# Service difficulty reports: N305DU

A list on [N305DU](https://openairdocs.org/aircraft/N305DU.md).

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

- [SDR DALA2026061103538](https://openairdocs.org/sdr/DALA2026061103538.md): Door Frame · damaged · Jun 8, 2026 · N305DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT SERVICE DOOR FR74 DURING DVI INSPECTION HOLE #9 PER ER/A 634028-14 FOUND HOLE #9 OUT OF ROUND FR76. FOR ADDITIONAL INFORMATION 001-0584:5300-2008/010 00579 COMPLIED WITH PRI 634028-14 REV'S 0, 1, 2, 3. (LP# 1635529; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061003516](https://openairdocs.org/sdr/DALA2026061003516.md): Insert · corroded · Jun 6, 2026 · N305DU · Airbus BD5001A11 · Passenger/Crew Doors
  > AFT PAX DOOR SURROUND PANEL ATTACH NUT INSERTS HAVE LIGHT CORROSION AT FR76. COMPLIED WITH ERA 634027-14 PRI REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, REV 7, AND FINAL ER/A 634027-14 REV ORIGINAL. ORIGINAL THICKNESS 0.165", MAX MATERIAL REMOVED 0.021"
- [SDR DALA2026061003515](https://openairdocs.org/sdr/DALA2026061003515.md): Insert · corroded · Jun 6, 2026 · N305DU · Airbus BD5001A11 · Passenger/Crew Doors
  > AFT PASSENGER DOOR SURROUND ATTACH NUT INSERTS 8EA AT FR74 HAVE LIGHT CORROSION. COMPLIED WITH ERA 634027-14 PRI REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV 6, REV 7, AND FINAL ER/A 634027-14 REV ORIGINAL. ORIGINAL THICKNESS 0.165", MAX MATERIAL REMOVED 0.0
- [SDR DALA2026060903494](https://openairdocs.org/sdr/DALA2026060903494.md): Skin · corroded · Jun 5, 2026 · N305DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > DURING C2 + 6 YEAR (HEAVY) CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING THE EO 5331-01297-01C WORKCARD / SB BD500-530010 MODIFICATION WHEN CORROSION WAS FOUND COMMON TO THE FUSELAGE LOWER AND BOTTOM SKIN PANELS AT THE FWD CARGO DOOR CUTOUT. COMPLIED WITH ER/A 6
- [SDR DALA2026060903493](https://openairdocs.org/sdr/DALA2026060903493.md): Door Frame · corroded · Jun 5, 2026 · N305DU · Airbus BD5001A11 · Fuselage Main, Structure
  > DURING HEAVY CHECK IN MSP, MAINTENANCE FOUND CORROSION COMMON TO THE FWD SERVICE DOOR SURROUND FRAMES. FR 17 P/N C02316001-011 AND FR 20 P/N C02316003-011 ARE AFFECTED. COMPLIED WITH ER/A 634015-14 PRI REV 0, ER/A 634015-14 PRI REV 1, ER/A 634015-14 PRI REV 2
- [SDR DALA2026060903492](https://openairdocs.org/sdr/DALA2026060903492.md): Skin · corroded · Jun 5, 2026 · N305DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > DURING C2 + 6Y ( H) CHECK IN MSP, DAL FOUND CORROSION LOCALIZED AROUND THE SKIN SCUFF PLATE ATTACH HOLES PREVIOUSLY REPAIRED VIA REO 500-53-21-651. MTC REQUIRES ENGINEERING AUTHORITY TO ACCOMPLISH EO WORKCARD 533101297-01B (SB BD500-530010 ISSUE 004 PART B) O
- [SDR DALA2026060403392](https://openairdocs.org/sdr/DALA2026060403392.md): Fairing · corroded · Jun 2, 2026 · N305DU · Airbus BD5001A11 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON AFT FIXED FAIRING HAS CORROSION IN MULTIPLE FASTENER HOLES AND PITTING ON THE STRUCTURE. COMPLIED WITH ER/A 633933-14 PRI REV 0, 1 AND ER/A 633933-14 REV ORIGINAL, SECTION 1; PERMANENT REPAIR. (LP# 1626425; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060403391](https://openairdocs.org/sdr/DALA2026060403391.md): Bearing · damaged · Jun 2, 2026 · N305DU · Airbus BD5001A11 · Nacelle/Pylon, Attach Fittings
