# Service difficulty reports: N107DU

A list on [N107DU](https://openairdocs.org/aircraft/N107DU.md).

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

- [SDR DALA2026011400341](https://openairdocs.org/sdr/DALA2026011400341.md): Oil Cooler · leaking · Jan 12, 2026 · N107DU · Airbus BD5001A10 · Engine Oil Temperature Regulator
  > ATB/FUMES - RETURNED TO MSP DUE TO FUMES IN THE FLIGHT DECK AND CABIN. PERFORMED HIGH POWER ENGINE RUNS WITH NO ODORS FOUND. P-TRACK DATA INDICATED APU AS LIKELY SOURCE OF ODOR. APU INSPECTION IN WORK. FOUND #2 ENGINE AIR/OIL COOLER CRACKED. SAME REPLACED. (
- [SDR DALA2025071705372](https://openairdocs.org/sdr/DALA2025071705372.md): Unknown · odor · Jul 12, 2025 · N107DU · Airbus BD5001A10 · Air Distribution System
  > PRIOR TOD AT FL 340 STRONG SMELL OF BURNING ELECTRICAL. THE SMELL DISSIPATED 5 MINUTES LATER. OXYGEN MASKS WERE DEPLOYED IN THE COCKPIT. REF LP#: 1077551 FOR T/S & ODI COMPLETION. T/S PER A220 EFIM. FOUND ALL (5) AFDS DIRTY & CAKED W/ DUST. CLEANED PER AMP 31-
- [SDR DALA2026031101697](https://openairdocs.org/sdr/DALA2026031101697.md): Door Frame · corroded · Jul 10, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD SERVICE DOOR CUTOUT FASTENER HOLES FOR TRIM NUT PLATES AT FR17 AND FR20 SHOW OXIDATION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0568:5321-2013/003 00338 REPAIRED IAW PRI 627026-14 REV 0, PRI 627026-14 REV 1, PRI 627026-14 REV 2, PRI 627026-14 REV 3,
- [SDR DALA2026031101696](https://openairdocs.org/sdr/DALA2026031101696.md): Door Frame · corroded · Jul 10, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD PAX DOOR FRAME 19 HAS MULTIPLE FASTENER HOLES WITH CORROSION. REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORIGINAL SECTION 1. (LP# 1074103)
- [SDR DALA2026031101695](https://openairdocs.org/sdr/DALA2026031101695.md): Door Frame · corroded · Jul 10, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD PAX DOOR FRAME 22 HAS MULTIPLE FASTENER HOLES WITH CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0567:5321-2009/003 00324 REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORI
- [SDR DALA2025070805074](https://openairdocs.org/sdr/DALA2025070805074.md): Skin · corroded · Jul 1, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FUSELAGE SKIN FWD OF THE WASTE BOX AND FRAME 75. (P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0549:0500-2020/004 00354 COMPLIED WITH ER/A PRI 597330-14 REV 0, REV 1, AND FINAL ERA 597330-14AD
- [SDR DALA2025070304969](https://openairdocs.org/sdr/DALA2025070304969.md): Seat Track · corroded · Jun 30, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 43.5. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/003 00303 REMOVED AND REPLACED AFT FUSELAGE SEAT TRACK PER A220 ASRP 51-77-00. (LP# 1055505)
- [SDR DALA2025070104901](https://openairdocs.org/sdr/DALA2025070104901.md): Door Sill · corroded · Jun 29, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT CARGO LOWER SILL FWD CORNER STRIKER HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0523:5300-2012/002 00456 COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A
- [SDR DALA2025070104900](https://openairdocs.org/sdr/DALA2025070104900.md): Door Sill · corroded · Jun 29, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT CARGO LOWER SILL AFT CORNER STRIKER HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0523:5300-2012/003 00457 COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A
- [SDR DALA2025070104902](https://openairdocs.org/sdr/DALA2025070104902.md): Drain Mast · corroded · Jun 28, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD FUSELAGE DRAIN MAST CUTOUT / CORROSION UNDER FWD DRAIN MAST. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0471:3833-2001/002 00525 COMPLIED WITH PRI 627174-14 REV 0, PRI 627174-14 REV 1 AND FINAL ER/A 627174-14 REV ORIGINAL. SECTION I, SEE LOG # 1036214.
