# Service difficulty reports: N117DU

A list on [N117DU](https://openairdocs.org/aircraft/N117DU.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 3 · 112 reports

- [SDR DALA2026082504825](https://openairdocs.org/sdr/DALA2026082504825.md): Skin · corroded · Jul 16, 2026 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ERA 627451-14 REV B: MID FUSELAGE SKIN - FRAME 34-35, S36L-S36R - CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN 52,500 FLIGHT HOURS OR 30,000 FLIGHT CYCLES FROM TIME OF SECT. I REPAIR AT 15,269 FH AND 6,972 FC (WITHIN AIRCRA
- [SDR DALA2026031201742](https://openairdocs.org/sdr/DALA2026031201742.md): Battery Pack · inoperative · Mar 9, 2026 · N117DU · Airbus BD5001A10 · Emergency Lighting
  > DURING SVC FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. CONFIRMED EXIT SIGN ASSEMBLY WORKED NORMAL BY SWAPPING TO DIFFERENT LOCATION IAW AMP 33-54. REMOVED EPSU BATTERY IAW AMP 33-51-03AAA-520A-A. WAITING FOR NEW SERVICEABLE PART INSTALLATION. KIM 6275
- [SDR DALA2026021701093](https://openairdocs.org/sdr/DALA2026021701093.md): Hydraulic Line · leaking · Feb 15, 2026 · N117DU · Airbus BD5001A10 · Hydraulic System, Main
  > PERFORMED AN AIR TURN BACK TO MSP DUE TO FUMES IN THE COCKPIT AND CABIN. SUSPECT LEFT ENGINE OVERSERVICED AND FOUND HYD LEAK AT PYLON DISCONNECT WITH EVIDENCE OF HYDRAULIC FLUID INTRUSION AT CLAMP FORWARD OF PRECOOLER. (LP 8110358)
- [SDR DALA2025122309354](https://openairdocs.org/sdr/DALA2025122309354.md): Seal · leaking · Dec 17, 2025 · N117DU · Airbus BD5001A10 · Turbine Engine Oil System
  > SHIP 8117 RETURNED TO SAT DUE TO ODOR IN CABIN. FOUND OIL IN #2 SPINNER. REPLACED SEAL REF PW1000G-A-72-00-11. WHILE PERFORMING P-TRAK PROCEDURE PER WORK CARD 0550-2001, FOUND PARTICULATE MATTER READINGS INCONCLUSIVE TO DEFINITE SOURCE. DUE TO HISTORY ON #1
- [SDR DALA2025112508592](https://openairdocs.org/sdr/DALA2025112508592.md): Hydraulic Line · leaking · Nov 21, 2025 · N117DU · Airbus BD5001A10 · Hydraulic System, Main
  > ATB- RETURNED TO MSP DUE TO DIRTY SOCK FUME IN CABIN. EMERGENCY WAS DECLARED. LEAK FOUND BETWEEN HPC AND LPC DUE TO HYDRAULIC LINE LOOSE. SAME TIGHTENED. (LP# 7601488)
- [SDR DALA2025110308039](https://openairdocs.org/sdr/DALA2025110308039.md): Engine · odor · Oct 24, 2025 · N117DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > FUMES EVENT WHEN APU ON, ALSO WITH ENGINE BLEEDS ON. REPLACED NR 1 ENGINE. (LP 7601408, 1283162).
