# Service difficulty reports: N302DU

A list on [N302DU](https://openairdocs.org/aircraft/N302DU.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 · 55 reports

- [SDR DALA2026070904024](https://openairdocs.org/sdr/DALA2026070904024.md): Light · inoperative · Jul 6, 2026 · N302DU · Airbus BD5001A11 · Emergency Lighting
  > AFT RIGHT SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. R & R REAR RT EXTERNAL EMERGENCY EXIT LIGHT IAW AMP 33-55- 02-03AAA-720A-A. OPS CHKD GOOD. MEL AND PLACARD REMOVED. (LP# 8710655; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060903495](https://openairdocs.org/sdr/DALA2026060903495.md): Turbine · damaged · Jun 7, 2026 · N302DU · Airbus BD5001A11 · Turbine Section
  > DIV- DIVERTED TO RDU DUE TO #2 ENGINE HIGH N2 VIBRATION. CARRIED OUT BOROSCOPE INSPECTION ON RT ENGINE. FOUND LPT DAMAGE, REQUIRES ENGINE CHANGE. ENGINE REPLACED. (LP# 8761056, 8761058; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050602889](https://openairdocs.org/sdr/DALA2026050602889.md): Pressure Sensor · failed · May 5, 2026 · N302DU · Airbus BD5001A11 · Airfoil Anti/De-ice System
  > DIVERTED TO DFW DUE TO LEFT WING ANTI-ICE FAIL. REMOVED AND REPLACED OUTBOARD PRESSURE SENSOR. SECURED SENSE LINE OPS AND LEAK CHECK GOOD. (LP# 8477622, 1577317; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026042002484](https://openairdocs.org/sdr/DALA2026042002484.md): Door Frame · corroded · Apr 16, 2026 · N302DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT PASSENGER DOOR SURROUND.FWD FRAME (FR74) HAS 4 FASTENERS HOLES WITH CORROSION.-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/003 00419 COMPLIED WITH ER/A 632912-14 PRI REV 0, REV 1, AND FINAL ER/A 632912-14 REV ORIGINAL. ORIGINAL THI
- [SDR DALA2026042002483](https://openairdocs.org/sdr/DALA2026042002483.md): Door Frame · corroded · Apr 16, 2026 · N302DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT PASSENGER DOOR SURROUND.AFT FRAME (FR76) HAS 13 FASTENERS HOLES WITH CORROSION.-M-PIC. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0583:5300-2005/002 00418 COMPLIED WITH ER/A 632912-14 PRI REV 0, REV 1, AND FINAL ER/A 632912-14 REV ORIGINAL. ORIGINAL TH
- [SDR DALA2026041402356](https://openairdocs.org/sdr/DALA2026041402356.md): Support Fitting · corroded · Apr 12, 2026 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE LAV E SUPPORT FITTING (REF. A220 ASRP 53-61-43-06AAA-041A-A ITEM 24). COMPLIED WITH ER/A 633268-14 PRI REV 0, REV1, REV2 AND FINAL ER/A 633268- 14 REV ORIGINAL. (LP# 1541085)
- [SDR DALA2026041402357](https://openairdocs.org/sdr/DALA2026041402357.md): Skin · corroded · Apr 11, 2026 · N302DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE FRAME 81, JUST FWD OF AFT ACCESSORY COMPARTMENT OPENING, CORROSION FROM CENTER LINE LEFT 18" AROUND DOOR HINGE. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0790:2090-2106/002 00247 REPLACED FRAME 81 LOWER SECTION REF. A220 DWG C01401201 AND A220
- [SDR DALA2026041202312](https://openairdocs.org/sdr/DALA2026041202312.md): Seat Track · corroded · Apr 11, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN-SEAT TRACK LBL43.5 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342701. (LP 1539725 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026041202311](https://openairdocs.org/sdr/DALA2026041202311.md): Seat Track · corroded · Apr 11, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN-SEAT TRACK RBL23 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REMOVED DAMAGED SEAT TRACK AND INSTALLED REPAIR PARTS, COMPLIED WITH ER/A 632950-14 PRI REV 0, REV 1, ERA 623169-14TR REV. A, AND FINAL ER/A 632950-14 REV ORIGINAL, AND ER
