N123DQ

Service difficulty reports · 102

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 = 'N123DQ' 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 DALA2026092305317Wire · brokenFWD SERVCE DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER A220 AMP 33-5 NO HELP. FOUND BROKEN WIRE GOING TO ASSEMBLY. SPLICED WIRE PER A220 ESPP 20-15 TEST OK THIS CLEARS MEL PLACARD REMOVED. (LP# 9474011; AIRCRAFT WAS GROUNDED)Sep 17, 2026 · N123DQ · Airbus BD5001A10 · Light System WiringSDR DALA2026092305316Light · inoperativeFWD LEFT OVERWING EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT IAW A220 AMP 33-55-02. OPS TEST GOOD. (LP# 9474010; AIRCRAFT WAS GROUNDED)Sep 17, 2026 · N123DQ · Airbus BD5001A10 · Emergency LightingSDR DALA2026020900938Light · inoperativeFORWARD RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. OPS CHECKED GOOD. (LP# 7728279)Feb 6, 2026 · N123DQ · Airbus BD5001A10 · Emergency LightingSDR DALA2026020900937Light · inoperativeFORWARD RT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. OPS CHECKED GOOD. (LP# 7728278)Feb 6, 2026 · N123DQ · Airbus BD5001A10 · Emergency LightingSDR DALA2026020300806Door · icedFLIGHT ATTENDANTS ARE UNABLE TO DISARM DOOR 2L AFTER ARRIVAL AT DESTINATION. CLEARED OBSTRUCTION & ICE FROM DOOR 2L DRAINS, DOOR DISARMED & OPS CHECK NOW GOOD. OK FOR SVC. (LP# 7728258)Jan 30, 2026 · N123DQ · Airbus BD5001A10 · Passenger/Crew DoorsSDR DALA2025111208281Valve · faultedDECLARED EMERGENCY DUE TO "RT BLEED FAIL" MESSAGE WITH LEFT PACK ON MEL. REPLACED RT HIGH PRESSURE VALVE (HPV). (LP# 7670286)Nov 9, 2025 · N123DQ · Airbus BD5001A10 · Pneumatic Indicating SystemSDR DALA2025032602235Skin · corrodedCORROSION FOUND ON FWD AND AFT WASTE BOX PREVIOUS REPAIR DOUBLER AT WASTE SERVICE DOOR OPENING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 063-0001:10-0653-8- 7228/001 00153 CMOR: REPAIRED PER PRI 602195-14 REV 0, PRI 602195-14 REV 1, PRI 602195-14 REV 2, AND FMar 22, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025032602234Striker · corrodedCORROSION FOUND AROUND 3 HOLES ON AFT CORNER STRIKER, AFT RIGHT SERVICE DOOR. FOUND WORKING PRI FOR N/R 260 STEP 1 PART C. MARKED AREAS WITH BLACK MARKER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/002 00390 REPAIRED PER PRI 624617-14 RMar 22, 2025 · N123DQ · Airbus BD5001A10 · Service DoorsSDR DALA2025032602231Scuff Plate · corrodedFWD CARGO SILL, SCUFF PLATE ATTACH HOLE #1 CORRODED BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0499:5321-2015/002 00380 COMPLIED WITH ER/A 624684-14 REV ORIGINAL AND PRI REV 0. LINE 03 SHOULD STATE:Mar 22, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025032602233Skin · corrodedFUSELAGE SKIN AT AFT SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLES 2OL, 4OL , 5OL, 6OL, 8OL, 9OL,10OL, 11OL, 12OL, 13OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/001 00260 REPAIREDMar 21, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025032602232Scuff Plate · corrodedFUSELAGE SKIN AT FORWARD SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLE 7OL, 8OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 018-0001:5331-01297- 01B/001 00268 REPAIRED PER PRI 624621-14 REV 0, PRI 624621-14 RMar 21, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025031001816Seat Track · corrodedSEAT TRACK CORROSION LBL 43.5 AT FRAME 74-72. -M-. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2016/004 00349 REPAIRED PER ERA 623167-14TR SECTION I. ERA SHOULD READ ERA 623167-14TR REV ORIG SECTION I (68Mar 9, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025031001815Seat Track · corrodedSEAT TRACK CORROSION LBL 23 AT FRAME 74-72. -M-. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2016/003 00348 REPAIRED PER ERA 623168-14TR SECTION I. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE Mar 9, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025030901794Mount · corrodedAIRCRAFT 8123, GALLEY G4 FWD HALF MOUNT FITTINGS CORRODED. CORRECTIVE ACTION: REPLACED FITTINGS W/REF TO SAFRAN CMM 25-30-17. (LP 0847834)Mar 8, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Equipment Attach FittingsSDR DALA2025030601771Seat Track · corrodedAIRCRAFT 8123, SEAT TRACKS FWD FUSELAGE - RH SIDE, INBOARD SEAT TRACK, FORWARD END, SHOWS EVIDENCE OF CORROSION. CORRECTIVE ACTION: REPLACED SEAT TRACK REF A220 ASRP 51-42-00 AND A220 DWG C02312600. (LP 0842670)Mar 5, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025030601769Seat Track · corrodedAIRCRAFT 8123, SEAT TRACK CORROSION RBL 23 AT FRAME 74-72. CORRECTIVE ACTION: REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342701 REV G. (LP 0840860)Mar 4, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025030601768Seat Track · corrodedAIRCRAFT 8123, SEAT TRACKS FWD FUSELAGE - RH SIDE, OUTBOARD SEAT TRACK, FORWARD END, SHOWS EVIDENCE OF CORROSION. CORRECTIVE ACTION: CORROSION CONTAINED WITH SPLICE REPAIR. ACCOMPLISHED SPLICE REPAIR PER ER/A 623174-14TR REV ORIGINAL. (LP 0840824)Mar 4, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024122311956Duct · disconnectedON TAXI-IN SMOKE/ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT, ALSO GOT A L PACK DISCHARGE DUCT DISCONNECTED INFO MESSAGE. C/W SMOKE/FUMES T/C 0550-2001, NTF, SUSPECT DUCT FOUND IN LOG 6562870 ALLOWED FOR PACK/AVIONICS EXHAUST INGESTION AND RECIRCULATION THROUGHOUTDec 21, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution SystemSDR DALA2024122311955Cover · out of positionCHECK HARD COVER ON 2R DOOR EMER SLIDE. FOUND COVER BINDING ON DOOR SLIDE, SUSPECT BAD SLIDE. REMOVED 2R DOOR SLIDE AS PER A220 AMM 25-63. INSTALLED NEW SLIDE AS PER A220 WORK CARD 2563-4006, ALL CHECKS OK. REQUIRED INSPECTION COMPLIED WITH 202288 SLIDE, AFT SDec 20, 2024 · N123DQ · Airbus BD5001A10 · Escape SlideSDR DALA2024121011577Unknown · odorDIRTY SOCK SMELL ON DEPARTURE DURING CLIMB. SMELL DISSIPATED AT CRUISE. C/W WORK CARD 0550-2001 ISOLATE SMOKE AND FUMES IN COCKPIT/CABIN . NOTE : #1 ENG ON MEL 36-12-00A. PRSOV AND HPV LOCKED CLOSED. NO FINDINGS NOTED. #1 ENG SUSPECTED SOURCE. C/W A220 EFIM SODec 7, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution SystemSDR DALA2024121011575Bleed Air Sys · odorFUME /DIRTY SOCK SMELL ON T/O DISSIPATED QUICKLY RETURNED ON FINAL APPROACH. PERFORMED A220 NO GO ODI PREVENTION ATA 2172-SMOKE /FUMES IN THE CABIN PERFORMED STEP 1 :AMDS WORKCARD 0550-2001 STILL REQUIRES STEP 12 TO BE COMPLETED .FOUND SOURCE OF SMELL COMING FDec 6, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution SystemSDR DALA2024092009269Slat Track · no discrepancyRH SLAT TRACT NBR 5 UPPER FWD SURFACE (2 LOCATIONS) REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP BD500-A-J51-01-20- 01AAA-353A-A. NO DEFECTS NOTED. (LP# 0565092)Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Propeller SystemSDR DALA2024092009268Slat Track · no discrepancyLH SLAT TRACK NBR 3 LOWER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP BD500-A-J51-01-20- 01AAA-353A-A. NO DEFECTS NOTED. (LP# 0565088)Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Standard Practices/StructuresSDR DALA2024092009267Slat Track · no discrepancyLH SLAT TRACK NBR 2 LOWER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAQ AND TP BD500-A-J51-01-20- 01AAA-353A-A NO DEFECTS NOTED. (LP# 0565077)Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024081308074Module · faultedSHIP 8123 -ATO- DUE TO "RT BRAKE FAIL" MESSAGE. CORRECTIVE ACTION: REPLACED TIRE PRESSURE MODULE. (LP# 6073953)Aug 11, 2024 · N123DQ · Airbus BD5001A10 · TireSDR DALA2024053005634Unknown · odorFAINT DIRTY SOCK SMELL FROM 4,000 FT.-8000 FT. DISSIPATED AFTER 1-2 MIN. T/S PER AMDS WORKCARD NUMBER 0550-2001 (ISOLATE SMOKE AND FUMES IN COCKPIT AND/OR CABIN) STEPS 1-4 COMPLETED (ER 955691). C/W STEPS 5 TO 8 (EC 741818). DURING HIGH PWR ENG RUN OIL SMELL NMay 29, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution SystemSDR DALA2024040904237Valve · faultedSHIP 8123 - DIV - TO ATL DUE TO "R BLEED FAIL" MESSAGE. CORRECTIVE ACTION: DEFERRED RIGHT BLEED PER MEL 36-12-01B. LATER, REPLACED RIGHT PRSOV VALVE. (LP 0280826)Apr 6, 2024 · N123DQ · Airbus BD5001A10 · Compressor Bleed ValveSDR DALA2024021302021Light · inoperativeR4 EMERGENCY LIGHT INOP. REMOVED AND