- [SDR DALA2025080705930](https://openairdocs.org/sdr/DALA2025080705930.md): Skin · debonded · Aug 1, 2025 · N117DU · Airbus BD5001A10 · Horizontal Stabilizer, Plate/Skin
  > ER/A 601550-14 REV A. A220 / RH HORIZONTAL STABILIZER / UPPER AND LOWER SKINS / @ REAR SPAR / HINGE RIB 2 TO HINGE RIB 3 / DISBOND. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 601550-14 REV A, SEC. V WITHIN 18,500 FH FROM 7,614 TOTAL FH (WITHIN 1
- [SDR DALA2026073004414](https://openairdocs.org/sdr/DALA2026073004414.md): Skin · debonded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Horizontal Stabilizer, Plate/Skin
  > DTE / MONITOR INSPECTION LOG REF. ER/A 601550-14 REV A. A220 / HORIZONTAL STABILIZER / UPPER AND LOWER SKINS / @ REAR SPAR / HINGE RIB 2 TO HINGE RIB 3 / DISBOND. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM 31
- [SDR DALA2025080505879](https://openairdocs.org/sdr/DALA2025080505879.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14 REV ORIGINAL ASSOCIATED ER/A 1
- [SDR DALA2025080505878](https://openairdocs.org/sdr/DALA2025080505878.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/A 14-627451 ADDE
- [SDR DALA2025080505877](https://openairdocs.org/sdr/DALA2025080505877.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FRAMES 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN. FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14.
- [SDR DALA2025080505876](https://openairdocs.org/sdr/DALA2025080505876.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN & FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/A 14-627451 ADDED.
- [SDR DALA2025080505875](https://openairdocs.org/sdr/DALA2025080505875.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L HAD SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW DELTA ERA 627451-14. REMOVE
- [SDR DALA2025080505874](https://openairdocs.org/sdr/DALA2025080505874.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE 6 INCHES AFT OF DRAIN FR 34 - 35. S36R - 36L. SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R-36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/
- [SDR DALA2025080505873](https://openairdocs.org/sdr/DALA2025080505873.md): Skin · corroded · Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FWD WTBF AT LWR FUSELAGE, 6 INCHES AFT OF DRAIN FR 34 - 35, S36R - 36L SIGNS OF CORROSION. REMOVED CORROSION ON LOWER SKIN FR 34 - 35, S36R -36L, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-31-01. PERFORMED SKIN REPAIR IAW ERA 627451-14. ASSOCIATED ER/A
- [SDR DALA2025072905699](https://openairdocs.org/sdr/DALA2025072905699.md): Skin · corroded · Jul 24, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL SKIN FR79, AFT LAP JOINT, STRINGER 36 TO 37L. BLENDED CORROSION ON EXTERNAL SKIN @ LAP JOINT FR 79, STGR 36R- 36L IAW A220 ASRP 31-21-06-01. FOUND OUT OF LIMITS IAW A220 ASRP 53-61-01. RESTORED FINISH TO AFFECTED AREA IAW ERA 627700
- [SDR DALA2025072905698](https://openairdocs.org/sdr/DALA2025072905698.md): Skin · corroded · Jul 24, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL SKIN FR77 TO FR78 AROUND STRINGER 36. BLENDED OUT CORROSION ON EXTERNAL SKIN @ FR 77-78 @ STGR 36 IAW A220 ASRP 51-21-06-01AAA. FOUND OUT OF LIMITS IAW A220 ASRP 53- 61-01. RESTORED FINISH TO AFFECTED AREA IAW ERA 627700-14 REV. ASS
- [SDR DALA2025072105449](https://openairdocs.org/sdr/DALA2025072105449.md): Skin · corroded · Jul 17, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL SKIN FR79, AFT LAP JOINT, STRINGER 36 TO 37L. BLENDED CORROSION ON EXTERNAL SKIN @ LAP JOINT FR 79, STGR 36R- 36L IAW A220 ASRP 31-21-06-01. FOUND OUT OF LIMITS IAW A220 ASRP 53-61-01. RESTORED FINISH TO AFFECTED AREA IAW ERA 627700
