N106DU
Service difficulty reports · 60
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 = 'N106DU' 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.
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 = 'N106DU' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2026052603173Bleed Valve · faultedDIV - TO MCI DUE TO LT BLEED FAIL FAULTING LT HPV FAILED CLOSED WITH WEATHER IN TEXAS UNABLE TO CONTINUE. REMOVED AND REPLACED LT HPV VALVE, OPS CHECK GOOD. (LP 8639908 - AIRCRAFT WAS GROUNDED)SDR DALA2026040802255Bleed Air Sys · failedDIVERTED TO DEN DUE TO LT BLEED FAIL CLOSED. FLIGHT SAFELY ON THE GROUND. R & R LT ENGINE HPV. (LP 8313718, AIRCRAFT WAS GROUNDED)SDR DALA2026031701844Rudder · damagedRUDDER PERMANENT REPAIR PER ERA 632577-14 REVISION ORIGINAL SECTION IV. ERA 632577 REV ORIGINAL SEC IV COMPLIED WITH PERMANENT REPAIR PER ERA 632617-14. (LP# 8456720)SDR DALA2026022601375Rib · damagedDURING REPAIR OF LOG 8456712 FOUND HINGE RIB 1, HINGE RIB 2,AND LWR CLOSURE RIB DAMAGED. WILL REQUIRE REPLACEMENT. REPAIR WORK COMPLIED WITH PRI 632577-14 REV 2. FINAL ERA 632577- 14 REV, ORIGINAL MATCHES. ALL RII'S COMPLIED WITH LEAK CK + OPS CK GOOD. (LP# 84SDR DALA2026012100453Engine · odorRETURNED TO SEA DUE TO FUMES IN FLIGHT DECK AND CABIN. CREW DONNED O2 MASKS. TROUBLESHOT IAW MSI WORKCARDS. ISOLATED ODOR TO NR 2 ENGINE. PERFORMED ECS DECONTAMINATION IAW JIC 0550-2003. REPLACED RECIRCULATION FILTERS. (LP# 8195694)SDR DALA2025122609408Pin · inoperativeLEFT OVERWING EMERGENCY EXIT DOOR SLIDE WOULD NOT PIN. PERFORMED SLIDE DEPLOYMENT IAW WC 2561-9005. WILL REQ NEW SLIDE. DURING INSTALL IF NEW SLIDE FOUND CABLE OUT OF RIG. CHECKED RIG PER A220 AMP 52-21 THROUGH STEP F. (203641) RE-RIGGED SHORT CABLE ABD C/W RESDR DALA2026030201407Unknown · odorFUMES NOTED AFTER ROTATION AND DURING CLIMB. STRONG METALLIC TASTE AND BURNING SENSATION IN EYES NOTED. ACRID ODOR NOTED ALSO. BOTH ENGINES REPLACED. REF LOG #'S 1337408, 1337407, AND 133904 FOR CORRECTIVE ACTION. (LP# 7670644)SDR DALA2026030201408Ecs · contaminatedODOR EVENT, STARTED AFTER T/O. SMELLED LIKE GLYCOL BUT WE DIDN'T DEICE. SMELL NEVER WENT AWAY. USED O2 MASKS. WHEN WE TOOK MASKS OF AT GATE THERE WAS A STRONG DIRTY SOCK SMELL. PERFORMED W/C 0500-2001. NO ODORS NOTED. (WIP HM 959004). PERFORMED ECS DECONTAMINASDR DALA2025112108507Hydraulic System · leakingSHIP 8106 - MISC / DE - CREW REPORTED NR 3 HYDRAULIC SYSTEM QTY AND PRESSURE LOW MESSAGES. DECLARED AN EMERGENCY. LANDED SAFELY. REPLACED 3A AND 3B ACMP. (LP# 7670624)SDR DALA2026030201405Spinner · contaminatedON TAKEOFF COCKPIT HAD DIRTY SOCK SMELL BUT MASKED BY TYPE I FLUID THAT HAD JUST BEEN APPLIED. NO SMELL ANYWHERE ELSE. SMELL RETURNED WITH THRUST REVERSE APPLICATION. DISSIAPATED WITH APU USE. INSPECTED BOTH ENG INLETS , PACK INLETS AND APU INLETS NO EVIDENCE SDR DALA2025111208277Light · inoperativeR/H FWD FUSELAGE EXTERIOR EMER LIGHT INOP (NEAR R1 DOOR). R/R THE R/H FWD FUSELAGE EXTERIOR EMER LIGHT ASSEMBLY. CHECKS GOOD. A220 AMP 33-55. (LP# 8002585)SDR DALA2025111208276Light · inoperativeL/H AFT FUSELAGE EXTERIOR EMER LIGHT INOP (NEAR L2 DOOR). R/R THE L/H AFT FUSELAGE (REAR BARREL) EXTERIOR EMER LIGHT ASSEMBLY . CHECKS GOOD. A220 AMP 33-55. (LP# 8002584)SDR DALA2025102907935Engine · odorDIRTY SOCK SMELL IN COCKPIT AND CABIN AFTER TAKE OFF. C/W STEP 1 AMDS WORKCARD 0550-2001. C/W STEP 2 FOUND #2 ENG AT FAULT. C/W STEP 3 DECONTAMINATION IAW WORKCARD 0550-2003. C/W STEP 4 NOTIFIED MCC. C/W STEP 5 AMDS WORKCARD 0550-9001-A220. (LP# 1267779)SDR DALA2025102007626A/C Pack · odorFUMES IN COCKPIT ON CLIMB OUT. RETURN TO FIELD. ODOR PERSISTS. OPERATED LEFT & RIGHT PACK ON BOTH APU & RT ENG BLEED. VERIFIED SOURCE OF SMELL TO BE COMING FROM LEFT PACK. NO SMELL DURING RIGHT PACK OPS ON EITHER RT ENG OR APU BLEED SOURCE. ALL ENG RUNS & BLEESDR DALA2025102007623Unknown · odorON SHORT FINAL FA REPORTED DIRTY SOCK ODOR. REPORTED TO CAPT AFTER CLEARING RUNWAY. STARTED APU SMELL DISSIPATED. NO SMOKE, JUST ODOR. ON ARRIVAL CHECKED BOTH ENG OIL LEVEL ON NR 1 & 2 ENGS. BOTH ENG'S WERE NOT OVER SERVICED. REMOVED NR1 ENG SPINNER IAW AMP 7SDR DALA2025101607580Spinner · leakingON APPROACH AND SHORTLY AFTER LANDING CABIN CREW AS WELL AS FLIGHT CREW NOTED "DIRTY SOCK" SMELL. ODOR DISSIPATED SHORTLY AFTER TOUCHDOWN DURING TAXI IN. DURING INSPECTION FOUND OIL ON BOTH ENGINE SPINNER CONES. REPLACED FAN SHAFT COVER O-RING ON #1 & #2 ENG PSDR DALA2025091006688Seal · tornAT FL 380 RECEIVED CABIN ALTITUDE CAUTION. CREW COMPLIED WITH QRH DECLARED EMERGENCY AND DONNED O2 MASKS AND DESCENDED TO FL 200. CREW WAS ABLE TO STABILIZE CABIN PRESSURE IN MANUAL. PASSENGER O2 MASKS DID NOT DEPLOY. CREW HAS ELECTED TO CONTINUE ON TO SNA. SDR DALA2025090206509Engine · odorRETURNED TO BOS DUE TO DIRTY SOCK SMELL. MTC PERFORMED TROUBLESHOOTING FOUND ODOR COMING FROM RIGHT ENGINE. PERFORMED BOROSCOPE INSPECTION FOUND BIRD DEBRIS COMPRESSOR STAGES 1,2 AND 3. SUSPECT BIRD STRIKE DEBRIS FROM PRIOR FLIGHT. MAINTENANCE FERRIED A/C TOSDR DALA2025043003336Bleed Air Sys · odor800 FT ON APPROACH FO SMELLED DIRTY SOCK ODER , 500 FT CA SMELLED IT AS WELL.APU WAS STARTED ONCE LANDED .R BLEED TURNED OFF SMELL DISAPPEARED. DUCT BURNOUT C/ W AGAIN WITH RT ENG PER AMDS CARD 0550-2008.LT ENG BLEED LOCKED BACK PER AMP 36-11 AS NOTED IN LOG #SDR DALA2025043003335A/C Pack · odorDIRTY SOCK SMELL ON TAXI OUT .STARTED IN FLT DECK AND CONTINUED THROUGH CABIN.PACKS ON ENGINES.TURNED LEFT PACK OFF AND SMELL DISAPPEARED FOR 1-2 MINUTES BUT SHORTLY RETURNED.SWITCHED TO APU BLEED ON TAXI BACK TO THE GATE AND SMELL REMAINED. PERFORMED T/S OF SSDR DALA20250429001Skin · corrodedER/A 625049-14; A220-100 / FWD FUSELAGE / FWD CARGO DOOR CUTOUT / FR 24-29 / BOTTOM SKIN AND SILL / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 625049-14, SECTION V REPETITIVE INSPECTION WITHIN 50,050 FLIGHT HOURS FROM 11,686 TOTAL AIRSDR DALA2025042903301Skin · corrodedER/A 625049-14; A220-100 / FWD FUSELAGE / FWD CARGO DOOR CUTOUT / FR 24-29 / BOTTOM SKIN AND SILL / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 625049-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 11,686 TOTSDR DALA2025041703030Door Sill · corrodedFWD CARGO LOWER SILL SURFACE