# Service difficulty reports: N104DU

A list on [N104DU](https://openairdocs.org/aircraft/N104DU.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 · 96 reports

- [SDR DALA2026012300525](https://openairdocs.org/sdr/DALA2026012300525.md): Light · inoperative · Jan 19, 2026 · N104DU · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS. R & R AFT RT LED ASSEMBLY PER AMP 33-55. OPS CK GOOD MEL + PLACARD INSTALLED. (LP# 7904243)
- [SDR DALA2025121209104](https://openairdocs.org/sdr/DALA2025121209104.md): Unknown · odor · Dec 9, 2025 · N104DU · Airbus BD5001A10 · Air Distribution System
  > ON APPROACH AT 4000' MSL, BOTH PILOTS NOTICED FUMES ON THE FLT DECK. VERY NOTICEABLE DIRTY SOCK SMELL. NO VISIBLE FUMES. 2 PACKS, SINGLE RIGHT BLEED DUE TO MEL CONFIGURATION. SMELL AFTER APU START WE TURNED OFF REMAINING RIGHT BLEED AND SMELL SLIGHTLY DISSIPAT
- [SDR DALA2025120408875](https://openairdocs.org/sdr/DALA2025120408875.md): None · none · Dec 1, 2025 · N104DU · Airbus BD5001A10 · Standard Practices/Structures
  > DAMAGE TOLERANCE EVALUATION. ERA 621788-14, REV B, PROVIDES STAGE 2 APPROVAL FOR SECTION IV REPAIR. FOLLOW ON ACTION IS REQUIRED ON THE FUSELAGE SKIN FWD OF FR 15, STR. 6R - STR 8R. MAJOR REPAIR, SDR YES. ACCOMPLISH ERA 621788-14 REV B SECTION V WITHIN 15,000
- [SDR DALA2025042403240](https://openairdocs.org/sdr/DALA2025042403240.md): Smoke Detector · faulted · Apr 20, 2025 · N104DU · Airbus BD5001A10 · Smoke Detection
  > FA REPORTED BURNING SMELL IN RIGHT AFT LAV, SMOKE DETECTOR BEEPED TWICE FA CALL LIGHT WENT ON THEN OUT AND SMELL DISSIPATED CONFERRED WITH MAINT CONTROL FOLLOWED QRH DETERMINED SAFE TO CONTINUE. DE-BRIEFED FLT CREW & ENSURED SMOKE & FUMES QUESTIONNAIRE WAS COM
- [SDR DALA2025040802751](https://openairdocs.org/sdr/DALA2025040802751.md): Unknown · odor · Apr 3, 2025 · N104DU · Airbus BD5001A10 · Air Distribution System
  > ON TAXI OUT RECEIVED CALL FROM AFT FA'S STATING SMELL OF DIRTY SOCKS COMING FROM AFT AIR VENTS. FORWARD FA SMELLED NOTHING UPFRONT WENT TO BACK AND SMELLED DIRTY SOCK SMELL TOO. BOTH ENGINES RUNNING SMELL CAME FIVE MINUTES INTO TAXI. SMELL NOT AS STRONG BUT ST
- [SDR DALA2025030201591](https://openairdocs.org/sdr/DALA2025030201591.md): Outlet · failed · Feb 27, 2025 · N104DU · Airbus BD5001A10 · AC Power Distribution System
  > AIRCRAFT 8104, RIGHT AFT LAV WAS REPORTED THAT THE EMERGENCY HORN AND LIGHT REPEATLY TRIPPED. THEY ALSO REPORTED SMELLING A MILD ELECTRICAL ODOR. FOUND OUTLET UNIT AT 29CD BURNED MARK. R/R OUTLET WITH MPN 1292-7-117 PER AMP 44-28, CK GOOD. VISUAL INSPECTED L
- [SDR DALA2025011300286](https://openairdocs.org/sdr/DALA2025011300286.md): Skin · corroded · Jan 10, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION SSI: 53-60-02-03. CORROSION FOUND BETWEEN FR 70 AND FR71 AND BETWEEN STGR 36L AND STGR 35L. REPAIRED PER PRI 622727-14 REV 0,1,2,3 AND ERA 622727-14 REV ORIGINAL. (LP# 0754712)
- [SDR DALA2025100207162](https://openairdocs.org/sdr/DALA2025100207162.md): Seat Track · corroded · Jan 9, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > OUTBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK PER ER/A 622672-14 PRI REV. 0, REV. 1, REV. 2, AND FINAL ER/A 622672-14 REV. ORIGINAL. (LP# 0752599)