- [SDR DALA2025072105448](https://openairdocs.org/sdr/DALA2025072105448.md): Skin · corroded · Jul 17, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON EXTERNAL SKIN FR77 TO FR78 AROUND STRINGER 36. BLENDED OUT CORROSION ON EXTERNAL SKIN @ FR 77-78 @ STGR 36 IAW A220 ASRP 51-21-06-01AAA. FOUND OUT OF LIMITS IAW A220 ASRP 53- 61-01. RESTORED FINISH TO AFFECTED AREA IAW ERA 627700-14 REV. O P
- [SDR DALA2026031101705](https://openairdocs.org/sdr/DALA2026031101705.md): Scuff Plate · corroded · Jul 9, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > DOOR LOWER SCUFF PLATE FASTENER HOLES 20OL, 19OL, 18OL AND 16OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD CARGO DOOR LOWER SCUFF PLATE, FOUND OUT OF LIMITS IAW J51-21-06, J53-21-01. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW DELTA ERA 627318-
- [SDR DALA2026031101704](https://openairdocs.org/sdr/DALA2026031101704.md): Door Sill · corroded · Jul 8, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Structure
  > DOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA OF FWD CARGO DOOR LWR SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-25. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW DELTA ERA 627232-14 REV. ORIGINAL. (LP#
- [SDR DALA2026031101703](https://openairdocs.org/sdr/DALA2026031101703.md): Door Sill · corroded · Jul 8, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Structure
  > DOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA ON AFT CARGO DOOR LOWER SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-25. RESTORED FINISH, ACCOMPLISHED ALL WORK IAW DELTA ERA 627233-14 REV.. ORIGINAL. ASSO
- [SDR DALA2026031101700](https://openairdocs.org/sdr/DALA2026031101700.md): Scuff Plate · corroded · Jul 3, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > L1 DOOR SCUFF PLATE FASTENER HOLES 15OL, 14OL, 11OL, 5OL, 4OL, 3OL, 2OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD PAX DOOR LWR SCUFF PLATE FOUND OUT OF LIMITS IAW A220 ASRPJ51-21-06, J53-21-02. RESTORED FINISH AND ACCOMPLISHED ALL WORK
- [SDR DALA2026031101702](https://openairdocs.org/sdr/DALA2026031101702.md): Scuff Plate · corroded · Jun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR, LOWER SCUFF PLATE FASTENER HOLES 11OL, 10OL, 9OL, 8OL, 7OL, 6OL, 5OL, 4OL, 3OL, 2OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON AFT CARGO DOOR LOWER SCUFF PLATE, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-01. RESTORED
- [SDR DALA2026031101701](https://openairdocs.org/sdr/DALA2026031101701.md): Scuff Plate · corroded · Jun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR, LOWER SCUFF PLATE FASTENER HOLES 11OU AND 10OU HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON FWD CARGO DOOR UPPER SCUFF PLATE, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-01. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW DELTA ER
- [SDR DALA2026031101699](https://openairdocs.org/sdr/DALA2026031101699.md): Scuff Plate · corroded · Jun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > R1 DOOR SCUFF PLATE FASTENER HOLES 15OL, 14OL, 13OL, 12OL, 11OL, 5OL, 3OL, AND 1OL HAVE CORROSION. REMOVED CORROSION, EVALUATED AREA ON R1 DOOR SCUFF PLATE, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-01. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW D
- [SDR DALA2025062504761](https://openairdocs.org/sdr/DALA2025062504761.md): Seat Track · corroded · Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT RH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED DAMAGED AFT L/H I/B SEAT TRACK IAW A220 ASRP J51-21-06, J53-61- 49, J51-40-11, J51-42-20. (LP# 1038128)