COVERED BY SCUFF PLATE HAS CORROSION AROUND FASTENER HOLES FROM FR24 TO FR29. (MARKED) SSI: 53-21-25-02. (NO PRESENCE OF BLUE PAINT OR BLUE INK INDICATING PREVIOUS CORROSION REPAIR). ACCOMPLISHED ERA 625049 REV ORG SECTION IV ASSOCSDR DALA2025041703029Skin · corrodedFWD CARGO DOOR LOWER SKIN SURFACE COVERED BY SCUFF PLATE HAS CORROSION IN THE SURROUNDING AREA OF SCREW HOLE #14OL. (MARKED) REF AA# 5331-01297-01C. ACCOMPLISHED ERA 625049-14 REV ORG SECTION 1 ASSOCIATED ER/A 14-625049 ADDED FOR AC 8106. (LP# 0910152)SDR DALA2025040802749Seat Track · corroded***CORROSION*** CABIN SEAT TRACK SURFACE FR 74 RBL 43 WL 151.5 . REMOVED AND REPLACED SEAT TRACK RBL 43 AT STA FR61 TO FR 74 WL151.5 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV-G. (LP# 0895527)SDR DALA2025040802748Seat Track · corrodedCORRODED CABIN SEAT TRACK UPPER SURFACE FR 74 LBL 23 WL 151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR61 TO 74 LBL 23 WL 151.5 IAW BOMBARDIER PL CO1342701 REV E. (LP# 0893236)SDR DALA2025033102391Seat Track · corroded***CORROSION*** CABIN SEAT TRACK UPPER SURFACE FR19 RBL 23 WL 151.5. REMOVED AND REPLACED SEAT TRACK AT STA FR 20 TO FR 34 RBL23 WL 151.5 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV:-E. (LP# 0880601)SDR DALA2025032602228Seat Track · corroded***CORROSION*** CABIN SEAT TRACK UPPER SURFACE FR 74 LBL 43 WL 151.5. REMOVED AND REPLACED SEAT TRACK BETWEEN FR61+13" TO FR 74+6", LBL 43, WL 151.5 IAW BOMBARDIER DWG : C01342701 REV :G AND A220 ASRP BD500-A-J51-42-20-00AAA-0748A-A. ** -0748A-A SHOULD READ -0SDR DALA2025032602236Door · damagedFWD CARGO COMPARTMENT DOOR AFT LOWER CORNER IS DAMAGED (MARKED). REMOVED DAMAGE AT FWD CARGO COMPARTMENT DOOR AFT LOWER CORNER IAW A220 ASRP BD500-A-J52J30-01-01AAA-664A-A AND INSTALLED REPAIR PARTS. (2A) A DTE HAS DETERMINED THAT A SPECIAL INSPECTION IS NECESSDR DALA2025031201905Seat Track · corrodedCORRODED CABIN SEAT TRACK UPPER SURFACE FR20 RBL 43 WL 151.5. REMOVED AND REPLACED SEAT TRACK AT RBL 43 FROM FR19 TO FR30 IAW A22O ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DRW# C02312600 REV E. (LP# 0852293)SDR DALA2025040902771Protector · damagedFOUND LEADING EDGE PROTECTOR MATERIAL DAMAGED/MISSING ON RIGHT WINGLET . REPLACED MISSING LEADING EDGE EROSION PROTECTIVE MATERIAL ON RIGHT WINGLET IAW A220 AMP BD500-A-J51-22-01-00AAA-621A-A. NO FURTHER DAMAGE NOTED. OK TO CLOSE MONITOR. (LP# 5534229)SDR DALA2023122110506Unknown · unknownLH SLAT TRACK #6 UPPER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #6 UPPER PER ERA 607543-14AD REV. B & PSDR DALA2023122110505Unknown · unknownLH SLAT TRACK #6 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA5742-01028A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #6 LOWER PER ERA 607543-14AD REV B & PRI REV 0 MSDR DALA2023122110504Unknown · unknownLH SLAT TRACK #5 LOWER SURFACE HAS CORROSION AT AFT AND FWD ROLLER. EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA5742-01028 -02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK # 5 LOWER PER ERA 607543-14AD REV B SDR DALA2023122110503Unknown · unknownLH SLAT TRACK #4 