  > BEARINGS FOUND DAMAGED ON PYLON SIDE LINK UPPER ATTACHMENT FITTING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH ERA 634589-14, PRI REV 0, 01, 02 AND ERA 634589-14, SECTION 1: PERMANENT REPAIR REV ORIGINAL. (LP# 1626312; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060403390](https://openairdocs.org/sdr/DALA2026060403390.md): Seat Track · corroded · Jun 2, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 43.5 NEAR FR74 AT AFT END HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH ERA 634276-14 PRI REV 0 AND E RA 634276-14 SECTION I PERMANENT REPAIR REV ORIGINAL. (LP# 1626070; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060303374](https://openairdocs.org/sdr/DALA2026060303374.md): Bearing · damaged · May 31, 2026 · N305DU · Airbus BD5001A11 · Nacelle/Pylon, Main Frame
  > SPHERICAL BEARINGS FOUND DAMAGED ON PYLON SIDE LINK LOWER ATTACHMENT FITTING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0678:5451-2007-RH/010 00710 COMPLIED WITH ERA 634593-14 PRI REV 0, 1, 2, AND ERA 634593-14 S
- [SDR DALA2026060403393](https://openairdocs.org/sdr/DALA2026060403393.md): Thrust Reverser · corroded · May 21, 2026 · N305DU · Airbus BD5001A11 · Engine Thrust Reverser
  > DURING H CHK IN MSP, CORROSION AND/OR MISSING COATING WAS FOUND ON THE #2 ENG, INBD THRUST REVERSER (P/N 999-3001577 WITH FTN 5T0778) TORQUE BOX V-BLADE AT THE UPPER TO LOWER V-BLADE SEGMENTS. DAMAGE EXCEEDS CMM GRAPW1500BA-A-54-30-22-00001-661A-D ALLOWABLE DA
- [SDR DALA2026052003096](https://openairdocs.org/sdr/DALA2026052003096.md): Skin · corroded · May 20, 2026 · N305DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION FOUND ON THE EXTERNAL FUSELAGE SKIN SURFACE NEAR FR 35 AND STGR 1R AND 1L. BLENDED SKIN PER ER/A 634142-14 PRI REV 0,1,2 AND REV ORIGINAL MIN REMAINING THICKNESS WAS.060. (LP 1602651 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051803053](https://openairdocs.org/sdr/DALA2026051803053.md): Seat Track · corroded · May 16, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION. SEAT TRACK RBL 23.0 NEAR FR74 AT AFT END HAS CORRISION. CORRECTIVE ACTION: REPLACED SEAT TRACK REF A220 AS PER RP BD500-A-J51-77-00-00AAA-028A-A. (LP 1597187 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051803052](https://openairdocs.org/sdr/DALA2026051803052.md): Brake · no test · May 16, 2026 · N305DU · Airbus BD5001A11 · Stabilizer Control System
  > HORIZONTAL STAB BRAKE FAILED FUNCTION TEST. REPLACED HORIZONTAL STAB BRAKE AND PERFORMED FUNCTION CHECK PER AMP 27-41-01. (LP 1596950 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302994](https://openairdocs.org/sdr/DALA2026051302994.md): Seat Track · corroded · May 9, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 43.5 NEAR FR22 AT FRONT END HAS CORROSION -P- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/003 00387 REPAIRED PER ER/A 623174-14TR REV A SECTION I. (LP# 1584895; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302993](https://openairdocs.org/sdr/DALA2026051302993.md): Seat Track · corroded · May 9, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 23.0 NEAR FR22 AT FRONT END HAS CORROSION -P- SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/002 00386 REMOVED AND REPLACED PER