- [SDR DALA2026041002298](https://openairdocs.org/sdr/DALA2026041002298.md): Floor Support · corroded · Apr 8, 2026 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > DURING C2 + 6 YEAR (HCK) CHECK IN MSP, MAINTENANCE FOUND CORROSION COMMON TO THE AFT FUSELAGE FLOOR LAV E SUPPORT AT FR79, LBL 23. REMOVED DAMAGED PARTS, TRIMMED AFT TAB OF FLOOW BEAM AT FR 79 PER BD500-A-J51-01-08-01AAA-353A-A, MANUFACTURED AND INSTALLED FL
- [SDR DALA2026040802254](https://openairdocs.org/sdr/DALA2026040802254.md): Seat Track · corroded · Apr 7, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8302, AFT CABIN-SEAT TRACK LBL 23 NEAR LAV MOUNT FR 72 HAS CORROSION. (M) REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. CORRECTIVE ACTION: REMOVED DAMAGED SEAT TRACK, APPLY CORROSION INHIBITING COMPOUND (CIC) IN AND AROUND REWORKED AREAS PER AMP BD50
- [SDR DALA2026040702211](https://openairdocs.org/sdr/DALA2026040702211.md): Floor Support · corroded · Apr 5, 2026 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE FLOOR STRUCTURE AT 2 LOCATIONS BETWEEN FR 76 AND FR 78 JUST AFT OF THE AFT SERVICE DOOR. REMOVED AND INSTALLED WEB PER A220 ASRP 51-42-00. (LP# 1529805)
- [SDR DALA2026040702210](https://openairdocs.org/sdr/DALA2026040702210.md): Floor Support · corroded · Apr 5, 2026 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > WHILE PREPARING FOR CIC IN ZONE 240, CORROSION WAS FOUND ON THE FLOOR STRUCTURE AT 1 LOCATION BETWEEN FR 76 AND FR 78 JUST AFT OF THE AFT PASSENGER DOOR. COMPLIED WITH ERA PRI 633257-14 REV 0,1,2 AND FINAL ERA 633257-14 REV ORIGINAL. (LP# 1530008)
- [SDR DALA2026040702209](https://openairdocs.org/sdr/DALA2026040702209.md): Doubler · corroded · Apr 5, 2026 · N302DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > WASTE BOX DOUBLER HAS CORROSION ON FWD AND AFT FLANGE. REPAIRED PER PRI 632674-14 REV 0 REV 1 AND FINAL ER/A 632674-14. (LP# 1530122)
- [SDR DALA2026040602178](https://openairdocs.org/sdr/DALA2026040602178.md): Seat Track · corroded · Apr 3, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 23 AFT INTERCOSTAL FROM FR 70 TO 71 PILOT HOLES IN NEW SEAT TRACK DO NOT LINE UP WITH INTERCOSTAL HOLES. COMPLIED WITH PRI 633015-14 REV 0 AND SECTION I OF ERA 633015-14 REV ORIGINAL. (LP# 1526968)
- [SDR DALA2026040602174](https://openairdocs.org/sdr/DALA2026040602174.md): Blade · corroded · Apr 1, 2026 · N302DU · Airbus BD5001A11 · Engine Thrust Reverser
  > NR 2 ENGINE, RT THRUST REVERSER V-BLADE HAD NUMEROUS SMALL AREAS OF CORROSION OVER ALL SEGMENTS. COMPLIED WITH PRI 632856 REV 00,01,02 AND SECTION I OF ERA 632856-14 REV ORIGINAL. ORIGINAL MATERIAL THICKNESS -.350. REMAINING MATERIAL THICKNESS-.305. MATERI
- [SDR DALA2026032501996](https://openairdocs.org/sdr/DALA2026032501996.md): Seat Track · corroded · Mar 23, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN-SEAT TRACK RBL43.5 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. NO PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0585:5300-2015/005 00395 SUMMARY - 863539 - CARPENTER,
- [SDR DALA2026032301951](https://openairdocs.org/sdr/DALA2026032301951.md): Seat Track · corroded · Mar 20, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN - SEAT TRACK RBL 43.5 NEAR FR22 AT CLOSET MOUNT HAS CORROSION -M- REF. SSI 53-21-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/007 00393 REMOVED AND REPLACED SEAT TRACK REF A220 ASRP 51-71-00. (LP# 1504