UPPER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #4 UPPER PER ERA 607543-14AD REV B & PRI SDR DALA2023122110502Unknown · unknownLH SLAT TRACK #4 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #4 LOWER PER ERA 607543-14AD REV B & PRI REV SDR DALA2023122110501Unknown · unknownREMEASURE H AND W DIMENSIONS ON LH SLAT TRACK 9 FOR CLARIFICATION. REMEASURED H W1 AND W2 UPPER AND LOWER ON LH SLAT TRACK #9 PER ERA 607541-14AD REV B AND PRI REV 0 MATCHSDR DALA2023122110500Unknown · unknownRH SLAT TRACK #11 UPPER AND LOWER AT AFT ROLLER HAS CORROSION "M " PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028-02B. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOSDR DALA2023122110499Unknown · unknownRH SLAT TRACK #10 UPPER AT AFT ROLLER HAS CORROSION FWD AND AFT HAS CORROSION"M" PROVIDED TO ASSIST WITH LOCATION. REF 5742- 01028-02B. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION ISDR DALA2023122110498Unknown · unknownLT SLAT TRACK #11 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #11 UPPER PER ERA 607543-14AD REV. B AND SDR DALA2023122110497Unknown · unknownLH SLAT TRACK #10 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028- 02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #10 UPPER PER ERA 607543-14AD REV. B ANSDR DALA2023122110496Unknown · unknownLH SLAT TRACK #1 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #1 LOWER PER ERA 60754314AD REV B, PRISDR DALA2023122110495Unknown · unknownRH SLAT TRACK #7 UPPER AND LOWER AT AFT ROLLER HAS CORROSION. "M " PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028-02A. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURSDR DALA2023122110494Unknown · unknownLH SLAT TRACK # 10 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H # 10 LOWER SLAT TRACK PER ERA 607543-14AD REV. B SDR DALA2023122110493Unknown · unknownLH SLAT TRACK#9 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #9 UPPER PER ERA 607543-14AD REV. B AND PRI RESDR DALA2023122110492Unknown · unknownRH SLAT TRACK #8 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION "M" PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028- 02B EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING SUPPOIRT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQSDR DALA2023122110491Unknown · unknownLH SLAT TRACK 9 LOWER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #9 LOWER PER ERA 607543-14AD REV. B AND PRI RESDR DALA2023122110490Unknown · unknownLH SLAT TRACK #8 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #8 UPPER PER ERA 607543-14AD REV. B AND PRSDR DALA2023122110489Unknown · unknownRH SLAT TRACK #6 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION. "M" PROVIDED TO ASSIST WITH LOCATION. EVIDENCE OF PREVIOUS IS PRESENT. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED . ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR FURTHER FLIGHTSDR DALA2023122110488Unknown · unknownLH SLAT TRACK #8 LOWER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED SLAT TRACK #8 LOWER PER ERA 667543-14AD REV B AND PRI REV.
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