- [SDR DALA2025062504760](https://openairdocs.org/sdr/DALA2025062504760.md): Seat Track · corroded · Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED DAMAGED AFT L/H O/B SEAT TRACK IAW A220 ASRP J51-21-06, J53-61- 49, J51-40-11, J51-42-20. (LP# 1038119)
- [SDR DALA2025062504759](https://openairdocs.org/sdr/DALA2025062504759.md): Seat Track · corroded · Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD LH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION FOUND WITH OUT LIMITS, REMOVED AND REPLACED FWD LH I/B SEAT TRACK IAW A220 J51-42-20, 51-40-11, 53-21-49. (LP# 1038113)
- [SDR DALA2025062504758](https://openairdocs.org/sdr/DALA2025062504758.md): Seat Track · corroded · Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD RH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED FWD R/H O/B SEAT TRACK IAW A220 ASRP J51-21-06, J53-21-49, J51-40- 11 AND J51-42-20. (LP# 1038100)
- [SDR DALA2025062404721](https://openairdocs.org/sdr/DALA2025062404721.md): Seat Track · corroded · Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT RH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED AFT R/H O/B SEAT TRACK IAW A220 ASRP J51-21-06, J53-61-49, J51-40- 11 AND J51-42-21. (LP# 1035461)
- [SDR DALA2025062404720](https://openairdocs.org/sdr/DALA2025062404720.md): Seat Track · corroded · Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT LH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR72 TO FR74. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED AND REPLACED AFT L/H I/B SEAT TRACK IAW A220 ASRP J51-21-06, J51-61-49, J51-40- 11, J51-42-20. (LP# 1035454)
- [SDR DALA2025062404719](https://openairdocs.org/sdr/DALA2025062404719.md): Seat Track · corroded · Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD LH, O/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED AND REPLACED SEAT TRACK AT FWD L/H O/B IAW A220 ASRP J51 -42-21, J51-21-06, J51-40-11 JOB COMPLETE, AFTER CORROSION REMOVED FOUND OUT OF LIMITS. (LP# 1035448)
- [SDR DALA2025062404718](https://openairdocs.org/sdr/DALA2025062404718.md): Seat Track · corroded · Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD RH, I/B SEAT TRACK HAS EVIDENCE OF CORROSION FROM FR22 TO FR24. REMOVED CORROSION AND FOUND FWD R/H I/B SEAT TRACK OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-49. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW A220 ASRP J51-42-20, J51-40-11. (LP# 1035442)
- [SDR DALA2025031201906](https://openairdocs.org/sdr/DALA2025031201906.md): Light · inoperative · Mar 12, 2025 · N117DU · Airbus BD5001A10 · Emergency Lighting
  > R2 EXTERNAL EMERGENCY LIGHT INOP. R/R R2 EXTERNAL EMERGENCY LIGHT IAW A220 AMP 33-55. OPS CHECK OK. (LP# 7248522)
- [SDR DALA2024120311423](https://openairdocs.org/sdr/DALA2024120311423.md): Light · inoperative · Nov 26, 2024 · N117DU · Airbus BD5001A10 · Emergency Lighting
  > DURING TEST OF EMERGENCY LIGHTS, AISLE LIGHTS FOUND INOP. INSPECTED INTERNAL EMERGENCY LIGHTS PER A220 AMP 33-52-00. NO FAULTS FOUND. (LP# 5724699)
- [SDR DALA2024102310334](https://openairdocs.org/sdr/DALA2024102310334.md): Cover · missing · Oct 19, 2024 · N117DU · Airbus BD5001A10 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. OVER HEAD EMERGENCY FLOODLIGHT IS MISSING COVER / INTERIOR. RE-SECURED OVERHEAD EMERGENCY FLOOD LIGHT COVER AS REQUIRED. A/C OK FOR SVC. (LP# 0616441)
- [SDR DALA2024080707862](https://openairdocs.org/sdr/DALA2024080707862.md): Cable · failed · Aug 3, 2024 · N117DU · Airbus BD5001A10 · Communications System Wiring
  > SHIP 8117 - SMK - RETURNED TO GATE DUE TO SMOKE FROM ROW 17 IN-SEAT MONITOR USB. CORRECTIVE ACTION: PLACED IN-SEAT POWER MASTER CONTROL RELAY ON MEL 44-20-01. R/R CABLE ASSEMBLY AT SEAT ROW 16 CDE. (LP# 5723430)
