N115DU

Service difficulty reports · 81

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 = 'N115DU' 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 DALA2024011800782Slat Track · corrodedL/H SLAT TRACK NBR 4 UPPER FORWARD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. 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 FURTHJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011800780Slat Track · corrodedL/H SLAT TRACK NBR 6 UPPER 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 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011800779Slat Track · corrodedL/H SLAT TRACK NBR 10 LOWER AFT 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 FURTHERJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011800776Slat Track · corrodedL/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. 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 FJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011800774Slat Track · corrodedL/H SLAT TRACK NBR 1 UPPER AFT HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.L/H PRI ER/A 607387-14AD STEP 3 [QC 5333] C/W PRI ER/A 607387- 14AD STEP 9. CORROSION BLEND MEEJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011800770Slat Track · corrodedL/H SLAT TRACK NBR 1 LOWER FORWARD 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[QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIAJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600676Slat Track · unknownL/H SLAT TRACK NBR 8 UPPER AFT HAS EVIDENCE OF CORROSIN AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA NO FURTHER REWORK RJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600675Slat Track · unknownL/H SLAT TRACK NBR 6 UPPER FORWARD 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 CRITERIJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600674Slat Track · unknownL/H SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. RII: N ENTR 00748182 W C/W PRI ER/A 607387-14AD STEP 9 [QC5333] CORROSION BLEND MEETSJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600672Slat Track · unknownL/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 9 [QC5333] CORROSION BLEND MEETS PRI STEP 8 CRITERIA, NO FUJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600668Slat Track · corrodedL/H SLAT TRACK NBR 8 LWR FWD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF AA5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. C/W PRI ER/A 607387-14AD STEP 9 QC 5333. CORROSION BLEND MEETS PRI STEP 8 CRITERIA, NO FURTHER REWOJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024011600664Unknown · unknownL/H SLAT TRACK NUMBER 5 LOWER FORWARD 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. CORROSION BLEND MEETS PRI STEP 8 CRITERIA. NJan 11, 2024 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2023032002086Unknown · unknownSHIP 8115 - DIV - TO LAS DUE TO "L GEN FAIL" CATION MESSAGE FOLLOWED BY "APU FAIL" WARNING MESSAGE. CORRECTIVE ACTION: REPLACED VARIABLE FREQUENCY GENERATOR (VFG) AND GENERATOR CONTROL UNIT (GCU). (LP# 9493830)Mar 18, 2023 · N115DU · Airbus BD5001A10 · Alternator-Generator DriveSDR DALA2023021001068None · noneSTRONG ODOR AFTER APU START AND APU BLEED TURNED ON. SMELLED LIKE A SHARPIE MARKER. OCCURED DURING TAXI IN AFTER LANDING. NORMAL LANDING AUTOBRAKE LO BRAKE TEMPS 06 AND LESS. ER NO GO-ODI 21-72, PERFORMED "SMELL OF SMOKE OR FUMES" EFIM SOLUTION #1-09264. COULDFeb 8, 2023 · N115DU · Airbus A300* · Air Conditioning SystemSDR DALA2023013000752Engine · vibrationAIRCRAFT 8115 -DIV- AIRCRAFT DIVERTED TO SMF DUE TO RIGHT ENGINE VIBE MESSAGE. CORRECTIVE ACTION: RIGHT ENGINE REPLACED.Jan 26, 2023 · N115DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2022070604697None · noneREMOVE #2 LH SLAT ACTUATOR TO FOM. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0275:2021-2065-LH/012 00232 REMOVED AND REINSTALLED LH WING #2 SLAT ACTUATOR IAW A220 AMP 27-81-30. (LP# 2303406)Jul 2, 2022 · N115DU · Airbus BD5001A10 · Leading Edge Slat ActuatorSDR DALA2022063004556None · noneLH WING LEADING EDGE SKIN CRACKED AT #3 SLAT CTR CUT OUT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0275:2021-2065-LH/ 005 00104 COMPLIED WITH PRI 599749-14 REVISION 0, REVISION 1, AND ER/A 599749-14 REVISION ORIGINAL. (LP# 2299001)Jun 29, 2022 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2022063004555None · noneDURING FINAL BUYBACK OF REPAIR OF FIXED LEADING EDGE CUTOUT FOR LEFT WING #2 SLAT TRACK #6, TOOLING DAMAGE WAS NOTED ON THE UPPER TRACK ROLLER SUPPORT FITTING INBOARD AND OUTBOARD SIDES. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONALJun 29, 2022 · N115DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2022061604213Skin · corrodedSHIP 8115 - AFT LOWER FUSELAGE - LIGHT CORROSION ON FUSELAGE SKIN AT FWD INBD CORNER OF WASTE BOX. CORRECTIVE ACTION: REMOVED DAMAGED SKIN AND REPLACED PER PRI 599797-14AD REV 0, 1, 2, 3 AND ER/A 59979 7-14AD REVISION B.(2279352)Jun 15, 2022 · N115DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022061604212Hinge · corrodedSHIP 8115 - WASTE BOX FWD, L/H HINGE ASSEMBLY HAS LIGHT CORROSION. CORRECTIVE ACTION: COMPLIED WITH PRI 599797-14AD REV 0, 1, 2, 3 AND ER/A 599797-14AD REVISION B.(2279302)Jun 15, 2022 · N115DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022061604211Bracket · corrodedSHIP 8115 - WASTE BOX BONDING JUMPER BRACKET IS CORRODED. CORRECTIVE ACTION: COMPLIED WITH PRI 599797-14AD REV 0, 1, 2, 3 AND ER/A 599797-14AD REVISION B.(2279297)Jun 15, 2022 · N115DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022061604210Hinge · corrodedSHIP 8115 - WASTE BOX FWD, R/H HINGE ASSEMBLY HAS LIGHT CORROSION. CORRECTIVE ACTION: REPLACED HINGE AND COMPLIED WITH PRI 59 9797-14AD REV 0, 1, 2, 3 AND ER/A 599797-14AD REVISION B.(2279291)Jun 15, 2022 · N115DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022060804007Hinge · crackedR/H HORIZONTAL STAB. #2 ELEVATOR HINGE RIB CRACKED.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 001 00019 REPAIRED PER PRI 599786-14, REV. 3 AND ERA 599786-14, REV. ORIGINAL. (LP# 2264276)Jun 4, 2022 · N115DU · Airbus BD5001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022060804006Rib · crackedR/H HORIZONTAL STAB. #3 ELEVATOR HINGE RIB CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 003 00021 REPAIRED W/REF. TO PRI 599778-14, REV. 0 AND ERA 599778-14, REV. ORIGINAL. (LP# 2264257)Jun 4, 2022 · N115DU · Airbus BD5001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022060804005Rib · crackedR/H HORIZONTAL STABILIZER, TRAILING EDGE COIL RIB CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 005 00082 REPAIRED PER PRI 599790-14, REV. 0 AND ERA 599790-14, REV. ORIGINAL. (LP# 2264301)Jun 4, 2022 · N115DU · Airbus BD5001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022060804008Skin · damagedER/A 599797-14AD SECTION I ISSUED FOR A FUSELAGE SKIN AND WASTE BOX REPLACEMENT. SECTION I ACCOMPLISHED DURING 'C' CHECK IN MSP PER NR 149, 150, 180. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II REPEAT INSPECTIONS AT 850 FH INTERVALS UNTIL SECTION III. Jun 3, 2022 · N115DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2022041902736Smoke Barrier · fault messageSHIP 8115 -DIV- TO SFO DUE TO AN EQUIPMENT BAY SMOKE FAIL MESSAGE. CORRECTIVE ACTION: REPLACED BOTH EQUIPMENT BAY SMOKE DETECTORS. EXTRACTION DUCT REPAIRED PER ERA 598813-14. (LP# 8798022)Apr 16, 2022 · N115DU · Airbus BD5001A10 · Smoke DetectionSDR DALA2022041902735Dmu · failedSHIP 8115 -DIV- TO LAX DUE TO DMC 1B FAIL. CORRECTIVE ACTION: REPLACED DCM CARD 1B. (LP# 8798018)Apr 15, 2022 · N115DU · Airbus BD5001A10 · Central DisplaySDR DALA2021030501285Seal · missingMISSING FIXED STRUCTURE (IFS) SEALS AND FITTINGS UPPER FAN CASE. TASK PW1000G-A-78-36-22-00B-720A-D LOG-PAGE UPDATED @ 02MAR21 1649 UTC 02 CORR BY MILLER 00850289 MSP 02MAR21 ATA 7831 RII: N ENTR 00850289 W INSTALLED SEALS AND FITTINGS ON UPPER FAN CASE TASK PMar 2, 2021 · N115DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2021101406360None · noneBIRD STRIKE ON LEFT NOSE FUSELAGE. IMPACT DENT FWD FR12 MEASURING 2.5INCH X 0.5 INCHES AND 0.0005 DEEP. DENT IS 10 INCHES ABOUT CUTOUT PANEL. DENT IS NOT PERMITTED PER A220 ASRP 53-11-01-06AAA-661A-A . C/W 10X DVI OF DENT FOR CRACKS, NO DAMAGE FOUND. COMPLIED Oct 24, 2020 · N115DU · Airbus BD5001A10 · Aircraft StructuresSDR DALA2020022501403Bulb · brokenEMERGENCY LIGHT 2R DOOR HAS BROKEN COVER AND BROKEN BULB, REPLACED COVER AND BULBFeb 23, 2020 · N115DU · Airbus BD5001A10 · Emergency Lighting
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