# Service difficulty reports: N106DU

A list on [N106DU](https://openairdocs.org/aircraft/N106DU.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 60 reports

- [SDR DALA2026052603173](https://openairdocs.org/sdr/DALA2026052603173.md): Bleed Valve · faulted · May 19, 2026 · N106DU · Airbus BD5001A10 · Compressor Bleed Valve
  > DIV - 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 DALA2026040802255](https://openairdocs.org/sdr/DALA2026040802255.md): Bleed Air Sys · failed · Apr 3, 2026 · N106DU · Airbus BD5001A10 · Engine Bleed Air System
  > DIVERTED TO DEN DUE TO LT BLEED FAIL CLOSED. FLIGHT SAFELY ON THE GROUND. R & R LT ENGINE HPV. (LP 8313718, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026031701844](https://openairdocs.org/sdr/DALA2026031701844.md): Rudder · damaged · Mar 12, 2026 · N106DU · Airbus BD5001A10 · Rudder Structure
  > RUDDER 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 DALA2026022601375](https://openairdocs.org/sdr/DALA2026022601375.md): Rib · damaged · Feb 24, 2026 · N106DU · Airbus BD5001A10 · Vertical Stabilizer, Spar/Rib
  > DURING 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# 84
- [SDR DALA2026012100453](https://openairdocs.org/sdr/DALA2026012100453.md): Engine · odor · Jan 15, 2026 · N106DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > RETURNED 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 DALA2025122609408](https://openairdocs.org/sdr/DALA2025122609408.md): Pin · inoperative · Dec 25, 2025 · N106DU · Airbus BD5001A10 · Escape Slide
  > LEFT 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 RE
- [SDR DALA2026030201407](https://openairdocs.org/sdr/DALA2026030201407.md): Unknown · odor · Dec 7, 2025 · N106DU · Airbus BD5001A10 · Air Distribution System
  > FUMES 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 DALA2026030201408](https://openairdocs.org/sdr/DALA2026030201408.md): Ecs · contaminated · Nov 22, 2025 · N106DU · Airbus BD5001A10 · Cabin Cooling System
  > ODOR 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 DECONTAMINA
- [SDR DALA2025112108507](https://openairdocs.org/sdr/DALA2025112108507.md): Hydraulic System · leaking · Nov 20, 2025 · N106DU · Airbus BD5001A10 · Hydraulic System, Main
  > SHIP 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 DALA2026030201405](https://openairdocs.org/sdr/DALA2026030201405.md): Spinner · contaminated · Nov 9, 2025 · N106DU · Airbus BD5001A10 · Turbine Engine Oil System
  > ON 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 DALA2025111208277](https://openairdocs.org/sdr/DALA2025111208277.md): Light · inoperative · Nov 9, 2025 · N106DU · Airbus BD5001A10 · Emergency Lighting
  > R/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 DALA2025111208276](https://openairdocs.org/sdr/DALA2025111208276.md): Light · inoperative · Nov 9, 2025 · N106DU · Airbus BD5001A10 · Emergency Lighting
  > L/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 DALA2025102907935](https://openairdocs.org/sdr/DALA2025102907935.md): Engine · odor · Oct 23, 2025 · N106DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > DIRTY 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 DALA2025102007626](https://openairdocs.org/sdr/DALA2025102007626.md): A/C Pack · odor · Oct 14, 2025 · N106DU · Airbus BD5001A10 · Cabin Cooling System
  > FUMES 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 & BLEE
- [SDR DALA2025102007623](https://openairdocs.org/sdr/DALA2025102007623.md): Unknown · odor · Oct 12, 2025 · N106DU · Airbus BD5001A10 · Air Distribution System
  > ON 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 7
- [SDR DALA2025101607580](https://openairdocs.org/sdr/DALA2025101607580.md): Spinner · leaking · Oct 10, 2025 · N106DU · Airbus BD5001A10 · Turbine Engine Oil System
  > ON 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 P
- [SDR DALA2025091006688](https://openairdocs.org/sdr/DALA2025091006688.md): Seal · torn · Sep 9, 2025 · N106DU · Airbus BD5001A10 · Cabin Pressure Control System
  > AT 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 DALA2025090206509](https://openairdocs.org/sdr/DALA2025090206509.md): Engine · odor · Sep 1, 2025 · N106DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > RETURNED 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 TO
- [SDR DALA2025043003336](https://openairdocs.org/sdr/DALA2025043003336.md): Bleed Air Sys · odor · Apr 27, 2025 · N106DU · Airbus BD5001A10 · APU Bleed Air System
  > 800 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 DALA2025043003335](https://openairdocs.org/sdr/DALA2025043003335.md): A/C Pack · odor · Apr 25, 2025 · N106DU · Airbus BD5001A10 · Cabin Cooling System
  > DIRTY 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 S
- [SDR DALA20250429001](https://openairdocs.org/sdr/DALA20250429001.md): Skin · corroded · Apr 12, 2025 · N106DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/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 AIR
- [SDR DALA2025042903301](https://openairdocs.org/sdr/DALA2025042903301.md): Skin · corroded · Apr 12, 2025 · N106DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/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 TOT
