N306DU

Service difficulty reports · 98

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 = 'N306DU' 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 DALA2026081404650Seal · leakingIN FLIGHT LIGHT ODOR DETECTED AROUND ROWS 17,18,19,20. FOUND OIL IN NR 2 ENGINE SPINNER, REPLACED FAN SHAFT COVER SEAL PER A220 AMP 72-15. AMDS W/C'S 0550-2001 AND 0550-2003 COMPLIED WITH. (LP 9615706 - AIRCRAFT WAS GROUNDED)Aug 12, 2026 · N306DU · Airbus BD5001A11 · Turbine Engine Oil SystemSDR DALA2026080404485Engine · vibrationDIVERTED TO ATL DUE TO NBR 2 ENGINE VIBES. NR 2 ENG VIBS 1.25 FOR 38 SEC. MAINTENANCE IN PROGRESS.Aug 3, 2026 · N306DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)SDR DALA2026070904025Strut · fodATB - WOW FAIL ON TAKE OFF. REMOVED LT MLG SHOCK STRUT. FOUND CHEESE CLOTH WRAPPED AROUND BEARING AND SEALS. REMOVED ALL DEBRIS, RE-PACKED LEFT MLG SLIDING TUBE. REPLACED LEFT MLG INBOARD SHOCK STRUT HARNESS. (LP# 8948758, 8948756, 8948760; AIRCRAFT WAS GROUNJul 7, 2026 · N306DU · Airbus BD5001A11 · Landing Gear Position and WarningSDR DALA2026062903853Anti-Ice Valve · faultedDIV - TO SLC DUE TO "R WING A/ICE FAIL" MESSAGE. R & R RT WAI VALVE AND PRESSURE SENSOR HARNESS. (LP# 8948718; AIRCRAFT WAS GROUNDED)Jun 24, 2026 · N306DU · Airbus BD5001A11 · Airfoil Anti/De-ice SystemSDR DALA2026062303731Light · inoperativeMULTIPLE EMERGENCY EXIT EXTERIOR LIGHTS OUT. REPLACED EMERGENCY EXTERNAL LIGHTS (FWD RT, AFT LT AND AFT RT) IAW AMP BD500-A-J33-55-02-01AAA-520A-A, BD500-A-J33-55-02- 01AAA-720A-A, BD500-A-J33-55-02-03AAA-520A-A AND BD500-A-J33-55- 00-01AAA-320A-A. OPERATIONALJun 20, 2026 · N306DU · Airbus BD5001A11 · Emergency LightingSDR DALA2026062303730Light · inoperativeBOTH LT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE, NEED TO REPLACE. REPLACED BOTH LT OVERWING EXTERNAL EMERGENCY LIGHT IAW AMP BD500-A-J33-55-02-02AAA-720A-A. OP TEST PASSED. (LP# 1655680, AIRCRAFT WAS GROUNDED)Jun 19, 2026 · N306DU · Airbus BD5001A11 · Emergency LightingSDR DALA2026061703626Floor Support · corrodedCORROSION AT REAR BARREL FLOOR EDGE SUPPORT AT FR 76 RBL 49 WL 147 . REMOVED AND REPLACED SILL FLOOR WEB AT STA FR76 RBL 49 WL 147 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342700 REV:-T. (LP# 1648146; AIRCRAFT WAS GROUNDED)Jun 15, 2026 · N306DU · Airbus BD5001A11 · Fuselage Miscellaneous StructureSDR DALA2026061703625Floor Panel · corrodedFORWARD CABIN FLOOR PANEL 221 KLF (L1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 221 KLF AT L1 DOOR PER AMP BD500-A-J53 -00-47-12AAA-720A-A. (LP# 1645035; AIRCRAFT WAS GROUNDED)Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026061503586Floor Panel · corrodedCORROSION ON FORWARD CABIN FLOOR PANEL 222 KRF (R1 ACCESS DOOR) CORROSION FOUND ON AFT INBOARD SIDE. REPLACED FLOOR PANEL 222 KRF AT R1 DOOR IAW AMP BD500-A-J53 -00-47-12AAA-720A-A. (LP# 1643774; AIRCRAFT WAS GROUNDED)Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026061503585Floor Panel · corrodedAFT SERVICE DOOR FLOOR PANEL 242MRF CORRODED ON AFT INBD CORNER. REMOVED AND REPLACED FLOOR PANEL 242MRF AT AFT SERVICE DOOR IAW AMP BD500-A-J53-00-47-14AAA-720A-A. (LP# 1643694; AIRCRAFT WAS GROUNDED)Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Floor PanelSDR DALA2026061503584Floor Support · corrodedCORROSION AT REAR BARREL FLOOR EDGE SUPPORT BETWEEN FR 74 TO FR 76 LBL 49 WL147. REMOVED AND REPLACED FLOOR PANEL SUPPORT FROM FR74 TO FR76 LBL 49 WL 147 IAW A220 AMP BD500-A-J53-00-47-13AAA-720A-A. (LP# 1643683; AIRCRAFT WAS GROUNDED).Jun 12, 2026 · N306DU · Airbus BD5001A11 · Fuselage Miscellaneous StructureSDR DALA2026060903489Seat Track · corrodedCORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342722-009S1 LOT 5196527-3 AT REAR BARREL FROM FR 61 TO FR74 LBL 23 WL 147 PER DWG BOMBARDIER PL C01342701 REV- G. AND A220 ASRP BD500-A-J51-42 -20-00Jun 4, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026060903488Seat Track · corrodedCORROSION AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 23 WL 147. REMOVED AND INSTALLED NEW SEAT TRACK P/N C01342723-0095 LOT 5194663-1 OF REAR BARREL FROM FR61 TO FR74 PER DWG BOMBARDIER PL C01342701 REV-G AND A220 ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP# 16Jun 4, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026053003280Seat