SEAT TRACK A220 ASRP BD500-A-J51 -77-00-00AAA-028A-A. (LP# 1584888; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051302992](https://openairdocs.org/sdr/DALA2026051302992.md): Seat Track · corroded · May 9, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE- FWD END OF THE SEAT TRACK AT LBL43.5, FR22 IS CORRODED. "M" SEE PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0573:5321-2022/004 00424 CMOR REMOVED AND REPLACED PER SEAT TRACK A220 ASRP BD500- A-J51-77-00-00AAA-028A-A. (LP# 1584546;
- [SDR DALA2026051302991](https://openairdocs.org/sdr/DALA2026051302991.md): Seat Track · corroded · May 9, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT 23LBL AT FR 74 HAS CORROSION. REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2015/001 00516 REMOVED AND REPLACED PER SEAT TRACK A220 ASRP BD500-A-J51 -77-00-00AAA-028A-A. (LP# 1584973; AIRCR
- [SDR DALA2026051302990](https://openairdocs.org/sdr/DALA2026051302990.md): Seat Track · corroded · May 9, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL43 AT FR 74 HAS CORROSION. REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2015/002 00517 REMOVED AND REPLACED IAW ASRP BD500-A-J51 -77-00-00AAA-028A-A. (LP# 1584887; AIRCRAFT WAS GROUNDE
- [SDR DALA2026050602885](https://openairdocs.org/sdr/DALA2026050602885.md): Threshold · not reported · May 3, 2026 · N305DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > PERFORMED AN OPPORTUNITY INSPECTION OF FWD AND AFT SERVICE AND PASSENGER DOOR THRESHOLD PANELS AND SURROUNDING STRUCTURE IAW AMP 05-40-00. SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/006 00390, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050402800](https://openairdocs.org/sdr/DALA2026050402800.md): Longeron · cracked · Apr 30, 2026 · N305DU · Airbus BD5001A11 · Aerodynamic Fairings
  > WING TO BODY FAIRING LONGERON FOUND CRACKED. REPLACED WTBF LONGERON IAW ASRP 53-82-55 AND A220 ASRP 51- 42-21. (LP# 1570816; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051403013](https://openairdocs.org/sdr/DALA2026051403013.md): Attach Fitting · corroded · Apr 27, 2026 · N305DU · Airbus BD5001A11 · Fuselage, Equipment Attach Fittings
  > AFT RT GALLEY-AFT RT FLOOR ATTACH POINT CORRODED 8" FORWARD OF FR 79. REF SSI 53-61-43-02. NO REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0586:5300-2016/003 00526 REMOVED AND REPLACED FITTING, REF AIRBUS 220 DRAWING C01349710, AND A220 ASRP 51-
- [SDR DALA2026042802691](https://openairdocs.org/sdr/DALA2026042802691.md): Slide · no test · Apr 25, 2026 · N305DU · Airbus BD5001A11 · Escape Slide
  > RIGHT OVERWING SLIDE MECHANISM FAILED STEP 6C OF AMDS 5221-2001-02. (EXTERNAL SLIDE DEPLOYMENT MECHANISM ARM DID NOT RETURN TO NORMAL POSITION AFTER OWEED DOOR WAS CLOSED). CLEANED REF. A220 AMP 20-00-01. VERIFIED OPERATION ON AMDS 5221-2001-02. OPS CHECK GOO
- [SDR DALA2026030401496](https://openairdocs.org/sdr/DALA2026030401496.md): Lens · missing · Feb 25, 2026 · N305DU · Airbus BD5001A11 · Emergency Lighting
  > R1 DOOR OVERHEAD EMERGENCY LIGHT LENS MISSING. APPLIED ER/A 632694-14 REV. ORIG. SECTION 1: TIME LIMITED REPAIR. TEMPORARY LENS INSTALLED. PERMANENT RESTORATION IS REQUIRED PER THIS ER/A WITHIN 10 DAYS FROM FLIGHT 2108 IN ORD ON 24FEB26. PERFORMED PERM REP
