N117DU

Service difficulty reports · 112

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026082504825Skin · corrodedERA 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 AIRCRAJul 16, 2026 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026031201742Battery Pack · inoperativeDURING 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 6275Mar 9, 2026 · N117DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026021701093Hydraulic Line · leakingPERFORMED 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)Feb 15, 2026 · N117DU · Airbus BD5001A10 · Hydraulic System, MainSDR DALA2025122309354Seal · leakingSHIP 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 Dec 17, 2025 · N117DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2025112508592Hydraulic Line · leakingATB- 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)Nov 21, 2025 · N117DU · Airbus BD5001A10 · Hydraulic System, MainSDR DALA2025110308039Engine · odorFUMES EVENT WHEN APU ON, ALSO WITH ENGINE BLEEDS ON. REPLACED NR 1 ENGINE. (LP 7601408, 1283162).Oct 24, 2025 · N117DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2025080705930Skin · debondedER/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 1Aug 1, 2025 · N117DU · Airbus BD5001A10 · Horizontal Stabilizer, Plate/SkinSDR DALA2026073004414Skin · debondedDTE / 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 31Jul 31, 2025 · N117DU · Airbus BD5001A10 · Horizontal Stabilizer, Plate/SkinSDR DALA2025080505879Skin · corrodedLOWER 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 1Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505878Skin · corrodedLOWER 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 ADDEJul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505877Skin · corrodedLOWER 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.Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505876Skin · corrodedLOWER 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.Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505875Skin · corrodedLOWER 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. REMOVEJul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505874Skin · corrodedLOWER 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/Jul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025080505873Skin · corrodedLOWER 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/AJul 31, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025072905699Skin · corrodedCORROSION 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 627700Jul 24, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025072905698Skin · corrodedCORROSION 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. ASSJul 24, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025072105449Skin · corrodedCORROSION 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 627700Jul 17, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025072105448Skin · corrodedCORROSION 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 PJul 17, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026031101705Scuff Plate · corrodedDOOR 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-Jul 9, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026031101704Door Sill · corrodedDOOR 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#Jul 8, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026031101703Door Sill · corrodedDOOR 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. ASSOJul 8, 2025 · N117DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026031101700Scuff Plate · corrodedL1 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 Jul 3, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026031101702Scuff Plate · corrodedAFT 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. RESTOREDJun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026031101701Scuff Plate · corrodedFWD 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 ERJun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026031101699Scuff Plate · corrodedR1 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 DJun 26, 2025 · N117DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025062504761Seat Track · corrodedAFT 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)Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062504760Seat Track · corrodedAFT 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)Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062504759Seat Track · corrodedFWD 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)Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062504758Seat Track · corrodedFWD 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)Jun 21, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404721Seat Track · corrodedAFT 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)Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404720Seat Track · corrodedAFT 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)Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404719Seat Track · corrodedFWD 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)Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404718Seat Track · corrodedFWD 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)Jun 20, 2025 · N117DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025031201906Light · inoperativeR2 EXTERNAL EMERGENCY LIGHT INOP. R/R R2 EXTERNAL EMERGENCY LIGHT IAW A220 AMP 33-55. OPS CHECK OK. (LP# 7248522)Mar 12, 2025 · N117DU · Airbus BD5001A10 · Emergency LightingSDR DALA2024120311423Light · inoperativeDURING TEST OF EMERGENCY LIGHTS, AISLE LIGHTS FOUND INOP. INSPECTED INTERNAL EMERGENCY LIGHTS PER A220 AMP 33-52-00. NO FAULTS FOUND. (LP# 5724699)Nov 26, 2024 · N117DU · Airbus BD5001A10 · Emergency LightingSDR DALA2024102310334Cover · missingEMERGENCY 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)Oct 19, 2024 · N117DU · Airbus BD5001A10 · Emergency LightingSDR DALA2024080707862Cable · failedSHIP 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)Aug 3, 2024 · N117DU · Airbus BD5001A10 · Communications System WiringSDR DALA2024032803890Skin · damagedFUSELAGE 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 STAGMar 26, 2024 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2024032803889Skin · damagedFUSELAGE 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 STAGMar 26, 2024 · N117DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2024011900871Slat Track · corrodedR/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# Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900870Slat Track · corrodedR/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# 0155Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900869Slat Track · corrodedR/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# 015516Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900868Slat Track · corrodedLH 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. (Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900867Slat Track · corrodedLH 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. (Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900866Slat Track · corrodedLH 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. (LJan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900865Slat Track · corrodedLH 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 Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900864Slat Track · corrodedLH 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. (LJan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900863Slat Track · corrodedLH 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 - Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011900862Slat Track · corrodedLH 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 Jan 15, 2024 · N117DU · Airbus BD5001A10 · Leading Edge Devices
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