- [SDR DALA2025011300285](https://openairdocs.org/sdr/DALA2025011300285.md): Seat Track · corroded · Jan 9, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > REFERENCE AMDS 5300-2015. SSI 53-61-43-01. SEAT TRACK CORROSION NOTED AT RBL 23.0 AT FRAME 61. REMOVED AND REPLACED SEAT TRACK REF. A220 ASRP 51-77-00-28. (LP# 0752646)
- [SDR DALA2025011300284](https://openairdocs.org/sdr/DALA2025011300284.md): Seat Track · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SSI: 53-21-43-01 SEAT TRACK CORROSION RBL 43.5 AT FRAME 20 (M)(P) LOG-PAGE UPDATED @ 08JAN25 2130 UTC 02 CORR BY SACHS 00583347 MSP 08JAN25 ATA 5346 RII: N ENTR 00260220 W SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 0
- [SDR DALA2025011300283](https://openairdocs.org/sdr/DALA2025011300283.md): Door · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Cargo/Baggage Doors
  > WHILE ACCOMPLISHING AFT CARGO DOOR CORROSION INSPECTION PER AMDS 5331-01297-02C, FOUND CORROSION AT/AROUND HOLES 1OL, 2OL, 3OL, 4OL, 5OL, 6OL, 7OL, 8OL, 9OL, 10OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 179-0001:5331-01297- 02C/001 00242 REPAIRED PER ER/A 6
- [SDR DALA2025011300282](https://openairdocs.org/sdr/DALA2025011300282.md): Skin · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION BETWEEN HOLES 5OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 179-0001:5331-01297- 02C/004 00259 REPAIRED REF ER/A 622538-14 PRI REV 0, REV 1 AND ER/A 622538-1
- [SDR DALA2025011300281](https://openairdocs.org/sdr/DALA2025011300281.md): Skin · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD RIGHT SERVICE/PASSENGER DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 0.75" ABOVE HOLE 3OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 179-0001:5331-01297- 02C/003 00258 REPAIRED REF ER/A 622538-14 PRI REV 0, REV 1 AND ER/A 62253
- [SDR DALA2025011300280](https://openairdocs.org/sdr/DALA2025011300280.md): Door Sill · damaged · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD RH SERVICE/PASSENGER DOOR, LOWER DOOR SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 045-0001:5331-01297- 01B/002 00260 REPAIRED REF ER/A 622538-14 PRI REV 0, REV 1 AND ER/A 622538-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 045-0001:5331-0
- [SDR DALA2025011300279](https://openairdocs.org/sdr/DALA2025011300279.md): Service Door · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fluid Service Doors
  > WHILE ACCOMPLISHING FWD RIGHT SERVICE/PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-01B, FOUND CORROSION AT/AROUND HOLES 4OL, 8OL, SUMMARY SEE NR FOR ADDITIONAL INFORMATION 045-0001:5331-01297- 01B/001 00257 REPAIRED REF ER/A 622538-14 PRI REV 0, REV
- [SDR DALA2025011300278](https://openairdocs.org/sdr/DALA2025011300278.md): Skin · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > AFT RIGHT PASSENGER/SERVICE DOOR, FUSELAGE SKIN COVERED BY LOWER SCUFF PLATE, SMALL AREA OF CORROSION 1.5" ABOVE/FWD OF HOLE 12OL. MARKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 048-0001:5331-01297- 02B/001 00246 REPAIRED PER PRI 622574-14 REV 0,REV1 AND ER
- [SDR DALA2025011300277](https://openairdocs.org/sdr/DALA2025011300277.md): Seat Track · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SSI: 53-21-43-01 SEAT TRACK CORROSION LBL 43.5 FORWARD OF FRAME 22 (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0559:5321-2021/005 00360 REPAIRED REF ER/A 622665-14 PRI REV 0, REV 1 AND FINAL ER/A 622665-14
