# Service difficulty reports: N115DU

A list on [N115DU](https://openairdocs.org/aircraft/N115DU.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 · 81 reports

- [SDR DALA2026090805026](https://openairdocs.org/sdr/DALA2026090805026.md): Roller · worn · Sep 5, 2026 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RIGHT NR 4 SLAT TRACK BOTH INBD ROLLER WORN, EXCEED MAXIMUM DEPTH OF.010" AT.018" PER WC 5742-01028-02B. REPAIRED PER PRI 620677-14AD REV 0 ER/A REV C, AND FINAL ER/A 620677-14AD REV C SEC VI. (LP# 1796021; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026053103308](https://openairdocs.org/sdr/DALA2026053103308.md): Light · inoperative · May 31, 2026 · N115DU · Airbus BD5001A10 · Emergency Lighting
  > LEFT FWD FUSELAGE EXTERNAL EMERGENCY LIGHT AND L/H OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED LIGHTS REF A220 AMP 33-55. OPS CHECKS GOOD. (LP 8901899 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2025061004417](https://openairdocs.org/sdr/DALA2025061004417.md): Light · damaged · Jun 5, 2025 · N115DU · Airbus BD5001A10 · Emergency Lighting
  > LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WITH WATER DAMAGE (4) NEED REPLACE. REMOVED AND REPLACED LEFT AND RIGHT OVERWING EMERGENCY LIGHTS. PERFORMED EXTERNAL EMERGENCY LIGHTS OPERATION TEST, OPS CHECK GOOD. IAW A220 AMP BD500-A-J33-55-02-02AAA-520A-A, BD500-A
- [SDR DALA2025052704039](https://openairdocs.org/sdr/DALA2025052704039.md): Floor Panel · corroded · May 21, 2025 · N115DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION ALONG FWD AND INBOARD EDGES OF FSD ENTRY FLOOR PANEL 222KRF. REMOVED AND REPLACED APD ENTRY FLOOR PANEL 222KRF IAW A220 AMP BD500-A-J53-00-47-13AAA-520A-A AND AMP BD500-A-J53-00-47-12AAA- 720A-2. (LP# 0978241)
- [SDR DALA2025052704038](https://openairdocs.org/sdr/DALA2025052704038.md): Floor Panel · corroded · May 21, 2025 · N115DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION ON AFT INBOARD CORNER OF APD ENTRY FLOOR PANEL 241MLF. REMOVED AND REPLACED APD ENTRY FLOOR PANEL 241MLF IAW A220 AMP BD500-A-J53-00-47-13AAA-520A-A AND AMP BD500-A-J53-00-47-13AAA- 720A-A. (LP# 0978234)
- [SDR DALA2025052003865](https://openairdocs.org/sdr/DALA2025052003865.md): Seat Track · corroded · May 15, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON LOWER AREA SEAT TRACK BETWEEN FRAME 47 AND 48, AT RBL 43, WL 151. REMOVED AND REPLACED SEAT TRACK FROM FR 43-51 + 10" RBL 43 IAW BOMBARDIER DWG# C01335700 REV-H AND TOPP 30-10-50 STP 7 PG 3. (LP# 0969980)
- [SDR DALA2025050603475](https://openairdocs.org/sdr/DALA2025050603475.md): Floor Panel · corroded · May 5, 2025 · N115DU · Airbus BD5001A10 · Fuselage Floor Panel
  > ***CORROSION*** ALONG FWD EDGE, AFT INBOARD CORNER AND AFT EDGE OF ASD ENTRY FLOOR PANEL 242MRF. REMOVED AND REPLACED FLOOR PANEL 242MRF IAW A220 AMP BD500- A-J53-00-47-14AAA-520A-A AND A220 AMP BD500-A-J53-62-33-02AAA- 720A-A. (LP# 0950393)
- [SDR DALA2025050103372](https://openairdocs.org/sdr/DALA2025050103372.md): Seat Track · corroded · Apr 29, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON SEAT TRACK @ 22 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, LBL23, WL151.5. REMOVED AND REPLACE SEAT TRACK BETWEEN FR 61 TO FR 74 +8" LBL 23 WL 151.5 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV G. (LP# 0940147)
- [SDR DALA2025050603470](https://openairdocs.org/sdr/DALA2025050603470.md): Cargo Track · corroded · Apr 24, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON SEAT TRACK @ 12.5 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, RBL23, WL151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 61 TO FR 74, RBL23, WL 151.5. IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER PL: C01342701 REV: G. (LP# 094
- [SDR DALA2025042403231](https://openairdocs.org/sdr/DALA2025042403231.md): Seat Track · corroded · Apr 23, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK @ 4 INCHES FWD OF FR20 TO FR20, RBL43, WL151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR20 TO FR30 RBL43 WL 151.5 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A, BOMBARDIER PL: C01712000 REV: -A AND BOMBARDIER PL: C02312600 REV: E. (LP# 09
