N122DU

Service difficulty reports · 75

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 = 'N122DU' 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 DALA2026052503145Power Supply · inoperativeEXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHTS / L 4 AND R 4 DOORS EXTERIOR EMERGENCY LIGHTS OUT. REPLACED AFT LT EXTERIOR EMERGENCY LIGHT PER A220 AMM 33-55, OPS CHECK GOOD. REPLACED EPSU (PS5) PER AMM 33-51. OPS CHECK GOOD. (LP 8382986 - AIRCRAFMay 24, 2026 · N122DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026032301954B-Nut · looseDIV- IFSD OF NUMBER 1 ENGINE DUE TO OIL LOSS. CREW REPORTED QUANTITY DROPPED TO 9 QUARTS. FLIGHT MADE AN EMERGENCY LANDING IN DSM. TROUBLESHOT AND FOUND #4 BEARING SCAVENGE TUBE B-NUT LOOSE. CLEANED INSPECTED AND REINSTALLED LINE. PERFORMED WINDMILLING INSPECTMar 23, 2026 · N122DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2025060504286Connector · damagedWHILE WORKING ODI LOG #7412850, FOUND FWD GALLEY COFFEE MAKER PIN AND CONNECTOR A4070P1 SOCKET 5 BURNED FROM ARCING. SOCKET 5 AT CONNECTOR A4070P1 IS BURNT AND ELEC CONNECTOR AT POSITION 102 IS DAMAGED DUE TO ARCING. (571824). C/W SECTION 1: TIME LIMITED ALTERMay 31, 2025 · N122DU · Airbus BD5001A10 · Equipment/Furnishings WiringSDR DALA2025042203167Engine · bird ingestionSHIP 8122-DIV- DIVERTED TO AUS DUE TO DIRTY SOCK SMELL. CORRECTIVE ACTION: FOUND EVIDENCE OF BIRD STRIKE NBR 1 ENGINE. C/O ODI PREVENTION WORKCARDS. PERFORMED BOROSCOPE INSPECTION NTF. R/R UPPER BRACKET PER A220 AMP 79-11. PERFORMED ENGINE #1 GASPATH WASH PER Apr 21, 2025 · N122DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2025031201907Unknown · odorODOR IN CABIN AND COCKPIT ON DESCENT INTO LGA. C/W "NO GO ODI" PREVENTION FOR SMOKE AND FUMES IN CABIN 1.PERFORMED T/S TO ISOLATE SMOKE AND FUMES IAW A220 W/C 0550- 2001. NO SMOKE AND FUMES DETECTED ALSO PERFORMED ISOLATE SMOKE AND FUMES APU W/C 0550-2002. NO Mar 11, 2025 · N122DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025030201590Door Sill · corrodedAIRCRAFT 8122, AFT CABIN FLOOR- LT AFT MCD LWR SILL CORRODED AT FR 74 & 76. CORRECTIVE ACTION: REMOVED AND REPLACED LT AFT MCD LWR SILL REF A220 ASRP 51-40-00 AND A220 DWG C01342700. (LP 0836350)Mar 2, 2025 · N122DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025030201592Floor Support · corrodedAIRCRAFT 8122, AFT CABIN FLOOR- RT AFT MCD LWR SILL CORRODED AT FR 76. CORRECTIVE ACTION: COMPLIED WITH ER/A 623665-14 PRI REV 0, REV 1, AND FINAL ER/A 623665-14 REV ORIGINAL SECTION 1. (LP 0836262)Mar 1, 2025 · N122DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025022801566Seat Track · corrodedAIRCRAFT 8122, SEAT TRACK CORROSION AT LBL 43.50 AROUND FRAME 20. SSI 53-21-43-02. NO PREVIOUS REWORKING NOTED. CORRECTIVE ACTION: REPAIRED PER ER/A 623171-14TR REV ORIGINAL SECTION 1. (LP 0815756)Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025022801565Seat Track · corrodedAIRCRAFT 8122, AFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 RBL 45. CORRECTIVE ACTION: REPLACED DAMAGED SECTION OF SEAT TRACK PER ER/A 623170-14TR REV ORIGINAL. (LP 0815735)Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025022801564Seat Track · corrodedAIRCRAFT 8122, SEAT TRACK CORROSION AT RBL 43.50 AND FRAME 20. REF SSI 53-21-43-02, NO PREVIOUS REWORK NOTED. CORRECTIVE ACTION: REPLACED DAMAGED SECTION OF SEAT TRACK PER ER/A 623174-14TR REV ORIGINAL. (LP 0815760).Feb 17, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025021801192Seat Track · corrodedAFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 LBL 23. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/003 00424 REMOVED AND REPLACED SEAT TRACK PER A220 ASRP 51-77-00-00 -028A-A AND AIRBUS DRAWING C01342701. (LP# 0811435)Feb 14, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025021101076Skin · damagedLEFT SIDE OF FUSELAGE HAS A SMALL DENT/NICK BETWEEN STR23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0557:2090-2107/002 00406 REPAIRED GOUGE PER ER/A 623625-14 PRI REV 0,REV 1,REV 2, AND ER/A 623625- 14 REV ORIGIFeb 11, 2025 · N122DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025022701550Tail Cone · puncturedAIRCRAFT 8122, WHILE IN HCK VISIT @ MSP MAINTENANCE FOUND A PUNCTURE ON THE (PN C03113040-103) FORWARD UPPER TAIL CONE SKIN. THE PUNCTURE IS LOCATED APPROX. 