org/sdr/DALA2024020701651.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 LOWER OB SIDE IAW PRI 608198-14AD REV 0 AND ERA REV C MATCHED. (LP# 0185844)
- [SDR DALA2024020701650](https://openairdocs.org/sdr/DALA2024020701650.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 RACK TOOTH NBR 2 SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 RACK TOOTH NBR 2 IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185839)
- [SDR DALA2024020701649](https://openairdocs.org/sdr/DALA2024020701649.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 PINION TOOTH HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 PINION TOOTH SURFACE IAW PRI 608198 -14AD REV 0 AND ERA REV C MATCHED. (LP# 0185837)
- [SDR DALA2024020701648](https://openairdocs.org/sdr/DALA2024020701648.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 9 UPPER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED.
- [SDR DALA2024020701647](https://openairdocs.org/sdr/DALA2024020701647.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 8 UPPER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185829)
- [SDR DALA2024020701646](https://openairdocs.org/sdr/DALA2024020701646.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 7 UPPER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185827)
- [SDR DALA2024020701645](https://openairdocs.org/sdr/DALA2024020701645.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185825)
- [SDR DALA2024020701644](https://openairdocs.org/sdr/DALA2024020701644.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 5 UPPER FORWARD SURFACE IAW PRI 608198-14AD REV 0 AND ERA REV C MATCHED. (LP# 0185822)
- [SDR DALA2024020701643](https://openairdocs.org/sdr/DALA2024020701643.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER OB AFT SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02A. MEASURED RH SLAT TRACK NBR 4 UPPER AFT OB SIDE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185817)
- [SDR DALA2024020701642](https://openairdocs.org/sdr/DALA2024020701642.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185815)
- [SDR DALA2024020701641](https://openairdocs.org/sdr/DALA2024020701641.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW PRI 608198- 14AD REV 0 AND ERA REV C MATCHED. (LP# 0185814)
- [SDR DALA2024020701640](https://openairdocs.org/sdr/DALA2024020701640.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 3 UPPER FORWARD SURFACE IAW PRI 608198-14AD REV 0 AND ERA REV C MATCHED. (LP# 0185811)
- [SDR DALA2024020701639](https://openairdocs.org/sdr/DALA2024020701639.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED RH SLAT TRACK NBR 2 UPPER FORWARD SURFACE IAW PRI 608198-14AD REV 0 AND ERA REV C MATCHED. (LP# 0185807)
- [SDR DALA2024020701638](https://openairdocs.org/sdr/DALA2024020701638.md): Slat Track · corroded · Feb 3, 2024 · N310DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. L REPAIRED RH SLAT TRACK NBR 1 UPPER FORWARD SURFACE IAW PRI 608198-14AD REV 0 AND ERA REV C MATCHED. (LP# 0185805)

Next page: https://openairdocs.org/aircraft/N310DU/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 = 'N310DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N310DU/reports

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