N109DU

Service difficulty reports · 64

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 = 'N109DU' 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 DALA2022031701763None · noneWASTE BOX: 1/4" X 1/4" AREA OF CORROSION ON THE FWD LIP/SEAL AREA OF THE WASTE BOX CUTOUT FR75. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 027-0001:5327-01014-01 /004 00142 COMPLIED WITH ER/A 597572-14 PRI REV 0, REV 1, REV 2 AND FINAL ER/A 597572-14 REV ORIGINMar 6, 2022 · N109DU · Bombdr BD1001A10 · Fuselage Internal Mounting StructureSDR DALA2022031701762None · noneWASTE BOX: CORROSION ON THE INBD HINGE BRACKET OTBD SURFACE. ATA 5327 RII: N ENTR 00371519 W SUMMARY SEE NR FOR ADDITIONAL INFORMATION 027-0001:5327-01014-01 /005 00143 COMPLIED WITH ER/A 597572-14 PRI REV 0, REV 1, REV 2 AND FINAL ER/A 597572-14 REV ORIGINAL.Mar 6, 2022 · N109DU · Bombdr BD1001A10 · Fuselage Internal Mounting StructureSDR DALA2022030801500None · noneLEFT HORIZONTAL STABILIZER NUMBER 2 RIB HINGE CRACKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0099:2040-0025/001 00103 ACCOMPLISHED PRI 597575-14, REV. 0 AND ERA 597575-14,REV. ORIGINAL. (LP# 2142706)Mar 3, 2022 · N109DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022030101306None · noneRIGHT MLG SHOCK STRUT LOWER SPINDLE HAS PITTING AND MISSING CADMIUM PLATING AT GEAR LEG ATTACH POINT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:3211-01191- 01B/004 00186 REMOVED AND REPLACED RMLG LWR SPINDLE ASSY PER A220 AMP 32-11-17. OPS TEST PERFORFeb 27, 2022 · N109DU · Bombdr BD1001A10 · Main Landing Gear Strut/Axle/TruckSDR DALA2021120707541Unknown · odorDIRTY SOCKS/FUME EVENT. COMPLETED VISUAL INSPECTION OF #1 + #2 ENGINE. REMOVE AP-HTC-1 AND AP-TIC1 FROM BOTH ENGINES. BOROSCOPED BOTH ENGINES AT HPC-L AND TIC SECTION. PERFORMED NO GO ODI PROCEDURE FOR SMOKE/FUME EVENT.Dec 6, 2021 · N109DU · Bombdr BD1001A10 · Air Distribution SystemSDR DALA2021102106561None · noneSHIP 8109 - DIV - TO DEN DUE TO FUEL IMBALANCE. CORRECTIVE ACTION: PLACED CTR TANK XFR SYSTEM ON MEL REQUIRING CTR TANK EMPTY; R/R TRANSFER FLOAT VALVE SOV. (LP# 7910366)Oct 17, 2021 · N109DU · Bombdr BD1001A10 · Fuel StorageSDR DALA2020122904326Unknown · odorINBOUND CREW SAID FUME SMELL OF GLYCOL OR FUEL WAS OBSERVED IN THE CABIN DURING FLIGHT. CORRECTIVE ACTION: PFMD STEPS 1-7 OF AMDS W/C 0550-2001. NO DISCREPANCIES FOUND W/APU ENGINE 1+2 PNEU SOURCES FOR PACKS. STEP 8 REQUIRES A220 EFIM SMELL OF FUMES W/APU ADec 28, 2020 · N109DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2020080602720Cover · missingLOW PRESSURE INNER COVER REPORTED MISSING. INSTALLED LPGC COVER AS REQ'D. OK FOR SVC.Aug 5, 2020 · N109DU · Bombdr BD1001A10 · Air Conditioning SystemSDR DALA2020070402541Skin · dentedERA 581352-14 REVISED TO REV 'A'. SECTION I ISSUED FOR DENT DMG TO FWD FUSELAGE LOWER SKIN, FR17 S-23L TO S-24L. DAMAGE TOLERANCE STAGE II RECEIVED.Jul 2, 2020 · N109DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2019120407040Longeron · crackedWHILE WORKING WRITE UP RT WING TO BODY LONGERON CRACK FOUND. REMOVED LONGERON 846371 COMPLETED WITH STEP ONE OF RI 583549-14 WIP329603 COMPLETED HFEC PER A220 ANDTP BD5000-A-J51-10-05-00AAA -353A-A ALL CRACKS MARKED QC2047 786880 COMPLETED STEP 4 AND 5 OF RI58Dec 3, 2019 · N109DU · Bombdr BD1001A10 · Aerodynamic FairingsSDR DALA2019110406395Brake · malfunctionedDESCENDING THRU FL240 STAB TRIM FAIL EICAS MESSAGE. FAULT CODES 2741F0013, 2741F0013, 2741F0036 AND 274F0037 IN FAULT MSG SUMMARY. SUSPECT AFT 1 REU OR HSTA MOTOR BRAKE. T/S PER EFIM REU CHECKS GOOD. FOUND HSTA BRAKE TO FAIL STATIC TORQUE - FUNCTIONAL TEST. RENov 4, 2019 · N109DU · Bombdr BD1001A10 · Stabilizer ActuatorSDR DALA2019091705377Skin · damagedLOWER FUSELAGE, LT SIDE SKIN CREASED ALONGAFT SIDE OF FR 17 BETWEEN STR 23L -24L. ALSO DENTED AREA FWD & AFT OF FR 17 BETWEEN STR 23L & 24L . COMPLIED WITH ERA 581352-14 REV 0. A /C O/K FOR SERVICE. (LP# 1274315, 6234745)Sep 16, 2019 · N109DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2019091705376Skin · damagedLOWER FUSELAGE, LT SIDE, SKIN CREASED ALONG AFT SIDE OF FR 17 BETWEEN STR 23L - 24L. ALSO DENTED AREAS ARE FWD & AFT OF FR 17 BETWEEN STR 23L -24L. ACCOMPLISHED PRI 581352-14AD REV 2 AWAITING FINAL EA 430466 REV ORIG ACCOMPLISHED RII 708436 {QC1976}. COMPLIED Sep 16, 2019 · N109DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2019081324742Warning Message · false activationAT APPROX 70 KTS DURING TAKE OFF ROLL HAD SPOILER CONFIG WARN. ABORTED TAKE OFF. WARNING WENT AWAY IMMEDIATELY AFTER INITIATING ABORT. 110, 000 LBS TAKE OFF WEIGHT. UPON RETURN TO GATE NO CONFIG SPOILER CAS MSG PRESENT. NO INFO MESSAGES OR OMS MESSAGES RELATEDAug 10, 2019 · N109DU · Bombdr BD1001A10 · Drag Control System
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