N121DU

Service difficulty reports · 68

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 = 'N121DU' 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 DALA2026073104439Horn · false activationERRONEOUS EVAC HORN WHILE ON DESCENT (~15,000 FT). ONLY INDICATION ON FLIGHT DEC WAS EVAC CMD GUARDED SWITCH LIGHT ILLUMINATED. HORN CONTINUED ALL THE WAY UNTIL SHORTLY PRIOR TO LANDING. CORRECTIVE ACTION: PERFORMED EVAC HORN OPS TEST REF A220 AMP 44-11, TEST Jul 28, 2026 · N121DU · Airbus BD5001A10 · Interphone/Passenger Announcement (PA) SystemSDR DALA2026071604194Charger · failedBATTERY CHARGER FAULT AND CB TRIP MESSAGES WHILE SITTING AT GATE, BURNING SMELL IN COCKPIT AND FORWARD CABIN. OPENED MID E& E -FOUND STRONG BURNT ELECTRICAL SMELL. REPLACED #2 BATTERY CHARGER PER A220 AMP 24-32-02. TEST PASSES. MSI WORK CARDS 0550-2001 AND 055Jul 13, 2026 · N121DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026030401497Seat · stuckLOOSE PART UNDER CAPTAIN SEAT GOT CAUGHT AT CRUISE AND SEAT STUCK IN FULL AFT POSITION, NOT SAFE FOR FLIGHT UNTIL FIXED. FOUND CABLE PULLEY AND BOLT DISCONNECTED & HARDWARE LOOSE, ALL PARTS INTACT . RESECURED MISSING HARDWARE IAW A220 AMP 25-11 , OPS CHECK GOOMar 1, 2026 · N121DU · Airbus BD5001A10 · Flight Compartment EquipmentSDR DALA2025080705926Light · inoperativeDURING SVC CHK, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING LIGHT REF A220 AMP 33-55-02, LIGHT ILLUMINATES. A/C OK FOR SVC.Aug 3, 2025 · N121DU · Airbus BD5001A10 · Emergency LightingSDR DALA2025070304972Service Panel · corrodedCORROSION ON TOILET SERVICE PANEL SKIN CUTOUT. ACCOMPLISHED AND COMPLIED WITH ER/A 601047-14AD REV-A SECTION I ASSOCIATED ER/A 14-601047 ADDED FOR AC 8121. (LP# 1055921)Jun 30, 2025 · N121DU · Airbus BD5001A10 · Fluid Service DoorsSDR DALA2025070304971Pan · corrodedCORROSION ON LAVATORY PAN DOUBLER BETWEEN FR-75 AND FR-76, STR-34L AND STR-35L. ACCOMPLISHED AND COMPLIED WITH ER/A 601047-14AD REV-A SECTION I ASSOCIATED ER/A 14-601047 ADDED FOR AC 8121. (LP# 1055901)Jun 30, 2025 · N121DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025070304970Service Panel · corrodedCORROSION ON TOILET SERVICE PANEL. ACCOMPLISHED AND COMPLIED WITH ER/A 601047-14AD REV-A SECTION 1 ASSOCIATED ER/A 14-601047 ADDED FOR AC 8121. (LP# 1055873)Jun 30, 2025 · N121DU · Airbus BD5001A10 · Fluid Service DoorsSDR DALA2025070304968Seat Track · corrodedCORROSION ALONG PAX CABIN SEAT TRACKS AT WL-252.0, RBL- 23.5, FROM FR-30+7 TO FR-38+3. WL NEEDS TO BE WL-151. REMOVED DAMAGED SEAT TRACK AND REPLACED NEW SEAT TRACK FROM FR 30 + 7 TO FR 38, RBL 23.5 P/N C01335693-005S LOT. 5179492 IAW A220 ASRP BD500-J51-42-21Jun 22, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062504763Seat Track · corrodedCORROSION ALONG PAX CABIN SEAT TRACKS AT WL 151 RBL-23.5 FROM FR-43 TO FR-50+17. REMOVED AND REPLACED PAX CABIN SEAT TRACK AT WL 151 RBL-23.5, FROM FR-43 TO FR-50+17 PER A220 ASRP BD500-A-J51-42-21-00AAA- 078A-A AND PL C01335700 REV-H. (LP# 1039770)Jun 22, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404724Seat Track · corrodedCORROSION ON SEAT TRACK AT FR 74 RBL 43. REMOVED AND REPLACED SEAT TRACK AT FR 61 TO FR 74 RBL 43 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG # BOMBARDIER PL C01342701 REV: G. (LP# 1036303)Jun 20, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404723Seat Track · corrodedCORROSION ON SEAT TRACK AT FR 74 LBL 23. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 57+6" TO FR 74+6", LBL 23, WL 157 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER PL: C01342701. REV: G. (LP# 1036295)Jun 20, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404716Seat Track · corrodedCORROSION ALONG PAX CABIN SEAT TRACKS AT WL-151, RBL-43, FROM FR-20 TO FR-30+7. REMOVED AND REPLACED CABIN SEAT TRACKS AT WL 151 FR-20 TO FR-30+ 7 RBL-43 IAW A220 ASRP BD500-A-J51-40-11-01AAA-652A-A AND BOMBARDIER DWG # C02312600 REV E. (LP# 1034444)Jun 19, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404714Skin · bentFWD CARGO BAY DOOR LOWER AFT EXTERNAL SKIN BENT. REPAIRED FWD CARGO BAY DOOR LOWER AFT BENT SKIN IAW ASRP BP500. (LP# 1033421)Jun 19, 2025 · N121DU · Airbus BD5001A10 · Cargo/Baggage DoorsSDR DALA2025062404715Seat Track · corrodedCORROSION ON SEAT TRACK AT FR 74 LBL 43. REMOVED AND REPLACE SEAT TRACK FR61 TO FR74 LBL 43 P/N C01342721 -005S, LOT 