- [SDR DALA2025070104899](https://openairdocs.org/sdr/DALA2025070104899.md): Door Sill · corroded · Jun 28, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR LOWER SILL SURROUND STRUCTURE HAS CORROSION AROUND SEVERAL FASTENER HOLES. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0523:5300-2012/001 00269 COMPLIED WITH PRI 626953-14 REV 0, PRI 6269
- [SDR DALA2025070104898](https://openairdocs.org/sdr/DALA2025070104898.md): Structure · corroded · Jun 28, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AROUND AND ON COUNTERSINK BOLT HOLES10L, 30L, AND 70L. COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A 626953-14 REV ORIGINAL. SECTION I, SEE LOG # 1048121. REP INSPECTIONS. COMPLIED WITH PRI 62695
- [SDR DALA2025070104897](https://openairdocs.org/sdr/DALA2025070104897.md): Beam · corroded · Jun 28, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD CARGO - LOWER SILL BEAM HAS CORROSION IN SCUFF PLATE ATTACH HOLES (M)(P). COMPLIED WITH ER/A 626994-14 PRI REV0, ER/A 626994-14 PRI REV 1 AND FINAL ER/A 626994-14 REV ORIGINAL SECTION I. SEE LOG # 1043585 FOR SECTION II REP. INSPECTION. COMPLIED WITH ER/
- [SDR DALA2025070104892](https://openairdocs.org/sdr/DALA2025070104892.md): Attach Bracket · corroded · Jun 26, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Equipment Attach Fittings
  > AFT FUSELAGE GALLEY FLOOR SUPPORT BEAM GALLEY ATTACH BRACKET AT FR79 AND RBL23 HAS CORROSION ON UPPER SURFACE AND OXIDATION IN BORE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2016/003 00359 CORROSION CO
- [SDR DALA2025070104890](https://openairdocs.org/sdr/DALA2025070104890.md): Threshold · corroded · Jun 25, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Structure
  > 2R DOOR THRESHOLD PANEL FWD AND AFT INBD CORNERS HAVE CORROSION. -M-. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2016/001 00353 REMOVED AND REPLACED AFT SERVICE DOOR THRESHOLD PANEL REF A220 AMP 53-00-47. (LP# 1044440)
- [SDR DALA2025062504765](https://openairdocs.org/sdr/DALA2025062504765.md): Tie Down · corroded · Jun 21, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Attach Fittings
  > FWD FUSELAGE CLOSET HOLD DOWN AT FR20. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0570:5321-2022/002 00332 REMOVED AND REPLACED CLOSET HOLD DOWNS REF A220 AMP 25-24 -11. (LP# 1037701)
- [SDR DALA2025062504764](https://openairdocs.org/sdr/DALA2025062504764.md): Tie Down · corroded · Jun 21, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Attach Fittings
  > FWD FUSELAGE CLOSET HOLD DOWNS AT FR20 AND FR 22 AND RBL 43.5 CORRODED BETWEEN MOUNT AND SEAT TRACK. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0570:5321-2022/001 00331. REMOVED AND REPLACED CLOSET HOLD DOWNS REF A220 AMP 25-24 -11. (LP# 1037697)
- [SDR DALA2025062504762](https://openairdocs.org/sdr/DALA2025062504762.md): Frame · corroded · Jun 21, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Frame
  > FOUND FR40 WITH CORROSION IN SEVERAL HOLES FROM STGL32 TO STGR32. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0037:5123-4002/002 00521 REMOVED AND REPLACED LH AND RH FR 40 PER DRAWING A220 C02382210 REV A. (LP# 103
- [SDR DALA2025062504757](https://openairdocs.org/sdr/DALA2025062504757.md): Seat Track · corroded · Jun 21, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/005 00305 REMOVED AND REPLACED AFT SEAT TRACK PER ER/A 623168-14TR. SCEPTRE LOG PAGE ENTERED FOR S
- [SDR DALA2025062404725](https://openairdocs.org/sdr/DALA2025062404725.md): Seat Track · corroded · Jun 20, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 LBL 43.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/006 00306 REMOVED AND REPLACED SEAT TRACK PER ER/A 62 3167-14TR REV O SECTION 1 CLOSING REQUIREME
- [SDR DALA2025062404712](https://openairdocs.org/sdr/DALA2025062404712.md): Seat Track · corroded · Jun 18, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 20 RBL 43.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/002 00302 REPLACED SEAT TRACK PER A220 ASRP 51-77-00. (LP# 1032018)
- [SDR DALA2025062004645](https://openairdocs.org/sdr/DALA2025062004645.md): Bracket · out of limits · Jun 17, 2025 · N107DU · Airbus BD5001A10 · Aileron Control System
  > R/H AILERON ANTI-MIGRATION BRACKETS CLEARANCE TOLERANCES OUT OF LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0004:2715-4001-RH/003 00541 ADJUSTED R/H AILERON ANTI-MIGRATION BRACKETS CLEARANCE REF A220 AMP 27
- [SDR DALA2025062004644](https://openairdocs.org/sdr/DALA2025062004644.md): Seat Track · corroded · Jun 16, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION FWD OF STA 20 RBL 23 SSI: 53- 21-43-01. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/001 00301 REPLACED PER A220ASRP 51-77-00. (LP# 1027215)
- [SDR DALA2026031101698](https://openairdocs.org/sdr/DALA2026031101698.md): Floorbeam · corroded · Jun 14, 2025 · N107DU · Airbus BD5001A10 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR EDGE SUPPORT BEAM HAS CORROSION AROUND MOUNT HOLE APPROX 10" FWD OF FR79 AND 12" OUTBOARD OF LBL 43.5. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2016/002 00357 REMOVED AND REPLACED FLOOR SILL REF A220 ASRP 51-77-00- 00AAA-028A-A.
