N309DU

Service difficulty reports · 61

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 = 'N309DU' 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 DALA2026090204956Floor Panel · corrodedCORROSION AT L2 ENTRY FLOOR PANEL INBD AFT CORNER. REMOVED AND REPLACED THE FLOOR PANEL IAW ASRP BD500- A-J51-41-02-00AAA-078A-A. (LP 1789926; AIRCRAFT WAS GROUNDED)Sep 1, 2026 · N309DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026090204952Floor Panel · corrodedCORROSION ON PAX CABIN FLOOR PANEL 242MRF, AFT INBD EDGE. REMOVED AND REPLACED FLOOR PANEL 242MRF IAW AMP BD500- A-J53-00-47-14AAA-720A-A. (LP 1787247; AIRCRAFT WAS GROUNDED)Aug 30, 2026 · N309DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026082704866Floor Support · corrodedFLOOR SUPPORT BRACKET AT FR 79 LBL 48. DAMAGE BY CORROSION ON FLOOR SUPPORT BRACKET, FOUND OUT OF LIMITS PER A220-ASRP-BD500-A-J51-11-04-01-AAA-311A-A, REMOVED DAMAGED FLOOR SUPPORT BRACKET(FITTING) FROM FR79, LBL 48 AND INSTALLED NEW REPLACEMENT FLOOR SUPPORTAug 24, 2026 · N309DU · Airbus BD5001A11 · Fuselage Miscellaneous StructureSDR DALA2026082104772Web · corrodedCORROSION LEVEL 2 ON FLOOR STRUCTURE AT APPROXIMATELY STATION 1365 AND RBL 65 JUST INSIDE THE AFT SERVICE DOOR. REMOVED DAMAGED FLOOR WEB SILL FROM PASSENGER COMPARTMENT RBL 65 AND BTW FR-76 TO FR-79 AND REPLACED PER A220 ASRP BD500-A-J51-42-06-00AAA-078A-A Aug 21, 2026 · N309DU · Airbus BD5001A11 · Fuselage Miscellaneous StructureSDR DALA2026082104771Seat Track · corrodedFORWARD RT OTBD SEAT TRACK CORRODED, AT THE FORWARD END, RBL 43.5, FR 20. REMOVED DAMAGED SEAT TRACK RBL 43.5 BETWEEN FR 19+12 & FR 30+9, REPLACED IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, & DWG PL C02312600 REV -K. (LP 1768005 - AIRCRAFT WAS GROUNDED)Aug 21, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026081904752Access Panel · corrodedFORWARD FUSELAGE FLOOR STRUCTURE, R1 FLOOR ACCESS PANEL 222KRF MULTIPLE CORROSION LEVEL 2 SPOTS. REPLACED R1 FLOOR ACCESS PANEL 222KRF AT FORWARD FUSELAGE FLOOR STRUCTURE IAW A220 AMP BD500-A-J53-00-47-12AAA-720A-A. (LP 1763290 - AIRCRAFT WAS GROUNDED)Aug 16, 2026 · N309DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026081504668Seat Track · corrodedUPPER AFT FUSELAGE CABIN, RT OTBD SEAT TRACK CORROSION LEVEL 2 NOTED AT THE AFT END, RBL 43.5, FR 74. SEAT TRACK FROM FR 61-FR 74, RBL 43.5 WAS REPLACED IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01342701 REV-G. (LP 1755837 - AIRCRAFT WAS GROUNDED)Aug 14, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026081404649Floor Support · corrodedCORROSION LEVEL 2 ON FLOOR SUPPORT BRACKET AT FR 79 RBL 24. REPLACED FLOOR SUPPORT BRACKET AT FR79 RBL 24 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01342700 REV-T. (LP 1751325- AIRCRAFT WAS GROUNDED)Aug 11, 2026 · N309DU · Airbus BD5001A11 · Fuselage Miscellaneous StructureSDR DALA2026081104627Seat Track · corrodedUPPER AFT FUSELAGE CABIN, LT OTBD SEAT TRACK CORRODED, NOTED AT THE AFT END, LBL 43.5, FR 74. REPLACED THE AFT FUSELAGE CABIN LT OTBD SEAT TRACK IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01342701, REV-G. (LP 1748894 - AIRCRAFT WAS GROUNDED)Aug 10, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026081004612Support · wornAFTER EVALUATING THE BARE METAL ON THE AFT FAIRING SUPPORT LOCATED AT FR61 BETWEEN RBL 10 TO LBL 10 FOUND CORROSION. NO DAMAGE IS ALLOWED IAW ASRP BD500-A-J53-82-08-00AAA-661A-A, FIG 2. REPLACED THE FAIRING SUPPORT IAW PL C01731500 REV-E AND ASRP BD500-A-J51Aug 9, 2026 · N309DU · Airbus BD5001A11 · Aerodynamic FairingsSDR DALA2026080804589Seat Track · corrodedUPPER AFT FUSELAGE CABIN, RT, INBD SEAT TRACK CORROSION NOTED AT THE AFT END, RBL 23, FR 74. REPLACED SEAT TRACK RBL 23 BTW FR 61 TO FR 74 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, ASRP BD500-A-J51-42-06-00AAA-078A-A AND DWG C01342701, REV G. (LP 1744624 - AIAug 8, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026080804588Seat Track · corrodedFORWARD FUSELAGE FLOOR STRUCTURE, RT INBD SEAT TRACK CORROSION NOTED AT THE FORWARD END, RBL 23, FR 20. REPLACED SEAT TRACK FROM FR 20 - FR 30 RBL23 IAW ASRP BD500-J51-42-20-00AAA-078A-A AND DWG C02312600, REV-J. (LP 1743765 - AIRCRAFT WAS GROUNDED)Aug 7, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026080804587Seat Track · corrodedUPPER AFT FUSELAGE CABIN, LT INBD SEAT TRACK CORROSION NOTED AT THE AFT END, LBL 23, FR 