- [SDR DALA2025011300276](https://openairdocs.org/sdr/DALA2025011300276.md): Seat Track · corroded · Jan 8, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SSI: 53-61-43-02. LEFT INBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0573:5300-2016/004 00353 CMOR COMPLIED WITH ER/A PRI 622670-14 REV 0 REV 1
- [SDR DALA2025011000227](https://openairdocs.org/sdr/DALA2025011000227.md): Door Sill · corroded · Jan 7, 2025 · N104DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT LH PASSENGER DOOR, LOWER DOOR SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297- 02A/003 00249 REPAIRED PER ER/A 622582-14 PRI REV 0, REV 1, AND ER/A 622582-14 ORIGINAL, ORIGINAL THICKNESS.125 MIN MAX MATERIAL REMOVED.063, REMAINING THI
- [SDR DALA2025011000226](https://openairdocs.org/sdr/DALA2025011000226.md): Skin · corroded · Jan 7, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING AFT LEFT PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-02A, FOUND CORROSION AT/AROUND HOLES 12OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297- 02A/002 00247 REPAIRED PER ER/A 622582-14 PRI REV 0, REV 1, AND ER/A
- [SDR DALA2025011000225](https://openairdocs.org/sdr/DALA2025011000225.md): Skin · corroded · Jan 7, 2025 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING FWD CARGO DOOR CORROSION INSPECTION PER AMDS 5331-01297-01C, FOUND CORROSION AT/AROUND HOLES 13OL, 14OL, 16OL, 17OL, 18OL, 19OL, 20OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 046-0001:5331-01297-01C/001 00241 REPAIRED PER ER/A 623164-14 P
- [SDR DALA2025010800173](https://openairdocs.org/sdr/DALA2025010800173.md): None · none · Jan 4, 2025 · N104DU · Airbus BD5001A10 · Standard Practices/Structures
  > RE-INSTALL PREVIOUSLY REMOVED FWD CARGO DOOR UPPER SCUFF PLATE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 046-0001:5331-01297-01C/002 00616 ACCOMPLISHED INSTALLATION REF. NR 241 AND ASSOCIATED ER/A PRI 623164-14. (LP
- [SDR DALA2025010600114](https://openairdocs.org/sdr/DALA2025010600114.md): Seat Track · corroded · Jan 3, 2025 · N104DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OUTBOARD SEAT TRACK IN AREA AFT OF FRAME 71, MULTIPLE AREAS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0573:5300-2016/002 00351 REPAIRED PER ER/A 622671-14 PRI REV. 0, RE
- [SDR DALA2025010612133](https://openairdocs.org/sdr/DALA2025010612133.md): Door Sill · not reported · Dec 31, 2024 · N104DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > SSI: 53-21-25-02. FWD CARGO, LOWER SILL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0497:5321-2015/001 00261 REMOVED AND REPLACED LOWER SILL AND CORNER STRIKER PER A220 ASRP 51-40-00. (LP# 0737834)
- [SDR DALA2025010212124](https://openairdocs.org/sdr/DALA2025010212124.md): Frame · corroded · Dec 30, 2024 · N104DU · Airbus BD5001A10 · Fuselage Main, Frame
  > AFT EQUIPMENT BAY FRAME 81 (JUST FWD OF ACCESS DOOR 867) AFT FACE HAS CORROSION BETWEEN L36-R36 (FOUND DURING INSPECTION OF ACCESS DOOR 867). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0775:2090-2106/002 00252 REM
- [SDR DALA2024123112108](https://openairdocs.org/sdr/DALA2024123112108.md): Skin · cracked · Dec 27, 2024 · N104DU · Airbus BD5001A10 · Wing, Plate/Skin