Track · corrodedCORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 LBL 43.5 WL147. REPLACED SEAT TRACK AT LBL=43.5, WL=147 BTW FR=60 TO FR=75 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A PAR. 3, 5 AND BOMBARDIER DWG= C01342701 REV= G. (LP 1620113 - AIRCRAFT WAS GROUMay 29, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026053003279Seat Track · corrodedCORROSION LEVEL 2 AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 43.5 FR 20 WL 147. REPLACED SEAT TRACK RBL 43.5 FR20 - FR30 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV - K. (LP 1620095 - AIRCRAFT WAS GROUNDED)May 29, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052703196Seat Track · corrodedCORROSION LEVEL 2 AT REAR BARREL FLOOR SEAT TRACK AT FR 74 RBL 43.5 WL147. REPLACED SEAT TRACK RBL 43.5 FR61 - FR74 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV G. (LP 1614438 - AIRCRAFT WAS GROUNDED)May 26, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026052703195Seat Track · corrodedCORROSION AT FORWARD FUSELAGE FLOOR SEAT TRACK RBL 23 FR 20 WL 147. REPLACED FWD CABIN RIGHT SIDE SEAT TRACK RBL23 BTW FR19 TO FR31 WL 147 IAW ASRP BD500-A-J51-42-20-00AAA-078A-A PAR. 3 AND 5 AND DWG BOMBARDIER C02312600 REV: K. (LP 1614290 - AIRCRAFT WAS GRMay 26, 2026 · N306DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026011400342Slide · warning messageON FINAL APPROACH, WING SLIDE CAUTION COME ON INTERMITTENTLY. DOORS PAGE SHOWED LEFT SLIDE YELLOW DOOR INDICATION IN AFT. INTERMITTENT INDICATION CONTINUED ON THE GROUND. REMOVED AND REPLACED L/H OVERWING SLIDE IN REF. WITH AMDS W/C # 2563-4002. OK FOR SVC. RIJan 12, 2026 · N306DU · Airbus BD5001A11 · Escape SlideSDR DALA2025111708376Skin · puncturedHOLE IN FUSELAGE, AFT OF DOOR 1L. ACCESSED TO DAMAGE IS FWD BB, SUBMITTED DIMENSIONS OF DAMAGE TO ENGINEERING. ALL REPAIR WORK COMPLETED IAW ER/A 630504-14 REV. A. RII'S COMPLIED WITH. FWD CARGO SIDEWALL PANEL INSTALLED IAW AMP 50-11. ASSOCIATED ER/A 14-63Nov 14, 2025 · N306DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2025070204957Engine · odorDIRTY SOCK SMELL IN AFT GALLEY DURING DESCENT. T/S PER AMDS W/C 0550-2001. FOUND OIL ODOR COMING FROM LT ENG DURING HIGH POWER OP (+80% N1). C/W AMDS W/C 0550-6001. C/W MEL 36-12-00A, REF LOG # 7382643. ERA 613840-14TR SEC. II (WATER WASH) REQ WITHIN 5 CALENDAJun 25, 2025 · N306DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)SDR DALA2025052003863Slat Track · corrodedLH SLAT TRACK #4 RACK TEETH 1 AND 2 HAS EVIDENCE OF CORROSION WITH EVIDENCE OF PREVIOUS REWORK. LIAISON ENGINEERING SUPPORT WILL BE REQ BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 620728-14AD REV B AND PRI 620728-14AD REV O MATCHES. (LP# 0969341)May 16, 2025 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025010800175Unknown · odorON DESCENT THROUGH 8000 FT WE SMELLED A STRONG ODOR SIMILAR TO OIL BURNING FOR APPROXIMATELY TWO MINUTES IN BOTH THE FLIGHT DECK AND CABIN. NO SMOKE WAS PRESENT. BOTH ENGINES AND ALL SYSTEMS WERE OPERATING NORMAL. APU WAS OFF. LEFT OIL QUANTITY 26.5, RIGHT 25.Jan 5, 2025 · N306DU · Airbus BD5001A11 · Air Distribution SystemSDR DALA2024093009542Valve · lockedSHIP 8306 - ATB - DUE TO TRIM AIR INDICATION WITH TRIM AIR VALVE LOCKED CLOSED. CORRECTIVE ACTION: REMOVED AND REPLACED TRIM AIR PRESSURE REGULATING VALVE. OPS CHECK OK. (LP 6049314)Sep 28, 2024 · N306DU · Airbus BD5001A11 · Cabin Temperature Control SystemSDR DALA2024021302039Slat Track · corrodedLH SLAT TRACK NBR 7 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2107 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: NFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302038Slat Track · corrodedLH SLAT TRACK NBR 11 LOWER FORWARD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2054 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302037Slat Track · corrodedLH SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2050 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742 Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302036Slat Track · corrodedLH SLAT TRACK NBR 5 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2047 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302035Slat Track · corrodedL/H SLAT TRACK NBR 1 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2044 