- [SDR DALA2024032803890](https://openairdocs.org/sdr/DALA2024032803890.md): Skin · damaged · Mar 26, 2024 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / EXTERNAL DOUBLER REPAIR AT FR49 AND STGR8L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGE 3 DTA APPROVAL. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAG
- [SDR DALA2024032803889](https://openairdocs.org/sdr/DALA2024032803889.md): Skin · damaged · Mar 26, 2024 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / REPAIRED FASTENER AT FR50 AND ABOVE STGR7L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGE 3 DTA APPROVAL. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAG
- [SDR DALA2024011900871](https://openairdocs.org/sdr/DALA2024011900871.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #10 UPPER FORWARD SURFACE PER SUMMARY OF CORRECTIVE ACTION C/W PRI 607306-14AD REV O, 1 AND ERA 607306- 14AD REV E MATCH. (LP#
- [SDR DALA2024011900870](https://openairdocs.org/sdr/DALA2024011900870.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #10 LOWER AFT SURFACE PER SUMMARY OF CORRECTIVE ACTION C/W PRI 607306-14AD REV O, 1 AND ERA 607306- 14AD REV E MATCH. (LP# 0155
- [SDR DALA2024011900869](https://openairdocs.org/sdr/DALA2024011900869.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B, REPAIRED R/H SLAT TRACK #8 LOWER AFT SURFACE PER SUMMARY OF CORRECTIVE ACTION C/W PRI 607306-14AD REV O, 1 AND ERA 607306- 14AD REV E MATCH. (LP# 015516
- [SDR DALA2024011900868](https://openairdocs.org/sdr/DALA2024011900868.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR#10 UPPER FWD SURFACE PER SUMMARY OF CORRECTIVE ACTIONS - C/W PRI 607305-14AD REV 0, 1, 3 AND ERA 60735-14AD REV B MATCHED. (
- [SDR DALA2024011900867](https://openairdocs.org/sdr/DALA2024011900867.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 LOWER FWD SURFACE PER SUMMARY OF CORRECTIOIN ACTIONS. C/W PRI 607305-14AD REV 0,1,2 AND ERA 607305-14AD REV B - MATCHED. (
- [SDR DALA2024011900866](https://openairdocs.org/sdr/DALA2024011900866.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #9 IB LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR #9 IB LOWER FWD SIDE PER SUMMARY OF CORRECTIVE ACTIONS - C/W PRI 607305-14AD REV 0, 1, 3 AND ERA 60735-14AD REV B MATCHED. (L
- [SDR DALA2024011900865](https://openairdocs.org/sdr/DALA2024011900865.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 OUTBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 OUTBOARD LOWER FWD SIDE PER SUMMARY OF CORRECTIOIN ACTIONS. C/W PRI 607305-14AD REV 0,1,2 AND ERA 607305-14AD REV B
- [SDR DALA2024011900864](https://openairdocs.org/sdr/DALA2024011900864.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #9 OB LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR #9 OB LOWER FWD SIDE PER SUMMARY OF CORRECTIVE ACTIONS - C/W PRI 607305-14AD REV 0, 1, 3 AND ERA 60735-14AD REV B MATCHED. (L
- [SDR DALA2024011900863](https://openairdocs.org/sdr/DALA2024011900863.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 INBOARD LOWER FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 INBOARD LOWER FWD SIDE PER SUMMARY OF CORRECTIOIN ACTIONS. C/W PRI 607305-14AD REV 0,1,2 AND ERA 607305-14AD REV B -
- [SDR DALA2024011900862](https://openairdocs.org/sdr/DALA2024011900862.md): Slat Track · corroded · Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 OUTBOARD UPPER AFT SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 OUTBOARD UPPER AFT SIDE PER SUMMARY OF CORRECTIOIN ACTIONS. C/W PRI 607305-14AD REV 0,1,2 AND ERA 607305-14AD REV B

Next page: https://openairdocs.org/aircraft/N117DU/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 = 'N117DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N117DU/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.