- [SDR DALA2025041703030](https://openairdocs.org/sdr/DALA2025041703030.md): Door Sill · corroded · Apr 12, 2025 · N106DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD 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 ASSOC
- [SDR DALA2025041703029](https://openairdocs.org/sdr/DALA2025041703029.md): Skin · corroded · Apr 12, 2025 · N106DU · Airbus BD5001A10 · Cargo/Baggage Doors
  > FWD 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 DALA2025040802749](https://openairdocs.org/sdr/DALA2025040802749.md): Seat Track · corroded · Apr 4, 2025 · N106DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***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 DALA2025040802748](https://openairdocs.org/sdr/DALA2025040802748.md): Seat Track · corroded · Apr 3, 2025 · N106DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED 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 DALA2025033102391](https://openairdocs.org/sdr/DALA2025033102391.md): Seat Track · corroded · Mar 27, 2025 · N106DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***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 DALA2025032602228](https://openairdocs.org/sdr/DALA2025032602228.md): Seat Track · corroded · Mar 21, 2025 · N106DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***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 -0
- [SDR DALA2025032602236](https://openairdocs.org/sdr/DALA2025032602236.md): Door · damaged · Mar 19, 2025 · N106DU · Airbus BD5001A10 · Cargo/Baggage Doors
  > FWD 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 NECES
- [SDR DALA2025031201905](https://openairdocs.org/sdr/DALA2025031201905.md): Seat Track · corroded · Mar 11, 2025 · N106DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED 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 DALA2025040902771](https://openairdocs.org/sdr/DALA2025040902771.md): Protector · damaged · Dec 25, 2023 · N106DU · Airbus BD5001A10 · Wing Main, Frame Structure
  > FOUND 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 DALA2023122110506](https://openairdocs.org/sdr/DALA2023122110506.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 & P
- [SDR DALA2023122110505](https://openairdocs.org/sdr/DALA2023122110505.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 M
- [SDR DALA2023122110504](https://openairdocs.org/sdr/DALA2023122110504.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 DALA2023122110503](https://openairdocs.org/sdr/DALA2023122110503.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 DALA2023122110502](https://openairdocs.org/sdr/DALA2023122110502.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 DALA2023122110501](https://openairdocs.org/sdr/DALA2023122110501.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > REMEASURE 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 MATCH
- [SDR DALA2023122110500](https://openairdocs.org/sdr/DALA2023122110500.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH 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 PRIO
- [SDR DALA2023122110499](https://openairdocs.org/sdr/DALA2023122110499.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH 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 I
- [SDR DALA2023122110498](https://openairdocs.org/sdr/DALA2023122110498.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LT 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 DALA2023122110497](https://openairdocs.org/sdr/DALA2023122110497.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 AN
- [SDR DALA2023122110496](https://openairdocs.org/sdr/DALA2023122110496.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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, PRI
- [SDR DALA2023122110495](https://openairdocs.org/sdr/DALA2023122110495.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH 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 FUR
- [SDR DALA2023122110494](https://openairdocs.org/sdr/DALA2023122110494.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 DALA2023122110493](https://openairdocs.org/sdr/DALA2023122110493.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 RE
- [SDR DALA2023122110492](https://openairdocs.org/sdr/DALA2023122110492.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH 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 REQ
- [SDR DALA2023122110491](https://openairdocs.org/sdr/DALA2023122110491.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 RE
- [SDR DALA2023122110490](https://openairdocs.org/sdr/DALA2023122110490.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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 PR
- [SDR DALA2023122110489](https://openairdocs.org/sdr/DALA2023122110489.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > RH 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 FLIGHT
- [SDR DALA2023122110488](https://openairdocs.org/sdr/DALA2023122110488.md): Unknown · unknown · Dec 20, 2023 · N106DU · Bombdr BD1001A10 · Leading Edge Devices
  > LH 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.

Next page: https://openairdocs.org/aircraft/N106DU/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N106DU/reports

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