UTC 02 CORR BY SPURLIN 02405497Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302034Slat Track · corrodedLH SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2040 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742 RFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302033Slat Track · corrodedLH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2036 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302032Slat 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 FLT LOG-PAGE UPDATED @ 07FEB24 2016 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302031Slat Track · corrodedLH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2003 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302030Slat Track · corrodedRH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1912 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: NFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302029Slat Track · corrodedRH SLAT TRACK NBR 9 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1852 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: NFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302028Slat Track · corrodedRH SLAT TRACK NBR 7 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1833 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302027Slat Track · corrodedRH SLAT TRACK NBR 7 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1816 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302026Slat Track · corrodedRH SLAT TRACK NBR 6 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1756 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302025Slat 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 FLT LOG-PAGE UPDATED @ 07FEB24 1713 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302024Slat Track · corrodedRH SLAT TRACK NBR 3 LOWER FORWARD O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1653 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302023Slat Track · corrodedRH SLAT TRACK NBR 2 LOWER FORWARD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1624 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021302022Slat Track · corrodedRH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 1558 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201919Slat Track · corrodedLH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2101 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 02453691 WFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201918Slat Track · corrodedLH SLAT TRACK NBR 6 LOWER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2052 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 0245369Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201917Slat Track · corrodedRH SLAT TRACK NBR 5 LOWER SURFACE HIDDEN AREA (FORWARD ROLLER) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-2B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2049 UTC 02 CORR BY SPURLIN 02405497 Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201916Slat Track · corrodedLH SLAT TRACK NBR 9 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2045 UTC 02 CORR BY IAH 07FEB24 ATA 5742 RII: N ENTR 018Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201915Slat 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 FLT LOG-PAGE UPDATED @ 07FEB24 2042 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201914Slat Track · corrodedLH 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 FLIGHT. LOG-PAGE UPDATED @ 07FEB24 2039 UTC 02 CORR BY LITTLEFIEL 01832863 IAH 07FEB24 ATA 5742 Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201913Slat 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 FLT LOG-PAGE UPDATED @ 07FEB24 2031 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201912Slat Track · corrodedLH SLAT TRACK NBR 1 UPPER FORWARD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT LOG-PAGE UPDATED @ 07FEB24 2009 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RIIFeb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024021201911Slat 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 FLT LOG-PAGE UPDATED @ 07FEB24 1925 UTC 02 CORR BY COLEMAN 02453691 IAH 07FEB24 ATA 5742 RII: N Feb 7, 2024 · N306DU · Airbus BD5001A11 · Leading Edge Devices
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