  > LEFT WING, #2 SLAT CUTOUT IS CRACKED AT UPPER OUTBOARD CORNER. VERIFIED BY HFEC AT.457 INCHES LONG. MARKED/PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0679:5741-2001-LH/011 00154 COMPLIED WITH ER/A 602228-1
- [SDR DALA2024123112107](https://openairdocs.org/sdr/DALA2024123112107.md): Skin · cracked · Dec 27, 2024 · N104DU · Airbus BD5001A10 · Wing, Plate/Skin
  > RIGHT WING, #5 SLAT TRACK CUT OUT HAS A CRACK AT UPPER OUTBOARD CORNER. VERIFIED BY HFEC AT.236 INCHES LONG. MARKED/PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0679:5741-2001-LH/020 00163 REPAIRED PER ER/A
- [SDR DALA2025011300287](https://openairdocs.org/sdr/DALA2025011300287.md): Skin · dented · Oct 22, 2024 · N104DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > RAMP REPORTS DENT ON UPPER RT FUSELAGE AREA/CANOPY. FND DENT TO BE NEAR FRAME 15, DENT IS 4 3/16" BY 2 3/4" WITH A DEPTH OF.038". OUT OF LIMITS PER A220 ASRP 53-11-01-05AAA- 661A-A (314041) PERFORMED A DVI OF EXTERNAL AREA AT DAMAGE LOCATION PER ANDTP BD500-A
- [SDR DALA2024091909195](https://openairdocs.org/sdr/DALA2024091909195.md): Bleed Air Sys · odor · Sep 9, 2024 · N104DU · Airbus BD5001A10 · Engine Bleed Air System
  > BLEED AIR SYSTEMS - ENGINE **DISPATCHER SELECT EXTENSION** MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG RE DEFERRAL REQUIRED.- -DURING T/O ROLL HAD STRONG ODOR AS SOON AS THE POWER WAS ADVANCED. ACCOMPLISHED WATER WASH PER AMDS W/C 7200-9001-02.
- [SDR DALA2024091709115](https://openairdocs.org/sdr/DALA2024091709115.md): Unknown · odor · Sep 8, 2024 · N104DU · Airbus BD5001A10 · Air Distribution System
  > DIRTY SOCK SMELL - BEGAN ON TAKEOFF ROLL, LASTED ABOUT 5 MINUTES THEN DISSIPATED UNTIL FINAL APPROACH AND TAXI-IN. WHEN THE DIRTY SOCK ODOR WAS NOTICEABLE AGAIN. COMPLETED A220 WORK CARD 0550-2001 PER A220 NO GO ODI PREVENTION PROGRAM ATA 2172 - SMOKE/FUMES IN
- [SDR DALA2024052305450](https://openairdocs.org/sdr/DALA2024052305450.md): Waste Box · corroded · May 22, 2024 · N104DU · Airbus BD5001A10 · Fuselage Main, Structure
  > MON ERA 596162-14AD CORROSION IN WASTE BOX. WHILE PERFORMING REPEAT INSPECTION II OF ERA 596162-14AD REV ORIGINAL NOTED CORROSION ON EXTERNAL SKIN AND IN RH LOWER SIDE OF WASTE BOX. C/W ERA 596162-14AD REV A SEC III. TEMP REPAIR ACCOMPLISHED. (LOGS 2077486 AND
- [SDR DALA2024031803421](https://openairdocs.org/sdr/DALA2024031803421.md): Lens · missing · Mar 16, 2024 · N104DU · Airbus BD5001A10 · Emergency Lighting
  > ON SVC CHK, PORTION CHECKING EMERGENCY ESCAPE PATH LIGHTING FOUND R1 DOOR ILLUMINATION LIGHT LENS MISSING. REPLACED MISSING R1 DOOR GENERAL ILLUMINATION ESCAPE PATH LIGHT LENS IN REF. WITH A220 IPDP BD500-A-J33-52-02-03AAA-941A-A. OK FOR SVC. (LP# 5388165)
- [SDR DALA2024013001383](https://openairdocs.org/sdr/DALA2024013001383.md): Slat Track · corroded · Jan 28, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT INBOARD SIDE PER ERA 608598-14AD REV C & PRI REV
- [SDR DALA2024013001381](https://openairdocs.org/sdr/DALA2024013001381.md): Slat Track · corroded · Jan 28, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD INBOARD SIDE PER ERA 608598-14AD REV C & PRI REV
- [SDR DALA2024013001380](https://openairdocs.org/sdr/DALA2024013001380.md): Slat Track · corroded · Jan 28, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD OUTBOARD SIDE PER ERA 608598-14AD REV C & PRI R