- [SDR DALA2025061804586](https://openairdocs.org/sdr/DALA2025061804586.md): Seat Track · corroded · Jun 14, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/004 00304 BLENDED AND CHECKED LIMITS PER A220 ASRP53-61-49-00-661 AND REPLACED PER A220ASRP 51-77-0
- [SDR DALA2025061704572](https://openairdocs.org/sdr/DALA2025061704572.md): Seat Track · corroded · Jun 13, 2025 · N107DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > RH INBD SEAT TRACK FLOOR PANEL BRACKET CRACKED AT FR34-FR35. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0186:2040-0094/001 00524 REMOVED AND REPLACED BRACKET PER A220 ASRP 51-40-00. (LP# 1022780)
- [SDR DALA2023111009274](https://openairdocs.org/sdr/DALA2023111009274.md): Unknown · unknown · Nov 7, 2023 · N107DU · Bombdr BD1001A10 · Air Distribution System
  > W/O MCC APPROVAL" - DIRTY SOCK/OIL ODOR INCOCKPIT DURING CLIMBOUTODOR CLEARED ABOVE. PERFORMED EFIM T/S + W/C 0550-2001. FOUND SYS 2 HYD OVERSERVICED. DRAINED SYS 2 IAW A220 AMP TASK BD500-A-J12-10-29-01AAA-228A-A. SYS 2 WITHIN LIMITS WIP B.STRUCK 890079.C/W
- [SDR DALA2023050903633](https://openairdocs.org/sdr/DALA2023050903633.md): Unknown · unknown · Mar 31, 2023 · N107DU · Bombdr BD1001A10 · Leading Edge Devices
  > ER/A 607497-14AD ISSUED FOR DAMAGE TO THE RH WING SLAT TRACKS #1-11. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 607497-14AD SECTION II EVERY 850FH FOLLOWING THE ACCOMPLISHMENT OF SECTION I. ACCOMPLISH SECTION III WITHIN 8500FH FOLLOWING THE ACCOMPLISHMENT O
- [SDR DALA2023050903632](https://openairdocs.org/sdr/DALA2023050903632.md): Unknown · unknown · Mar 31, 2023 · N107DU · Bombdr BD1001A10 · Leading Edge Devices
  > ER/A 607499-14AD ISSUED FOR DAMAGE TO THE LH WING SLAT TRACKS #1-11. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 607499-14AD SECTION II EVERY 850FH FOLLOWING THE ACCOMPLISHMENT OF SECTION I. ACCOMPLISH SECTION III WITHIN 8500FH FOLLOWING THE ACCOMPLISHMENT O
- [SDR DALA2022110207098](https://openairdocs.org/sdr/DALA2022110207098.md): Slide · not reported · Oct 27, 2022 · N107DU · Bombdr BD1001A10 · Escape Slide
  > AIRCRAFT 8107, RH OVER WING SLIDE REQUIRES REPLACEMENT PER AMDS 2561-01380-02 SHORT CABLE REQUIRES RIGGING. UNABLE TO INSTALL SAFETY PIN IN REMOVED SLIDE BOTTLE. CORRECTIVE ACTION: REPLACED SLIDE. LP 2471282
- [SDR DALA2022110207097](https://openairdocs.org/sdr/DALA2022110207097.md): Slide · failed · Oct 27, 2022 · N107DU · Bombdr BD1001A10 · Escape Slide
  > AIRCRAFT 8107, LH OVERWING SLIDE NEEDS REPLACED PER AMDS 2561-01380-01. FOUND SCREW HEAD PROTRUDING FROM CABLE SLIDER COVER. SHORT CABLE NEEDS RIGGED BECAUSE BOTTLE SAFETY PIN DID NOT LINE UP. SLID FAILED DEPLOYMWNT DUE TO FAILURE TO STAY INFLATED. CORRECTTIVE
- [SDR DALA2022051203307](https://openairdocs.org/sdr/DALA2022051203307.md): Strip · missing · May 11, 2022 · N107DU · Bombdr BD1001A10 · Emergency Lighting
  > EPL STRIP ON FLOOR AT 10B MISSING. REPLACED EPL STRIP AT 10B WITH ROBBED PART FROM 8142. (LP# 8724481)
- [SDR DALA2022042202830](https://openairdocs.org/sdr/DALA2022042202830.md): Waste Box · corroded · Feb 16, 2022 · N107DU · Bombdr BD1001A10 · Fuselage Internal Mounting Structure