- [SDR DALA2025042203162](https://openairdocs.org/sdr/DALA2025042203162.md): Seat Track · corroded · Apr 16, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON SEAT TRACK @ 4 INCHES FWD OF FR20 TO 1.5 INCHES AFT OF FR20, RBL23, WL151.5. REMOVED AND REPLACED SEAT TRACK FROM FR 20 TO FR 34 RBL 23 WL 151.5 IAW DWG BOMBARDIER PL C02312600 REV E AND ASRP A220BD500- A-J51-42-21-00AAA-078A-A. (LP# 0918617
- [SDR DALA2025042103103](https://openairdocs.org/sdr/DALA2025042103103.md): Seat Track · corroded · Apr 15, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK @ 4 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, LBL43, WL151.5. REMOVED SEAT TRACK DAMAGED FROM FR 74 TO FR61 LBL 43 WL 151.5 AND INSTALL NEW SEAT TRACK PER A220 ASRP BD500-A-J51-42-21-00AAA -078A-A AND BOMBARDIER PL C01342701 REV E. (L
- [SDR DALA2025041002787](https://openairdocs.org/sdr/DALA2025041002787.md): Seat Track · corroded · Apr 7, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON SEAT TRACK @ 12.5 INCHES FWD OF FR74 TO 2 INCHES AFT OF FR74, RBL43, WL151.5. REMOVED AND REPLACE SEAT TRACK BETWEEN FR57+13" TO 74+6" RBL43, WL 151.5 IAW BOMBARDIER DWG: C01342701, REV G AND A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP# 09
- [SDR DALA2025041002786](https://openairdocs.org/sdr/DALA2025041002786.md): Seat Track · corroded · Apr 7, 2025 · N115DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON SEAT TRACK @ 5 INCHES FWD OF FR22 TO 15 INCHES AFT OF FR22, LBL43, WL151.5. REMOVED AND REPLACED SEAT TRACK LBL43 FR 20 TO FR 30 IAW A220 ASRP BD500-A-J51-40-11-01AAA-652A-A, ASRP BD500-A-J51-42-21- 00AAA-078A-A AND DWG BOMBARDIER PL 0231260
- [SDR DALA2025060904386](https://openairdocs.org/sdr/DALA2025060904386.md): Orifice · blocked · Apr 1, 2025 · N115DU · Airbus BD5001A10 · Escape Slide
  > THE VALVE PIN HOLE IS PARTIALLY OR FULLY BLOCKED AND THE SAFETY PIN CAN'T BE INSTALLED ON RH OWEE DOOR SLIDE. THE SLIDE WILL NEED TO BE DEPLOYED. REMOVED AND INSTALLED R/H OWEE DOOR SLIDE IAW A220 TASK CARD NO: 2563-4005. (LP# 0890038)
- [SDR DALA2025031001817](https://openairdocs.org/sdr/DALA2025031001817.md): Control Lever · faulty · Mar 8, 2025 · N115DU · Airbus BD5001A10 · Landing Gear Selector
  > SHIP 8115 - DIV - TO LAX DUE TO "NORM BRAKE FAIL MESSAGE". REPLACED LANDING GEAR CONTROL LEVER. (LP# 6875590)
- [SDR DALA2024091208951](https://openairdocs.org/sdr/DALA2024091208951.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR5 HAS EVIDENCE OF CORROSION ON UPPER AFT AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. RH SLAT TRACK NBR 5 UPPER AFT SURFACE BLENDED PER AMDS W/C 5742 -010280-02B PERFORMED HFEC AT
- [SDR DALA2024091208950](https://openairdocs.org/sdr/DALA2024091208950.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. RH SLAT TRACK NBR5 UPPER FWD SURFACE BLENDED PER AMDS W/C 5742- 010280-02B PERFORMED HFEC AT
- [SDR DALA2024091208949](https://openairdocs.org/sdr/DALA2024091208949.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. RH SLAT TRACK NBR 6 UPPER FWD SURFACE BLENDED PER AMDS W/C 5742- 010280-02B PERFORMED HFEC A
- [SDR DALA2024091208948](https://openairdocs.org/sdr/DALA2024091208948.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR4 HAS EVIDENCE OF CORROSION ON UPPER FWD AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. LH SLAT TRACK NBR4 UPPER FWD SURFACE BLENDED PER AMDS W/C 5742- 010280-02B PERFORMED HFEC AT
- [SDR DALA2024091208947](https://openairdocs.org/sdr/DALA2024091208947.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 HAS EVIDENCE OF CORROSION ON UPPER AFT AND HAS PREVIOUS REWORK, BLEND PER AMDS W/C 5742-010280-02B AND REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. LH SLAT TRACK NBR 5 UPPER AFT SURFACE BLENDED PER AMDS W/C 5742- 010280-02B PERFORMED HFEC A
