# Service difficulty reports: N102DU

A list on [N102DU](https://openairdocs.org/aircraft/N102DU.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 · 82 reports

- [SDR DALA2026091505149](https://openairdocs.org/sdr/DALA2026091505149.md): Skin · corroded · Sep 11, 2026 · N102DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WHILE PERFORMING REP INSPECTION PER ER/A 612524-14 REV C. FOUND CORROSION ON SKIN FWD OF WASTE PNL. BLENDED SKIN MINIMUM AMOUNT TO REMOVE CORROSION IAW ASRP 51 -21..25" X 2.5" GRIDED OUT OF BLENDED AREA (127702). REQUESTING UT OF BLENDED AREA (127702). ACCOMP
- [SDR DALA2026091605179](https://openairdocs.org/sdr/DALA2026091605179.md): Skin · corroded · Sep 10, 2026 · N102DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/A 612524-14 SECTION VII TIME LIMITED REPAIR VI WAS ISSUED FOR CORROSION FOUND ON THE FUSELAGE EXTERIOR SURFACE ADJACENT TO THE WASTE SERVICE CUTOUT, DURING SECTION V REPEAT INSPECTIONS PER LOG PAGE 0678171. CURRENT REV IS 'D'. ACCOMPLISH SECTION VIII REPEAT
- [SDR DALA2026052403144](https://openairdocs.org/sdr/DALA2026052403144.md): Hydraulic Line · sheared · May 24, 2026 · N102DU · Airbus BD5001A10 · Hydraulic System, Main
  > CREW DECLARED EMERGENCY DUE TO NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE LOSS. FOUND PRESSURE LINE FOR SYS 2 SHEARED. ALSO FOUND LOWER CLOSURE RIB BROKEN. ACCOMPLISHED REPAIR OF LOWER CLOSURE RIB 1, RIB 2, AND AFFECTED HYDRAULIC COMPONENTS AS PER ERA 63456
- [SDR DALA2026050402803](https://openairdocs.org/sdr/DALA2026050402803.md): Slide · warning message · Apr 29, 2026 · N102DU · Airbus BD5001A10 · Escape Slide
  > LEFT WING SLIDE CAUTION ON LANDING. R & R LEFT OVER WING EMERGENCY EXIT DOOR SLIDE PER 2563-4002 VERIFIED SLIDE INSTALL PIN REMOVED RII COMPLETED. QC 5352 (484068) NO DEFECTS NOTED, NO FAULT MESSAGES OR INDICATIONS. (M) PROCEDURES REVERSED. PLACARD REMOVED.
- [SDR DALA2026042002485](https://openairdocs.org/sdr/DALA2026042002485.md): Pump · failed · Apr 18, 2026 · N102DU · Airbus BD5001A10 · Hydraulic Pump (Electric/Engine), Main
  > DECLARED EMERGENCY DUE TO HYD PUMP 2B FAIL. REPLACED HYD PUMP 2B, RT EDP AND RUDDER PCU. R & R CASE DRAIN FILTER, PRESSURE FILTER ELEMENT, HYDRAULIC LINE AND O-RING. REPLACED PRESSURE COIL LINE OF THE MIDDLE PCU. OPS CHECK OKAY. (LP# 8717840; AIRCRAFT WAS GR
- [SDR DALA2026032301955](https://openairdocs.org/sdr/DALA2026032301955.md): Reu · failed · Mar 23, 2026 · N102DU · Airbus BD5001A10 · Rudder Control System
  > DIV - TO CLE DUE TO "RUDDER FAIL" WARNING MESSAGE. REPLACED #1 AFT REU. OK FOR SERVICE. (LP# 8384156)
- [SDR DALA2025081105982](https://openairdocs.org/sdr/DALA2025081105982.md): Handle · unsecure · Aug 9, 2025 · N102DU · Airbus BD5001A10 · Cargo/Baggage Doors
  > SHIP 8102 - DIV - DUE TO FORWARD CARGO DOOR CAUTION MSG FOLLOWED BY CABIN PRESSURE WARNING. EMERGENCY WAS DECLARED. CORRECTIVE ACTION: FOUND FORWARD CARGO DOOR HANDLE NOT SECURED. PERFORMED GVI NO DAMAGE NOTED. PERFORMED PRESSURIZATION CHECK, PRESSURE CHECKS G
- [SDR DALA2025061304495](https://openairdocs.org/sdr/DALA2025061304495.md): Slat Track · damaged · Jun 9, 2025 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #6 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621359-14 REV 0 AND ERA 621359-14AD REV B SECTION V. MATCHES. (LP# 1014483)
- [SDR DALA2025061304494](https://openairdocs.org/sdr/DALA2025061304494.md): Slat Track · damaged · Jun 9, 2025 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #6 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621359-14 REV 0 AND ERA 621359-14AD REV B SECTION V. MATCHES. (LP# 1014482)
- [SDR DALA2025061304493](https://openairdocs.org/sdr/DALA2025061304493.md): Slat Track · damaged · Jun 9, 2025 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #4 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621242-14 REV 0 AND ERA 621242-14AD REV A SECTION IV. MATCHES. (LP# 1014478)
- [SDR DALA2025061304492](https://openairdocs.org/sdr/DALA2025061304492.md): Slat Track · damaged · Jun 9, 2025 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #4 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621242-14 REV 0 AND ERA 621242-14AD REV A SECTION IV. MATCHES. (LP# 1014477)