- [SDR DALA2025121009038](https://openairdocs.org/sdr/DALA2025121009038.md): Landing Gear · faulted · Dec 7, 2025 · N305DU · Airbus BD5001A11 · Landing Gear Retraction/Extension System
  > ATB - DUE TO LOUD BANG AND "GEAR DISAGREE" AND "WOW FAIL" MESSAGES. SWITCHED TO SECONDARY NOSE LANDING GEAR STRUT SEALS, PERFORMED GEAR SWING TEST. OK FOR SERVICE. (LP# 7889415)
- [SDR DALA2025091506775](https://openairdocs.org/sdr/DALA2025091506775.md): Wire Harness · shorted · Aug 31, 2025 · N305DU · Airbus BD5001A11 · Electrical Power System Wiring
  > AFTER LEFT ENGINE START, ELECTRICAL FAULT LT FBW PC PMG INOPERATIVE. T/S IAW EFIM, FAULT CODE 2401F3249, RELAY PREVIOUSLY CHANGED, WIRING CHECK FOR PINS X1 & X2 AT K17 RELAY OK, WIRING CHECK FROM A276P1 PIN 1 TO 38 SHOWS 28 VDC. R & R CDC1 LRM09 IAW AMP 24-
- [SDR DALA2025042403239](https://openairdocs.org/sdr/DALA2025042403239.md): Unknown · odor · Apr 18, 2025 · N305DU · Airbus BD5001A11 · Air Distribution System
  > ON SHUTDOWN ELECTRICAL ODOR IN FORWARD GALLEY AND FLIGHT DECK. T/S PER AMDS WORKCARD 0550-2001. NO TROUBLE FOUND.NO. FUMES COULD BE FELT. NO RESIDUAL ODORS NOTED. IN ADDITION COMPLETED AMDS WORKCARD 0550-9001-A220.OK FOR SVC. (LP# 7001441)
- [SDR DALA2024092609469](https://openairdocs.org/sdr/DALA2024092609469.md): Switch · malfunctioned · Sep 25, 2024 · N305DU · Airbus BD5001A11 · Emergency Lighting
  > AIRCRAFT 8305, EMER LIGHTS ON STATUS MSG DURING FLIGHT. EMER LIGHTS BATT FAULT MSG ON CMC. CORRECTIVE ACTION: CYCLED EMERGENCY LIGHT POWER SWITCH IAW A220 AMP 33-52. NO FAULTS INDICATED. OPS CHK NORMAL.
- [SDR DALA2024080707861](https://openairdocs.org/sdr/DALA2024080707861.md): Engine · odor · Aug 4, 2024 · N305DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)
  > ON GROUND (BEFORE TAKEOFF) FOUL SMELL THROUGH OUT CABIN AND COCKPIT. FA CREWS SAID THEY HAD THE SAME ODOR DURING THEIR LAST LEG OUT OF MSO. SAID THEY HAD MAINTENANCE IN MSO LOOK AT THE ISSUE-- THEY COULD NOT FIND A CAUSE OF THE ODOR. LEAD FA TOLD ME ABOUT THE
- [SDR DALA2024022102404](https://openairdocs.org/sdr/DALA2024022102404.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. MEASURED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 611232- 14AD REV B AND PRI 611232-14AD REV 0 MATCHED. (LP# 0206674)
- [SDR DALA2024022102403](https://openairdocs.org/sdr/DALA2024022102403.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 611232- 14AD REV B AND PRI 611232-14AD REV 0 MATCHED. (LP# 0206669)
- [SDR DALA2024022102402](https://openairdocs.org/sdr/DALA2024022102402.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 611232- 14AD REV B AND PRI 611232-14AD REV 0 MATCHED. (LP# 0206666)
- [SDR DALA2024022102401](https://openairdocs.org/sdr/DALA2024022102401.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 UPPER AFT IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 UPPER AFT IB SIDE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206665)
- [SDR DALA2024022102400](https://openairdocs.org/sdr/DALA2024022102400.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206662)
- [SDR DALA2024022102399](https://openairdocs.org/sdr/DALA2024022102399.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER FWD IB SIDE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206660)