5178942 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV. G. (LP# 1034395)Jun 18, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404713Seat Track · corrodedCORROSION ON SEAT TRACK AT FR 20 RBL 23.5 WL151 (FWD WET AREA-MARKED). SSI 53-21-43-02. REMOVED AND REPLACED SEAT TRACK AT FR20 TO FR30 RBL 23.5 WL 151 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV: -E. (LP# 1033374)Jun 18, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025062404709Seat Track · corrodedCORROSION ON SEAT TRACK AT FR 74 RBL 23. REMOVED AND REPLACED SEAT TRACK FROM FR 61 TO FR 74 P/N C01342723-009S LOT 5179060 PER A220 ASRP BD500-A-J51-42-20-00AAA -078A-A AND DWG BOMBARDIER C1342701 REV G. (LP# 1030619)Jun 18, 2025 · N121DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025070104894Frame · corrodedCORROSION ON AFT FUSELAGE LOWER FRAME FR 81 BL0 TO LBL 7 WL 130 (MARKED). SSI: 53-71-09-01. REMOVED AND REPLACED AFT FUSELAGE LOWER FRAME FR 81 TO STRINGER 17R - 18L PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV: -R. (LP# 104780Jun 13, 2025 · N121DU · Airbus BD5001A10 · Fuselage Main, FrameSDR DALA2025070104893Bracket · corrodedCORROSION ON AFT FUSELAGE LOWER FRAME BRACKET BETWEEN FRAME FR81 AND WIRING HARNESS COVER BL 0 FR 81 WL 134 (MARKED). REMOVED AND REPLACED AFT FUSELAGE LOWER BRACKET BETWEEN FRAME FR 81 BL 0 WL 134 PER A220 ASRP BD500-A-J51-42-06-00AAA-078A-A AND BOMBARDIER DWJun 13, 2025 · N121DU · Airbus BD5001A10 · Fuselage Main, Attach FittingsSDR DALA2025051403747Engine · odorDIRTY SOCK SMELL DETECTED AFTER RIGHT ENGINE STARTED USING START CART (APU WAS INOP). MORE DETAILS INCLUDED ON SMOKE & FUME QUESTIONNAIRE. ISOLATED DIRTY SOCK SMELL PER JK 0550-2001. 0164/ DIRTY SOCK SMELL WAS ONLY DETECTED WHILE HIGH POWER RUN. THE LEFT ENGINMay 10, 2025 · N121DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2025041703031Bleed Air Sys · odorON DECENT FA'S IN AFT GALLEY SMELLED A BRIEF DIRTY SOCK/MUSTY SMELL. ABOUT 10 MIN LATER SYMPTOMS OF NAUSEA, HEADACHE AND BURNING OF NOSTRILS AND CHEST OCCURED. SYMPTOMS STAYED THROUGH THE REMAINDER OF THE FLIGHT. #2 PACK WAS ON MEL SO ONLY BLEED #1 WAS PRODUCIApr 14, 2025 · N121DU · Airbus BD5001A10 · Engine Bleed Air SystemSDR DALA2025032602238Unknown · odorSTRONG OZONE ODOR FROM APU BLEED AFTER START UP UPON LANDING. PERFORMED T/S IAW W/C. # 0550-2001 NO FINDINGS THEN C/W 0550- 2003 NO FINDINGS ALSO DUE TO RECENT DUEL ENG W/W SUSPECTED AS CAUSE REF LOG # 0873410 FOR NO GO ODI PREVENTION A/C OK FOR SVCMar 24, 2025 · N121DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025031902080Unknown · odorON TAXI INTO MSY AFTER APU START WE HAD A STRONG METALLIC FUME SMELL. TURNED OFF APU BLEED AND SMELL WENT AWAY. APU WAS STARTED IN A 30 KNOT TAIL WIND. INSP APU + MOTORS FOR NO EVIDENCE OF CONTAMINATION, COMPLETED WORKCARD 0500-2001, AC OK FOR SERVICE. ALL ODIMar 18, 2025 · N121DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025031902079Oven · odorTURNING INTO GATE FORWARD F/A REPORTED SAME ODOR AS PREVIOUS FLIGHT IN MSY IN CABIN. NO ODOR OBSERVED IN COCKPIT OR REAR OF AIRCRAFT. LASTED FOR JUST VERY SHORT PERIOD AND WAS COINCIDENT WITH APU START. C/W NO GO ODI PREVENTION A220 21-72. FOUND FWD GALLEY TO Mar 17, 2025 · N121DU · Airbus BD5001A10 · Buffet/GalleysSDR DALA2025012300565Longeron · crackedWTBF RHS LONGERON ASSEMBLY. PN: C02383111-002 HAS CRACK. REMOVED RHS LONGERON ASSEMBLY P/N: C02383111-002 IAW W/C 5352-01038- 07B H. MOORE 1943566. MOCK INSTALLED LONGERON P/N: C02383111-002 IAW W/C 5352-01038-07B. RIVETS AND SEALANT STILL REQUIRED. APPLIED FAJan 20, 2025 · N121DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2024091609043Wire Harness · damagedAFTER LANDING ON TAXI IN 36 R BLEED FAIL - R PRESS REG SOV INOP. ALSO SMELLED "BURNT SOCK ODOR". RT BLEED FAIL ADDRESSED REF LP 6099928. PERFORMED WC 0550-2001, NO ODOR DETECTED. CW ODI . R/R #2 ENG PRSOV PER A220 AMP 36-11. R/R RH ECS HARNESS.Sep 10, 2024 · N121DU · Airbus BD5001A10 · Air Conditioning System WiringSDR DALA2024082008304Slat Track · corrodedRH SLAT TRACK NBR 4 TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 RACK TEETH (2EA) IAW ER/A 620173- 14AD REV ORIGINAL AND PRI 62017Aug 17, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024082008303Slat Track · corrodedRH SLAT TRACK NBR 4 PINION TEETH (2 EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 