- [SDR DALA2025022701551](https://openairdocs.org/sdr/DALA2025022701551.md): Engine · odor · Feb 18, 2025 · N102DU · Airbus BD5001A10 · Pneumatic Distribution System
  > AIRCRAFT 8102, SWEATY SOCK SMELL DURING FINAL APPROCH AND TAXI IN. CORRECTIVE ACTION: C/W WORK CARD 0550-2001 AND WORK CARD 0550-6001. PERFORMED DUCT BURN OUT AND FOUND #2 ENG STILL SMELL. LOCKED OUT #2 ENG BLEED. CREATING MONITOR PER W/C 0550-6001 STEP 7, DEF
- [SDR DALA2025012900708](https://openairdocs.org/sdr/DALA2025012900708.md): Engine · odor · Jan 22, 2025 · N102DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > DIRTY SOCK SMELL ON T/O UNTIL AROUND 50000 FEET, AFTER LANDING DIRTY SOCK SMELL BECAME WORSE/ MORE PRONOUNCED. WORK IAW JIC 0550-2003, 0550-2001, JIC 0550-6001- PREFORMED MULTIPLE DUCT BURN OUTS FOUND #2 ENG STILL SMELLS, LOCKED OUT BLEED, REPLACED RECIRC FILT
- [SDR DALA2024121711786](https://openairdocs.org/sdr/DALA2024121711786.md): Not Reported · not reported · Dec 11, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > NR WRITTEN FOR THE CONTINUATION COMMENTS OF ER/A 621981-14 PRI REV 1, STEP 9. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5300-2015/010 00552 REPAIRED PER ERA PRI 321981-14 REV 0, REV 1, REV 2, REV 3, REV 4 AN
- [SDR DALA2024121711797](https://openairdocs.org/sdr/DALA2024121711797.md): Seat Track · corroded · Dec 11, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OUTBOARD AFT END OF SEAT TRACK HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND ON TOP SURFACE AND PITTING OF SEAT TRACK @ FRAME 74. NO PRESENCE OF BLUE PAINT/INK. REPAIRED PER ERA PRI 621981-14 REV 0, REV 1, REV 2, REV 3, RE V
- [SDR DALA2024121111658](https://openairdocs.org/sdr/DALA2024121111658.md): Scuff Plate · corroded · Dec 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SCUFF PLATE FASTENER HOLE 4OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M) SUMMARY SEE NR FOR ADDITIONAL INFORMATION 059-0001:5331-01297- 02B/001 00243 COMPLETED PRI 621850-14 REV 0, 1, AND ERA 621850- 14 REV A. ORIGINAL MATERIAL THIC
- [SDR DALA2024121111656](https://openairdocs.org/sdr/DALA2024121111656.md): Seat Track · corroded · Dec 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION @ STA 22 RBL 23 (P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0559:5321-2021/002 00403 COMPLETED PRI 622253-14, REV 0, REV 1 REV 2, REV 3, REV 4, AND ERA 622253- 14 REV A. SEAT
- [SDR DALA2024121011574](https://openairdocs.org/sdr/DALA2024121011574.md): Floor Panel · corroded · Dec 7, 2024 · N102DU · Airbus BD5001A10 · Fuselage Floor Panel
  > FWD CABIN FLOOR FWD PASSENGER ENTRY DOOR FR19 FWD INBD CORNER CORRODED.-M-PIC SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0560:5321-2022/001 00448 CMOR: REMOVED AND REPLACED FWD PASSENGER DOOR ENTRANCE FLOOR PANEL, REF A220 AMP 53-00-47-11. (LP# 0697197)
- [SDR DALA2024121011573](https://openairdocs.org/sdr/DALA2024121011573.md): Scuff Plate · corroded · Dec 3, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR UPPER SCUFF PLATE FASTENER HOLE 6OU HAS CORROSION AROUND THE SURROUNDING AREA. (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 057-0001:5331-01297-01C/001 00227 COMPLETED PRI 621840-14 REV 0, 1,
- [SDR DALA2024120311422](https://openairdocs.org/sdr/DALA2024120311422.md): Drain Mast · corroded · Nov 27, 2024 · N102DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FUSELAGE AT MATING SURFACE OF AFT HEATED DRAIN MAST. CEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0462:3833-2001/004 00521 REPAIRED PER ER/A 622287-14 PRI REV 0, ER/A 595615-14 REV B PRI REV 1, REV
- [SDR DALA2024120311421](https://openairdocs.org/sdr/DALA2024120311421.md): Mechanism · inoperative · Nov 26, 2024 · N102DU · Airbus BD5001A10 · Escape Slide
  > DURING TESTING FOUND LH OVERWING SLIDE DEPLOYMENT MODE SELECT MECHANISM IS NOT OPERATING CORRECTLY IN THE ARMED POSITION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0115:5221-2001-01/001 00330 ADJUSTED LH OWEED ES