- [SDR DALA2024022102398](https://openairdocs.org/sdr/DALA2024022102398.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN TWO LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IN TWO LOCATIONS IAW ER/A 611232-14AD REV B AND PRI 611232-14AD REV 0 MATCHED. (LP# 02066
- [SDR DALA2024022102397](https://openairdocs.org/sdr/DALA2024022102397.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206658)
- [SDR DALA2024022102396](https://openairdocs.org/sdr/DALA2024022102396.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206656)
- [SDR DALA2024022102395](https://openairdocs.org/sdr/DALA2024022102395.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206655)
- [SDR DALA2024022102394](https://openairdocs.org/sdr/DALA2024022102394.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 611441- 14AD REV A AND PRI 611441-14AD REV 0 MATCHED. (LP# 0206654)
- [SDR DALA2024022102393](https://openairdocs.org/sdr/DALA2024022102393.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206652)
- [SDR DALA2024022102392](https://openairdocs.org/sdr/DALA2024022102392.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206650)
- [SDR DALA2024022102391](https://openairdocs.org/sdr/DALA2024022102391.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206648)
- [SDR DALA2024022102390](https://openairdocs.org/sdr/DALA2024022102390.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206642)
- [SDR DALA2024022102389](https://openairdocs.org/sdr/DALA2024022102389.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206639)
- [SDR DALA2024022102388](https://openairdocs.org/sdr/DALA2024022102388.md): Slat Track · corroded · Feb 18, 2024 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 611233- 14AD REV B AND PRI 611233-14AD REV 0 MATCHED. (LP# 0206632)
- [SDR DALA2023091907710](https://openairdocs.org/sdr/DALA2023091907710.md): Unknown · unknown · Sep 9, 2023 · N305DU · Airbus BD5001A11 · Fuel Storage
  > SHIP 8305 - ATB - DUE TO FUEL IMBALANCE. CORRECTIVE ACTION: R/R RT WING TRANSFER FLOAT VALVE. (LP# 4035978)
- [SDR DALA2023081506639](https://openairdocs.org/sdr/DALA2023081506639.md): Unknown · unknown · Aug 14, 2023 · N305DU · Airbus BD5001A11 · Leading Edge Devices
  > LH WING SLAT TRACK 4 DAMAGED, ON INBD UPPER FWD, LOWER AFT, LOWER OUTBD FWD. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:5742-01028-02A/001 00003 REMOVED AND REPLACED TRACK ASSY 4, REF A220 AMP 27-81-17. OPS A
- [SDR DALA2023042603268](https://openairdocs.org/sdr/DALA2023042603268.md): Unknown · unknown · Apr 22, 2023 · N305DU · Airbus BD5001A11 · Cabin Temperature Control System
  > R PACK OVHT CAUTION MSG FOLLOWED BY L PACK OVHT MSG ON TAXI COMPLIED WITH ABNORMAL CHECKLISTS. REFERENCE LOG 4748840 AND 2730343 FOR CORRECTIVE ACTION. OK FOR SVC. (LP# 4748842)
- [SDR DALA2022092906398](https://openairdocs.org/sdr/DALA2022092906398.md): None · none · Sep 25, 2022 · N305DU · Airbus BD5001A11 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 8305 - ATB - DUE TO NUMBER 2 HYDRAULIC QTY ZERO AND HYDRAULIC PRESSURE LOW. ATC DECLARED EMERGENCY FOR THE FLIGHT. CORRECTIVE ACTION: TIGHTENED PYLON HYDRAULIC CONNECTION FITTING AND REPLACED THE NUMBER 2 ENGINE DRIVEN PUMP. (LP# 9160248)

## 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 = 'N305DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N305DU/reports

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