PINION TEETH (2EA) IAW ER/A 620173- 14AD REV ORIGINAL ANDAug 17, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024041104287Oil System · leakingSHIP 8121 - IFSD/ATB - RETURNED TO IAH. NUMBER 1 ENGINE WAS SHUT DOWN BY THE CREW DUE TO A LOW OIL PRESSURE WARNING. CORRECTIVE ACTION: FOUND OIL LEAK AT FUEL/OIL COOLER. REPLACED NBR 1 ENGINE.Apr 10, 2024 · N121DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2024031303284Pump · failedSHIP 8121 -IFSD- DECLARED EMERGENCY TO SEA DUE TO R ENG LOW OIL PRESSURE AND THE R ENG COMMANDED SHUTDOWN. CORRECTIVE ACTION: REPLACED #2 ENG OIL TANK PRESSURE RELIEF VALVE, RT ENG LUBE AND SCAVENGE OIL PUMP. (LP# 5274309)Mar 12, 2024 · N121DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2024021402153Slat Track · corrodedRH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0126 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402152Slat Track · corrodedRH SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0125 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402151Slat Track · corrodedRH SLAT TRACK NBR 9 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0124 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402150Slat Track · corrodedRH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0122 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402149Slat Track · corrodedRH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0121 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402148Slat Track · corrodedRH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0119 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402147Slat Track · corrodedRH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0118 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402146Slat Track · corrodedRH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 11FEB24 0117 UTC 02 CORR BY EASTMAN 01895233 IAH 11FEB24 ATA 5742 RIIFeb 11, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021402145Slat Track · corrodedLH SLAT TRACK NBR 11 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 10FEB24 2304 UTC 02 CORR BY EASTMAN 01895233 IAH 10FEB24 ATA 5742 RIFeb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302103Slat Track · corrodedLH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER FWD SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196233)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302102Slat Track · corrodedLH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD I/B SIDE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196232)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302101Slat Track · corrodedLH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196230)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302100Slat Track · corrodedLH SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 UPPER FWD SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196226)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302099Slat Track · corrodedLH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0916225)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302098Slat Track · corrodedLH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 LOWER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0916223)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302097Slat Track · corrodedLH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196220)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302096Slat System · corrodedLH SLAT TRACK NBR 8 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-*01028-02A. REPAIRED LH SLAT TRACK NBR 8 LOWER FWD IB SIDE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196219)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302095Slat System · corrodedLH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196217)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302094Slat System · corrodedLH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196215)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302093Slat System · corrodedLH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196212)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302092Slat Track · corrodedLH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196209)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge Devices
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