  > ER/A 597330-14AD ISSUED FOR CORROSION ON THE LOWER AFT FUSELAGE AT THE WASTE SERVICE COMPARTMENT. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II WITHIN 8500FH FOLLOWING THE ACCOMPLISHMENT OF SECTION I. ASSOCIATED ER/A 00-597330 ADDED FOR AC 8107. (LP# 212
- [SDR DALA2022012500519](https://openairdocs.org/sdr/DALA2022012500519.md): None · none · Jan 20, 2022 · N107DU · Bombdr BD1001A10 · Trailing Edge Flaps
  > #2 FLAP TRACK FAIRING DENT. INSP AND FOUND RIGHT WING #3 FLAP TRACK FAIRING CRACKED (~2 5/16 " LONG) AND DELAMINATED (1" X 2 5/16 " = 2.3125 IN2) IN ZONE E. DAMAGE OUT OF LIMITS PER A220 ASRP 57-54-84. WIP 145099 ACCOMPLISHED SECTION 1: TIME-LIMITED REPAIR PER
- [SDR DALA2020122104181](https://openairdocs.org/sdr/DALA2020122104181.md): Engine · contaminated · Dec 19, 2020 · N107DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > WE EXPERIENCED FUMES SMELL IN THE FLIGHT DECK DURING ENGINE START AFTER DEICING. T/S PER A220 JIC 0550-2001. FOUND SOURCE TO BE DEICING FLUID OF NR 2 ENGINE. ACCOMPLISHED ELIMINATION OF ODOR, IAW A220 EFIM SOLUTION 1-9264. ALL NO GO ODI PROCEDURES C/W. NO
- [SDR DALA2020082102835](https://openairdocs.org/sdr/DALA2020082102835.md): Bottle · low pressure · Aug 20, 2020 · N107DU · Bombdr BD1001A10 · Service Doors
  > DURING SERVICE CHECK FOUND RT AFT SERVICE DOOR EOAM BOTTLE LOW. SERVICED EOAM BOTTLE PER A220 AMP BD-500-A-J52-46-08. REQUIRED INSPECTION ITEMS COMPLETED.
- [SDR DALA2020081002741](https://openairdocs.org/sdr/DALA2020081002741.md): Bottle · low pressure · Aug 10, 2020 · N107DU · Bombdr BD1001A10 · Escape Slide
  > DURING ESCAPE SLIDE CHECK W/C 2561-2004. FOUND AFT RT SLIDE PRESSURE IN RED BAND. REMOVED AFT RT SLIDE PER W/C 2563-4006, STEPS 1-8. REQ'S OK TO INSTALL. INSTALLED SLIDE.
- [SDR DALA2020080902740](https://openairdocs.org/sdr/DALA2020080902740.md): Strip · broken · Aug 9, 2020 · N107DU · Bombdr BD1001A10 · Engine (Turbine/Turboprop)
  > DURING W/C 2620-01223-01B, FOUND ENG SIDE TORQUE STRIP BROKEN. C/W CLEANING AND TORQUE PROCEDURES OF HOSE ASSY IAW W/C 2620-01223-01B. NO OTHER DAMAGE. OK FOR SERVICE.
- [SDR DALA2020021801208](https://openairdocs.org/sdr/DALA2020021801208.md): Actuator · low pressure · Feb 14, 2020 · N107DU · Bombdr BD1001A10 · Service Doors
  > AFT SERVICE DOOR (EOAM) ACTUATOR PRESSURE LOW.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:0514-2001/003 00033 SERVICED AFT PASSENGER DOOR EOAM PER C SERIES AMP TASK BD500-A-J52-46-08-01AAA-214A-A. REMOVED EOAM SAFETY PIN FROM EOAM. (LP# 1490069)
- [SDR DALA2019051403020](https://openairdocs.org/sdr/DALA2019051403020.md): Pump · leaking · May 12, 2019 · N107DU · Bombdr BD1001A10 · Hydraulic Pump, Auxiliary
  > ON TAXI IN CREW NOTED VERY STRONG ODOR RESEMBLING ELECTRICAL SOURCE. NO ACTUAL SMOKE OBSERVED. SMELL DISSIPATED AFTER APU STARTED AIRFLOW. ON WALKAROUND FOUND HYD LEAK FROM AFT ACCESSORY COMPARTMENT. FOUND HYD PUMP 3A/3B ECOLOGY BOTTLE OVERFLOWING. FOUND ACMP

## 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 = 'N107DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N107DU/reports

---
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