- [SDR DALA2024091208946](https://openairdocs.org/sdr/DALA2024091208946.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND HAS PREVIOUS REWORK BLEND PER AMDS W/C 5742-01280 AND REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. RH SLAT TRACK NBR 1 UPPER FWD SURFACE BLENDED IAW AMDS W/C 5742- 01280-02B. NDT INSPECTION C/
- [SDR DALA2024091208945](https://openairdocs.org/sdr/DALA2024091208945.md): Slat Track · corroded · Sep 7, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND HAS PREVIOUS REWORK BLEND PER AMDS W/C 5742-01280 AND REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. RH SLAT TRACK NBR 1 UPPER AFT SURFACE BLENDED IAW AMDS W/C 5742- 01280-02B. NDT INSPECTION C/
- [SDR DALA2024090908864](https://openairdocs.org/sdr/DALA2024090908864.md): Slat Track · corroded · Sep 6, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH PRI AND PERFORMED HFEC OF BLENDED AREA PER ANDTP BD500-A-J51-01-20-01AAAA
- [SDR DALA2024051505240](https://openairdocs.org/sdr/DALA2024051505240.md): None · none · May 15, 2024 · N115DU · Airbus BD5001A10 · Standard Practices/Structures
  > THIS IS BEING CREATED TO ACCOMPLISH ONE-TIME INSPECTION FOR ER/A 618031-14. ACCOMPLISH ER/A SECTION III ONE-TIME INSPECTION AFTER ACCOMPLISHMENT OF SECTION I TIME-LIMITED REPAIR. SECTION III ONE-TIME INSPECTION ACCOMPLISHES A TAP TEST, DVI AND UT INSPECTION AT
- [SDR DALA2024020901832](https://openairdocs.org/sdr/DALA2024020901832.md): Packing · leaking · Feb 7, 2024 · N115DU · Airbus BD5001A10 · APU Start/Ignition System
  > WHEN APU FIRST STARTS STRONG DIRTY SOCKS FEET SMELL IN CABIN/ COCKPIT. UPON STARTING APU AFTER LANDING BURNT TOAST SMELL IN CABIN/COCKPIT. AS PER NO GO ODI PERFORMED A/C 0550-2002. BEGAN W/C 0550-2001 UP TO STEP 4 (DP 230877) C/W REMAINING STEPS ON A220 AMDS W
- [SDR DALA2024011800789](https://openairdocs.org/sdr/DALA2024011800789.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #9 UPPER INBOARD AFT SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF. AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NO
- [SDR DALA2024011800788](https://openairdocs.org/sdr/DALA2024011800788.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #8 LWR AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NO FURTHER REWORK R
- [SDR DALA2024011800787](https://openairdocs.org/sdr/DALA2024011800787.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 HAS WORN SPOT ON UPPER INBOARD AFT SIDE AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ERA 607388-14AD STEP 9. [5333]. WEAR MARK MEETS PRI STEP 9 CRITREIA. NO FURTHER REWO
- [SDR DALA2024011800785](https://openairdocs.org/sdr/DALA2024011800785.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #8 LWR FWD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 9 [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NO FURTHER REWORK R
- [SDR DALA2024011800781](https://openairdocs.org/sdr/DALA2024011800781.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #1 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORTING REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEN
- [SDR DALA2024011800778](https://openairdocs.org/sdr/DALA2024011800778.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #4 LWR FWD HAS EVIDENCE OF CORROSION REF AA5742- 01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA
- [SDR DALA2024011800777](https://openairdocs.org/sdr/DALA2024011800777.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #3 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14D STEP 9. [5333]. CORROSION BLEND MEE
- [SDR DALA2024011800775](https://openairdocs.org/sdr/DALA2024011800775.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND M
- [SDR DALA2024011800773](https://openairdocs.org/sdr/DALA2024011800773.md): Roller · worn · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH OUTBOARD LWR SIDE OF SLAT TRACK #4 HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FLIGHT. WEAR MARKS MEETS PRI STEP 9 CRITERIA. NO FURTHER REWORK REQUIRED. (LP# 0151210)