- [SDR DALA2024112511190](https://openairdocs.org/sdr/DALA2024112511190.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 9OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/003 00237 COMPLIED WITH ER/A 621911-14 PR
- [SDR DALA2024112511188](https://openairdocs.org/sdr/DALA2024112511188.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 10OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M) W SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/002 00236 COMPLIED WITH ER/A 621911-14
- [SDR DALA2024112511187](https://openairdocs.org/sdr/DALA2024112511187.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 8OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/004 00238 COMPLIED WITH ER/A 621911-14 P
- [SDR DALA2024112511186](https://openairdocs.org/sdr/DALA2024112511186.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 4OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/005 00239 COMPLIED WITH ER/A 621911-14 P
- [SDR DALA2024112511185](https://openairdocs.org/sdr/DALA2024112511185.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 3OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/006 00240 COMPLIED WITH ER/A 621911-14 P
- [SDR DALA2024112511184](https://openairdocs.org/sdr/DALA2024112511184.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 2OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/007 00241 COMPLIED WITH ER/A 621911-14 P
- [SDR DALA2024112511183](https://openairdocs.org/sdr/DALA2024112511183.md): Scuff Plate · corroded · Nov 21, 2024 · N102DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 11OL HAS CORROSION ON AT HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/001 00235 COMPLIED WITH ER/A 621911-14 P
- [SDR DALA2024111110822](https://openairdocs.org/sdr/DALA2024111110822.md): Seat Track · corroded · Nov 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION @ STA 22 RBL 43.5 (P). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0559:5321-2021/001 00402 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-77-00-00 -028. (LP# 0650524)
- [SDR DALA2024111110821](https://openairdocs.org/sdr/DALA2024111110821.md): Seat Track · corroded · Nov 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OUTBOARD AFT END OF SEAT TRACK (UNDER AFT RIGHT LAV) HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND PITTING ON TOP SURFACE OF SEAT TRACK FRAME 74. NO PRESENCE OF BLUE PAINT/INK. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0
- [SDR DALA2024111110820](https://openairdocs.org/sdr/DALA2024111110820.md): Seat Track · corroded · Nov 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBOARD AFT END OF SEAT TRACK (UNDER AFT RIGHT LAV) HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION ON TOP SURFACE OF SEAT TRACK FRAME 74. NO PRESENCE OF BLUE PAINT/INK. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5300-2015
- [SDR DALA2024111110818](https://openairdocs.org/sdr/DALA2024111110818.md): Seat Track · corroded · Nov 8, 2024 · N102DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OUTBOARD AFT END OF SEAT TRACK HAS SURFACE GALVANIC CORROSION (M) SSI: 53-61-43-01. GALVANIC CORROSION AND ON TOP SURFACE AND PITTING OF SEAT TRACK @ FRAME 65. NO PRESENCE OF BLUE PAINT/INK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR
- [SDR DALA2024110110583](https://openairdocs.org/sdr/DALA2024110110583.md): Slat Track · no discrepancy · Oct 29, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > RIGHT WING SLAT TRACK 6 REQUIRES NDT TO BLENDED AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 184-0001:5742-01028-02B/004 00489 PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353
- [SDR DALA2024110110581](https://openairdocs.org/sdr/DALA2024110110581.md): Slat Track · no discrepancy · Oct 29, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > RIGHT WING SLAT TRACK 9 REQUIRES NDT TO BLENDED AREA. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 184-0001:5742-01028-02B/005 00490 PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353
- [SDR DALA2024110110580](https://openairdocs.org/sdr/DALA2024110110580.md): Slat Track · no discrepancy · Oct 29, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > RIGHT WING SLAT TRACK 4 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED FINDINGS ON AMDS 5742- 01028-02B. NO CRACKS NOTED. (LP# 0634534)