74. REPLACED SEAT TRACK LBL 23, FR 74 - FR 60 IAW ASRP BD500-A-J51-42-20-00AAA-078A AND DWG C01342701, REV-G. (LP 1743757 - AIRCRAFT WAS GROUNDED)Aug 7, 2026 · N309DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026080404484Skin · damagedSEE LOG PAGE 8612918 FOR ERA 634635-14 REV ORIG SECT I STEP 9 RESTORE FINISHES TO EXTERNAL SURFACES . C/W REP INSP. OF FWD BELLY FAIRING DAMAGE PER ASRP 51-12-00-04AAA-661A-A. SPEED TAPE IN GOOD CONDITION OK. (LP# 8612921; AIRCRAFT WAS GROUNDED)May 21, 2026 · N309DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2026020300803Splice Plate · brokenFOUND SPLICE PLATE BROKEN P/N CO2386047-101 REMOVED DAMAGED SPLICE PLATE. INSTALLED SPLICE PLATE P/N C02386047-101 IAW A220 AMM 53-82. (LP# 1424461)Jan 28, 2026 · N309DU · Airbus BD5001A11 · Fuselage Main, StructureSDR DALA2026020300802Frame · crackedDURING AIRFRAME VIBRATION INVESTIGATION FOUND WTBF FRAME ASSEMBLY INBD END THAT ATTACHED TO LONGERON DEVELOPED A 1.25" L-CRACK REF A220 IPD 53-82-84-10AAB-941A-D. ITEM -75 P/M C02382115-001. REMOVED FRAME 48 OF WTBF SUPPORT STRUCTURE IAW AMP 220 53-82. INSTALLJan 28, 2026 · N309DU · Airbus BD5001A11 · Aerodynamic FairingsSDR DALA2025020400851Slat Track · corrodedLH SLAT TRACK NBR 4 PINION TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT LOG-PAGE UPDATED @ 01FEB25 1703 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 0Feb 1, 2025 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025020400850Slat Track · corrodedLH SLAT TRACK NBR 7 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1701 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: NFeb 1, 2025 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025020400849Slat Track · corrodedLH SLAT TRACK NBR 7 PINION (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE NEXT FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1659 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: N ENTR 0Feb 1, 2025 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025020400848Slat Track · corrodedLH SLAT TRACK NBR 4 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 01FEB25 1655 UTC 02 CORR BY FREE 01643853 IAH 01FEB25 ATA 5742 RII: NFeb 1, 2025 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025012400602Erosion Shield · peelingLH WINGLET LEADING EDGE EROSION TAPE PEELED UP AT LOWER EDGE. LH WINGLET LEADING EDGE WHERE EROSION TAPE IS DAMAGED AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 57-32-00-00AAA-662A-A. FWD TO MONIOct 18, 2024 · N309DU · Airbus BD5001A11 · Wing Main, Frame StructureSDR DALA2026090104929Erosion Shield · missingRIGHT HORIZONTAL TIP FAIRING EROSION PROTECTIVE MATERIAL NOT INSTALLED. APPLIED TIP FAIRING TEMP REPAIR IAW A220 AMP 55-12-86-01AAA- 662A-A. PERMANENT REPAIR REQUIRED AT 8500 FH. GVI TO BE PERFORMED EVERY 150 FH. FWD TO MON. (LP# 6171230; AIRCRAFT WAS GROUNJul 13, 2024 · N309DU · Airbus BD5001A11 · Horizontal Stabilizer StructureSDR DALA2026090104928Erosion Shield · missingLT HORIZONTAL TIP FAIRING EROSION PROTECTIVE MATERIAL NOT INSTALLED. APPLIED TIP FAIRING TEMP REPAIR IAW AMP 55-12-86-01AAA- 662A-A. REPAIR PERMITTED AT 8500 FH. GVI PERFORMED EVERY 150 FH. FWD TO MON. APPLIED ABRASION RESISTANT TAPE LT HORIZONTAL TIP FAIRINGJul 13, 2024 · N309DU · Airbus BD5001A11 · Horizontal Stabilizer StructureSDR DALA2024071507125Slat Track · wornRH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 1 UPPER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 608286-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507124Slat 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. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507123Slat Track · wornRH SLAT TRACK NBR 3 LOWER AFT SURFACE (2 LOCATIONS) HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 3 LOWER AFT SURFACE (2 LOCATIONS) IAW ER/A 608286-1Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507122Slat Track · corrodedRH SLAT TRACK NBR 5 LOWER AFT SURFACE 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 5 LOWER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507121Slat Track · wornRH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED RH SLAT TRACK NBR 1 LOWER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082286-1Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507120Slat Track · corrodedRH SLAT TRACK NBR 4 UPPER AFT SURFACE 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 UPPER AFT SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507119Slat Track · corrodedRH SLAT TRACK NBR 4 UPPER FWD SURFACE 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 UPPER FWD SURFACE IAW ER/A 608286- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507118Slat Track · wornLH SLAT TRACK NBR 8 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507117Slat Track · wornLH SLAT TRACK NBR 8 UPPER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 UPPER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507116Slat Track · wornLH SLAT TRACK NBR 8 LOWER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER FWD I/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507115Slat Track · wornLH SLAT TRACK NBR 8 UPPER FWD I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 UPPER FWD I/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507114Slat Track · wornLH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507113Slat Track · wornLH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 8 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507112Slat Track · wornLH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 7 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507111Slat Track · wornLH SLAT TRACK NBR 4 LOWER FWD O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 LOWER FWD O/B SIDE IAW ER/A 608285- 14AD REV C AND PRI 608285-Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507110Slat Track · wornLH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT.MEASURED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14AJul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507109Slat Track · wornLH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507108Slat Track · corrodedLH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507107Slat Track · corrodedLH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 1 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 608285-14Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507106Slat Track · corrodedLH SLAT TRACK NBR 6 UPPER 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 6 UPPER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507105Slat 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 608285- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024071507104Slat Track · corrodedLH SLAT TRACK NBR 2 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 2 LOWER AFT SURFACE IAW ER/A 608285- 14AD REV C AND PRI 6082Jul 13, 2024 · N309DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024060305749Skin · dentedDAMAGE FOUND- EXTERNAL DENT LEFT FWD FUSELAGE. 4 INCH X 3 INCH ABOVE STRG 29L AND AFT OF FR30A. TWO PANELS FWD CARGO OPENED FOR MTC(975849) REMOVED PAINT FROM EXTERNAL DENT FOR INSPECTION PER ENGINEERING REQUEST(249846) C/W HFEC OF DAMAGED AREA PER A220 ANDTP May 31, 2024 · N309DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2024042404686Lever · damagedCREW REPORTS 1L DOOR WILL NOT ARM AFTER CLOSURE. REMOVED SLIDE BUSTLE + PANEL SLIDE + SAFE TIED DOOR ASSIST BOTTLE . REMOVED SLIDE FROM DOOR + INNER DOOR LINER. REF. A220 AMP 52- 11, NO VISIBLE DAMAGE. GIRT BAR MAY BE BENT, DOOR WILL NOT CLOSE PROPERLY + "ARM Apr 20, 2024 · N309DU · Airbus BD5001A11 · Passenger/Crew DoorsSDR DALA2024020601597Seat Track · corrodedSEAT TRACK RBL 23 CORRODED AFT OF LAV D4 (204). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/120 00237 PERFORMED SEAT TRACK SPLICE REPLACEMENT PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND E R/A 615104-14 REV ORIGINAL. CLOSING REQUIREMENTS RII:Feb 1, 2024 · N309DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024020601596Seat Track · corrodedSEAT TRACK LBL 43.5 CORRODED AFT OF LAV C2 (203). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/118 00235 PERFORMED SPLICE REPAIR PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND ER/A 615104-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATIOFeb 1, 2024 · N309DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024020601595Seat Track · corrodedSEAT TRACK LBL 23 CORRODED AFT OF LAV C2 (203) SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/117 00234 PERFORMED SPLICE REPAIR PER PRI 615104-14 REV 0, REV 1, AND REV 2 AND ER/A 615104-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 0Feb 1, 2024 · N309DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach Fittings
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