- [SDR DALA2026032301950](https://openairdocs.org/sdr/DALA2026032301950.md): Seat Track · corroded · Mar 20, 2026 · N302DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN - SEAT TRACK RBL 23.0 NEAR FR22 AT CLOSET MOUNT HAS CORROSION -M- REF. SSI 53-21-43-01. NO PREVIOUS REWORK NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0572:5321-2021/006 00392 COMPLETED SPLICE REPAIR REF. ER/A 629030-14TR REV A. (LP# 1504008
- [SDR DALA2026041502389](https://openairdocs.org/sdr/DALA2026041502389.md): Doubler · corroded · Mar 18, 2026 · N302DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > ER/A 632674-14 SECTION I REPAIR WAS ISSUED TO ADDRESS WASTE BOX COMPARTMENT CORROSION TO INTERNAL DOUBLER AND SKIN. FOLLOW ON ACTIONS ARE REQUIRED.ACCOMPLISH SECT. II WITHIN EVERY 1000 FH FROM SECT. I ACCOMPLISHMENT. ACCOMPLISH SECT. III WITHIN 10,000 FH FROM
- [SDR DALA2026031901903](https://openairdocs.org/sdr/DALA2026031901903.md): Seal · damaged · Mar 18, 2026 · N302DU · Airbus BD5001A11 · Leading Edge Slat Control System
  > /H WING- DURING OK TO INSTALL # 2 SLAT FOUND TELESCOPIC DUCT SEAL DAMAGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0006:2781-4002-LH/003 00599 REMOVED AND REPLACED ALL SEALS IN REFERENCE WITH A220 AMP 57-41-07.
- [SDR DALA2025081906215](https://openairdocs.org/sdr/DALA2025081906215.md): Frame · not reported · Aug 14, 2025 · N302DU · Airbus BD5001A11 · Fuselage Main, Frame
  > FRAME REPLACED ON WORKCARD 5352-01038-08A ASSOCIATED AA 5352-01038 ADDED FOR AC 8302. (LP# 7852131)
- [SDR DALA2025081906214](https://openairdocs.org/sdr/DALA2025081906214.md): None · none · Aug 14, 2025 · N302DU · Airbus BD5001A11 · Standard Practices/Structures
  > SDR LOG CREATED PER WORKCARD 5352-01038-07A. MFG P/N C02383111-001 REPLACED ON WORKCARD 5352-01038-07A ASSOCIATED AA 5352-01038 ADDED FOR AC 8302. (LP# 7852130)
- [SDR DALA2025060104200](https://openairdocs.org/sdr/DALA2025060104200.md): Circuit Card · faulted · May 25, 2025 · N302DU · Airbus BD5001A11 · Flight Management Computing Hardware System
  > SHIP 8302 - ATO DUE TO FMS SPEED MESSAGE. CAPTAINS V SPEEDS WERE GRAYED OUT AT THROTTLE UP. RETURNED TO GATE. DEFERRED PER MEL 34-61-01A. LATER: REPLACED FMS 1 CMM IN IPC 1 SLOT 2. OPS TEST GOOD, SOFTWARE OF CCM 1 GOOD. (LP 0986229)
- [SDR DALA2025040802745](https://openairdocs.org/sdr/DALA2025040802745.md): Slat Track · corroded · Apr 2, 2025 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #4 PINION TOOTH (1EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 621466-14AD REV B AND PRI 621466-14AD REV 0 MATCHES. (LP# 0892334)
- [SDR DALA2025040802744](https://openairdocs.org/sdr/DALA2025040802744.md): Slat Track · corroded · Apr 2, 2025 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #4 RACK TOOTH (1 EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 621466-14AD REV B AND PRI 621466-14AD REV 0 MATCHES. (LP# 0892326)
- [SDR DALA2025040802743](https://openairdocs.org/sdr/DALA2025040802743.md): Slat Track · corroded · Apr 2, 2025 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #6 RACK TOOTH (1EA) HAS EVIDENCE OF CORROSION. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 621466-14AD REV B AND PRI 621466-14AD REV 0 MATCHES. (LP# 0892324)
- [SDR DALA2025021901226](https://openairdocs.org/sdr/DALA2025021901226.md): Slide · warning message · Feb 16, 2025 · N302DU · Airbus BD5001A11 · Escape Slide
  > WING SLIDE CAUTION MESSAGE (52 WING SLIDE - R OWEE SLIDE INOP). REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT DOOR SLIDE PER W /C 2563-4005.(D.D 830324) ALL RII TASK COMPLETED A/C OK FOR SVC MEL + PLAC REMOVED (LP# 6949398)
- [SDR DALA2024101510104](https://openairdocs.org/sdr/DALA2024101510104.md): Flange · broken · Oct 11, 2024 · N302DU · Airbus BD5001A11 · Aerodynamic Fairings