REPLACED R2 EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW A220 AMP 33-55-02. OPS CK GOOD. (LP# 5558752)Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Emergency LightingSDR DALA2024021302020Slat Track · corrodedR/H SLAT TRACK NBR 10 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1008 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTRFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302019Slat Track · corrodedR/H SLAT TRACK NBR 8 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1000 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201902Slat Track · corrodedR/H SLAT TRACK NBR 10 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1012 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTRFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201901Slat Track · corrodedR/H SLAT TRACK NBR 9 UPPER AFT O/B HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1005 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201900Slat Track · corrodedR/H SLAT TRACK NBR 7 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0955 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201899Slat Track · corrodedR/H SLAT TRACK NBR 7 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0951 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201898Slat Track · corrodedR/H SLAT TRACK NBR 6 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0948 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201897Slat Track · corrodedR/H SLAT TRACK NBR 6 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0941 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201896Slat Track · corrodedR/H SLAT TRACK NBR 5 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0937 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201895Slat Track · corrodedR/H SLAT TRACK NBR 5 LOWER I/B FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0930 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201894Slat Track · corrodedR/H SLAT TRACK NBR 5 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0923 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201893Slat Track · corrodedR/H SLAT TRACK NBR 4 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0919 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201892Slat Track · corrodedR/H SLAT TRACK NBR 4 UPPER I/B AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0914 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201891Slat Track · corrodedR/H SLAT TRACK NBR 4 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0910 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201890Slat Track · corrodedR/H SLAT TRACK NBR 3 UPPER FWD HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0909 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201889Slat Track · corrodedR/H SLAT TRACK NBR 2 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0907 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201888Slat Track · corrodedR/H SLAT TRACK NBR 2 LOWER O/B FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0905 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201887Slat Track · corrodedR/H SLAT TRACK NBR 2 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0903 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201886Slat Track · corrodedR/H SLAT TRACK NBR 1 LOWER AFT HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0900 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201885Slat Track · corrodedR/H SLAT TRACK NBR 1 UPPER AFT HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0859 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201884Slat Track · corrodedR/H SLAT TRACK NBR 1 UPPER FWD HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0857 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021201883Slat Track · corrodedR/H SLAT TRACK NBR 7 PINION TEETH HAS EVIDENCE OF WEAR. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0853 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR 01895233 W REPAIRED R/H SLAT TRACK NBR 7 PINION TEFeb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
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