- [SDR DALA2024011800772](https://openairdocs.org/sdr/DALA2024011800772.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8. CRITERIA. NO FURTHER REWO
- [SDR DALA2024011800771](https://openairdocs.org/sdr/DALA2024011800771.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEN
- [SDR DALA2024011800769](https://openairdocs.org/sdr/DALA2024011800769.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND
- [SDR DALA2024011800768](https://openairdocs.org/sdr/DALA2024011800768.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC 5333] CORROSION BLEND MEETS CRITERIA NO FURTHER
- [SDR DALA2024011800767](https://openairdocs.org/sdr/DALA2024011800767.md): Slat Track · corroded · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #9 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA. 607388- 14AD STEP 9. [5333]. CORROSION BLEND M
- [SDR DALA2024011800766](https://openairdocs.org/sdr/DALA2024011800766.md): Slat Track · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 5 LOWER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9[QC 5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHER REWORK
- [SDR DALA2024011600673](https://openairdocs.org/sdr/DALA2024011600673.md): Slat Track · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #2 LWR AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ERA 607388-14AD STEP 9. [5333]. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NO FURTH
- [SDR DALA2024011600671](https://openairdocs.org/sdr/DALA2024011600671.md): Unknown · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #4 LOWER AFT SURFACE HAS EVIDENCE OF ROLLER WEAR AND PREVIOUS REWORK REF AA5742-01028-02B LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. 0748182 W C/W PRI ERA 607388-14AD STEP 3. (1832863). C/W PRI ERA 607388- 14AD STEP 9. (5333). CORRO
- [SDR DALA2024011600670](https://openairdocs.org/sdr/DALA2024011600670.md): Unknown · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > COPY OF NRT #25 DUE TO LOST PAPERWORK. RH SLAT TRACK #4 PINION TEETH HAS EVIDENCE OF CORROSION. REF. AA5742-01028-02B. LIAISONENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD REV B STEP 1-16. (LP# 0151121)
- [SDR DALA2024011600669](https://openairdocs.org/sdr/DALA2024011600669.md): Slat Track · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B LIAISONENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 12JAN24 0907 UTC 02 CORR BY DAVIS 00748182 IAH 12JAN24 ATA 5742 RII: N ENTR 007
- [SDR DALA2024011600665](https://openairdocs.org/sdr/DALA2024011600665.md): Unknown · unknown · Jan 12, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #2 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. AA5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. C/W PRI ERA 607388-14AD STEP 3. [1832863]. C/W PRI ERA 607388- 14AD STEP 9. [5333]. CORROSION BLEND
- [SDR DALA2024012901254](https://openairdocs.org/sdr/DALA2024012901254.md): Slat Track · corroded · Jan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 8 CRITERIA, NO FURTHER REWORK REQUIRED; REPAIRED LH SLAT T
- [SDR DALA2024011800786](https://openairdocs.org/sdr/DALA2024011800786.md): Slat Track · corroded · Jan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 8 UPPER FORWARD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURT
- [SDR DALA2024011800784](https://openairdocs.org/sdr/DALA2024011800784.md): Slat Track · corroded · Jan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.C/W PRI ER/A 607387-14AD STEP 9[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO F
- [SDR DALA2024011800783](https://openairdocs.org/sdr/DALA2024011800783.md): Slat Track · corroded · Jan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 4 UPPER FORWARD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 C

Next page: https://openairdocs.org/aircraft/N115DU/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 = 'N115DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N115DU/reports

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