- [SDR DALA2024013001378](https://openairdocs.org/sdr/DALA2024013001378.md): Slat Track · corroded · Jan 28, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF A WEAR MARK AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE PER ERA 608598- 14AD REV C & PRI REV 0,1 MA
- [SDR DALA2024013001376](https://openairdocs.org/sdr/DALA2024013001376.md): Slat Track · corroded · Jan 28, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 11 UPPER AFT SURFACE PER ERA 608598- 14AD REV C & PRI REV 0,1 MA
- [SDR DALA2024013001375](https://openairdocs.org/sdr/DALA2024013001375.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 11 UPPER FWD SURFACE PER ERA 608598- 14AD REV C & PRI REV 0,1 MA
- [SDR DALA2024013001374](https://openairdocs.org/sdr/DALA2024013001374.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD INBOUND SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD I/B SIDE PER ERA 608598- 14AD REV C & PRI REV 0,
- [SDR DALA2024013001373](https://openairdocs.org/sdr/DALA2024013001373.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE PER ERA 608598- 14AD REV C & PRI REV 0
- [SDR DALA2024013001372](https://openairdocs.org/sdr/DALA2024013001372.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER AFT INBOARD SIDE HAS EVIDENCE OF WEAR MARK AND PREVIOUS REWORK REF REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. LH SLAT TRACK NBR 6 UPPER AFT INBOARD SIDE HAS EVIDENCE OF WEAR MARK AND PREVIOUS R
- [SDR DALA2024013001371](https://openairdocs.org/sdr/DALA2024013001371.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE PER ERA 608598- 14AD REV C & PRI REV 0,1 MATC
- [SDR DALA2024012901265](https://openairdocs.org/sdr/DALA2024012901265.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 8 LOWER AFT SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC
- [SDR DALA2024012901264](https://openairdocs.org/sdr/DALA2024012901264.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 INBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 7 I/B LOWER FWD SIDE PER ERA 608598- 14AD REV B & PRI REV 0,1
- [SDR DALA2024012901263](https://openairdocs.org/sdr/DALA2024012901263.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC
- [SDR DALA2024012901262](https://openairdocs.org/sdr/DALA2024012901262.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC
- [SDR DALA2024012901261](https://openairdocs.org/sdr/DALA2024012901261.md): Slat Track · corroded · Jan 27, 2024 · N104DU · 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 SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC
- [SDR DALA2024012901260](https://openairdocs.org/sdr/DALA2024012901260.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC
- [SDR DALA2024012901259](https://openairdocs.org/sdr/DALA2024012901259.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 2 UPPER AFT SURFACE PER ERA 608598- 14AD REV B & PRI REV O,1 MAT
- [SDR DALA2024012901272](https://openairdocs.org/sdr/DALA2024012901272.md): Slat Track · corroded · Jan 27, 2024 · N104DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NBR 1 UPPER AFT SURFACE PER ERA 608598- 14AD REV B & PRI REV 0,1 MATC

Next page: https://openairdocs.org/aircraft/N104DU/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 = 'N104DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N104DU/reports

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