1.00" AFT OF FR88 AND 3.20" INBD OF STGR1R. THE AREA AROUND THE PUNCTURE ALSO CONTAINS A SMALL DENT REPFeb 3, 2025 · N122DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2025012900704Attach Fitting · corrodedCORROSION FOUND ON DOOR THRESHOLD ATTACHMENT LOCATION AFT RH LAV . -P- SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0460:2000-1001/035 00330 REMOVED AND REPLACED DOOR THRESHOLD ATTACHMENT LOCATED AT AFT RH LAV. REF Jan 26, 2025 · N122DU · Airbus BD5001A10 · Fuselage Main, Attach FittingsSDR DALA2025012400596Seat Track · corrodedAFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 LBL 43. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/002 00423 REMOVED AND REPLACED SEAT TRACK, REF A220 ASRP 51-77-00. (LP# 0771501)Jan 21, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025012300566Seat Track · corrodedAFT CABIN FLOOR- SEAT TRACK CORRODED AT FR 74 RBL 23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2015/004 00425 REMOVED AND REPLACED TRACK PER A220, ASRP 51-77-00. (LP# 0771037)Jan 20, 2025 · N122DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024102110273Link · brokenLH SLAT #2 TRACK #4 ATTACHMENT LINK FOUND BROKEN. P/N CO1612553- 001. REMOVED AND REPLACED LH SLAT #2 TRACK #4 ATTACHMENT LINK ON NR008 JOB COMPLETE. (LP# 0610961)Oct 15, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607509Slat Track · corrodedLH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0610 UTC. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE PEJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607508Slat Track · corrodedLH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0608 UTC. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE PJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607507Slat Track · corrodedLH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0606 UTC 02. REPAIRED LH SLAT TRACK NBR 5 LOWER AFT SURFACEJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607506Slat Track · corrodedLH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0604 UTC 02. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACEJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607505Slat Track · corrodedLH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0601 UTC 02. REPAIRED LH SLAT TRACK NBR 6 UPPER FWD SURFACJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607504Slat Track · corrodedLH SLAT TRACK NBR 1 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0558 UTC 02. REPAIRED LH SLAT TRACK NBR 1 LOWER FWD SURFACEJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607503Slat Track · corrodedLH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0556 UTC 02. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607502Slat Track · corrodedLH SLAT TRACK NBR 2 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0551 UTC 02. REPAIRED LH SLAT TRACK NBR 2 LOWER FWD SURFACEJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607501Slat Track · corrodedLH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0545 UTC 02. REPAIRED LH SLAT TRACK NBR 3 UPPER FWD SURFACJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607500Slat Track · wornLH SLAT TRACK NBR 5 UPPER AFT O/B SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0534 UTC 02. MEASURED LH SLAT TRACK NBR 5 UPPER AFT O/B SURFJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607499Slat Track · wornLH SLAT TRACK NBR 5 LOWER FWD O/B SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0521 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE Jul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607498Slat Track · wornLH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0514 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE PERJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607497Slat Track · wornLH SLAT TRACK NBR 6 LOWER FWD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0507 UTC 02. MEASURED LH SLAT TRACK NBR 5 LOWER FWD SURFACE PERJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607496Slat Track · corrodedLH 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. LOG-PAGE UPDATED @ 24JUL24 0447 UTC 02. REPAIRED LH SLAT TRACK NBR 7 UPPER AFT SURFACJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024072607495Slat Track · corrodedLH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 24JUL24 0439 UTC 02. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD SURFACJul 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024050204866Relay · faultedSHIP 8122 - GEAR - AFTER SELECTING GEAR DOWN, RECEIVED "GEAR FAIL" CAUTION MESSAGE WITH 3 GREEN DOWN AND LOCKED INDICATIONS. CORRECTIVE ACTION: R/R LANDING GEAR RELAY K6. (LP# 5846460)May 1, 2024 · N122DU · Airbus BD5001A10 · Landing Gear Position and WarningSDR DALA2024042604719Slat Track · corrodedLH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024042604718Slat Track · corrodedLH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024042604717Slat Track · corrodedLH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024042604716Slat Track · corrodedLH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608595- 14AD REV D AND PRI 6085Apr 24, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024042604715Slat Track · corrodedRH SLAT TRACK NBR 6 UPPER AFT SURFACE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608598- 14AD REV C AND PRI 608598-1Apr 23, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001390Slat Track · corrodedL/H SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 8 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0, 1 MJan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001389Slat Track · corrodedL/H SLAT TRACK NBR 8 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 8 LOWER FWD I/B SIDE PER ERA 608595- 14AD REV C & PRI REVJan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001388Slat Track · corrodedL/H SLAT TRACK NBR 7 LOWER FWD INBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 LOWER FWD I/B SIDE PER ERA 608595- 14AD REV C & PRI 0.1Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001387Slat Track · corrodedL/H SLAT TRACK NBR 10 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 10 LOWER FWD O/B SIDE PER ERA 608595- 14AD REV C & PRI 0Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001386Slat Track · corrodedLH SLAT TRACK NBR 10 UPPER AFT OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 10 UPPER AFT O/B SIDE PER ERA 608595- 17AD REV C & PRI REJan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001385Slat Track · corrodedL/H SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 10 UPPER FWD SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1 Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001384Slat Track · corrodedLH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OR CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1 MATJan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001382Slat Track · corrodedLH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 3 LOWER AFT SURFACE PER ERA 608595- 14AD REV C & PRI REV 0.1 MAJan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001379Slat Track · corrodedLH SLAT TRACK NBR 3 LOWER FWD OUTBOARD SIDE HAS EVIDENCE OR CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 3 LOWER FWD O/B SIDE PER ERA 608595- 14AD REV C & PRI 0.1 Jan 28, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024013001377Slat Track · corrodedLH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR MARKS IN TWO SEPARATE LOCATIONS AND PREVIOUS REWORK REF 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 4 LOWER AFT SURFACE PER ERA 608595-Jan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024012901269Slat Track · corrodedL/H SLAT TRACK NBR 5 UPPER AFT OUTBOARD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 5 UPPER AFT OUTBOARD SIDE PER ER/A 608595-14AD REV C ANDJan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024012901268Slat Track · corrodedLH SLAT TRACK NBR 6 LOWER FWD INBOARD SIDE HAS EVIDENCE OF A WEAR MARK AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 6 LOWER FWD INBOARD SIDE PER ER/A 608595-14AD REV C AND Jan 27, 2024 · N122DU · Airbus BD5001A10 · Leading Edge Devices
Back to N122DU