- [SDR DALA2024110110579](https://openairdocs.org/sdr/DALA2024110110579.md): Slat Track · no discrepancy · Oct 29, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > RIGHT WING SLAT TRACK 3 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED FINDINGS ON AMDS 5742- 01028-02B. NO CRACKS NOTED. (LP# 0634533)
- [SDR DALA2024110110578](https://openairdocs.org/sdr/DALA2024110110578.md): Slat Track · no discrepancy · Oct 29, 2024 · N102DU · Airbus BD5001A10 · Standard Practices/Structures
  > SLAT TRACK 2 REQUIRES NDT TO BLENDED AREA. PERFORMED HFEC TO SLAT TRACK BLENDED AREAS REF A220 ANDTP BD500- A-J51-01-20-01AAA-353A-A AND DOCUMENTED FINDINGS ON AMDS 5742- 01028-02B. NO CRACKS NOTED. (LP# 0634530)
- [SDR DALA2024061106015](https://openairdocs.org/sdr/DALA2024061106015.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER AFT I/B SIDE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380399)
- [SDR DALA2024061106014](https://openairdocs.org/sdr/DALA2024061106014.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER FWD O/B SIDE IAW ERA 608252- 14AD REV C AND PRI 608252-13AD REV 0 MATCHED. (LP# 0380395)
- [SDR DALA2024061106013](https://openairdocs.org/sdr/DALA2024061106013.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 LOWER FWD I/B SIDE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380391)
- [SDR DALA2024061106012](https://openairdocs.org/sdr/DALA2024061106012.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380387)
- [SDR DALA2024061106011](https://openairdocs.org/sdr/DALA2024061106011.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF WEAR IN TWO LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED R/H SLAT TRACK NBR 11 LOWER AFT SURFACE IAW ER/A 608252 -14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380384)
- [SDR DALA2024061106010](https://openairdocs.org/sdr/DALA2024061106010.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. MEASURED R/H SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380380)
- [SDR DALA2024061106009](https://openairdocs.org/sdr/DALA2024061106009.md): Slat Track · cracked · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > CLOSING PLATES, SLAT NO.2 TRACK NO.4 CRACKED. REPLACED CLOSING PLATE, SLAT#2, TRACK#4, IAW A220 AMP BD500- A-J57-42-39-02AAA-720A-A. UP TO STEP#2 STANDING BY FOR ADJUSTMENT OF THE HOUSING PLATE IAW D500-A-J57-42-39- 02AAA-720A-A.
- [SDR DALA2024061106008](https://openairdocs.org/sdr/DALA2024061106008.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. MEASURED RH SLAT TRACK NBR 5 UPPER AFT O/B SIDE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380374)
- [SDR DALA2024061106007](https://openairdocs.org/sdr/DALA2024061106007.md): Slat Track · corroded · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380366)
- [SDR DALA2024061106006](https://openairdocs.org/sdr/DALA2024061106006.md): Slat Track · corroded · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H 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 608252- 14AD REV C AND PRI 608252-14AD REV 0 MATCHED. (LP# 0380362)
- [SDR DALA2024061106005](https://openairdocs.org/sdr/DALA2024061106005.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. RH SLAT TRACK#4 REPLACED. REF NR 001 FOR CORRECTIVE ACTION. (LP# 0379714)
- [SDR DALA2024061106004](https://openairdocs.org/sdr/DALA2024061106004.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. RH SLAT TRACK #4 REPLACED. REF NR 001 FOR CORRECTIVE ACTION. (LP# 0379700)
- [SDR DALA2024061106003](https://openairdocs.org/sdr/DALA2024061106003.md): Slat Track · worn · Jun 6, 2024 · N102DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK REF 5742-01028-02B. RH SLAT TRACK #4 REPLACED. REF NR001 FOR CORRECTIVE ACTION. (LP# 0379693)

Next page: https://openairdocs.org/aircraft/N102DU/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 = 'N102DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N102DU/reports

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