  > DURING REMOVAL OF WTBF PANEL 195HB FOUND WTBF LONGERON ASSEMBLY NUT PLATE ATTACHMENT FLANGES BROKEN 2 EA P/N: C02383111-001. INSTALLED WTBF LONGERON ASSEMBLY P/N: C02383111-001 IAW A220 ASRP 51- 42-21 AND AMDS WC 5352-01038-01A ASSOCIATED AA 5352-01038 ADDED F
- [SDR DALA2024082208373](https://openairdocs.org/sdr/DALA2024082208373.md): Control Lever · stiff · Aug 22, 2024 · N302DU · Airbus BD5001A11 · Passenger/Crew Doors
  > FA REPORTS 1 LEFT DOOR ARM/DISARM LEVER IS STIFF AND GETS STUCK BEFORE REACHING FULL DISARM MODE. DURING OPS CHK OF 1L REF 52-11-00, TASK 320A-A ON 3RD ATTEMPT GIRT BAR DID NOT DETACH AND EMERGENCY ESCAPE SLIDE DEPLOYED. REMOVED SLIDE PER AMP 25-63 ASSESSING D
- [SDR DALA2025050103375](https://openairdocs.org/sdr/DALA2025050103375.md): Skin · eroded · Jul 20, 2024 · N302DU · Airbus BD5001A11 · Horizontal Stabilizer, Plate/Skin
  > R/H HORIZONTAL STABILIZER TIP EROSION PROTECTIVE MATERIAL REQUIRES REPAIR. INSPECTED RH HORIZONTAL TIP IN AREA WHERE EROSION TAPE WAS DAMAGE AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF THE EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 AS
- [SDR DALA2024030503038](https://openairdocs.org/sdr/DALA2024030503038.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IN 2 LOCATIONS IAW ER/A 608357-14AD REV B AND PRI 608357-14AD REV 0 MATCHED. (LP# 0224464)
- [SDR DALA2024030503037](https://openairdocs.org/sdr/DALA2024030503037.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 UPPER FWD SURFACE IAW ER/A 608357- 14AD REV B AND PRI 608357-14AD REV 0 MATCHED. (LP# 0224462)
- [SDR DALA2024030503036](https://openairdocs.org/sdr/DALA2024030503036.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 UPPER FWD SURFACE IAW ER/A 608357- 14AD REV B AND PRI 608357-14AD REV 0 MATCHED. (LP# 0224460)
- [SDR DALA2024030503035](https://openairdocs.org/sdr/DALA2024030503035.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 608357- 14AD REV B AND PRI 608357-14AD REV 0 MATCHED. (LP# 0224457)
- [SDR DALA2024030503034](https://openairdocs.org/sdr/DALA2024030503034.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 608357- 14AD REV B AND PRI 608357-14AD REV 0 MATCHED. (LP# 0224446)
- [SDR DALA2024030503033](https://openairdocs.org/sdr/DALA2024030503033.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 UPPER AFT OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 UPPER AFT OB SIDE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224324)
- [SDR DALA2024030503032](https://openairdocs.org/sdr/DALA2024030503032.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER FWD OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LOWER FWD OB SIDE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224322)
- [SDR DALA2024030503031](https://openairdocs.org/sdr/DALA2024030503031.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224321)
- [SDR DALA2024030503030](https://openairdocs.org/sdr/DALA2024030503030.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 LOWER AFT SURFACE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224320)
- [SDR DALA2024030503029](https://openairdocs.org/sdr/DALA2024030503029.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 LOWER AFT SURFACE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224319)
- [SDR DALA2024030503028](https://openairdocs.org/sdr/DALA2024030503028.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IN 2 LOCATIONS IAW ER/A 608356-14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224315)
- [SDR DALA2024030503027](https://openairdocs.org/sdr/DALA2024030503027.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE IN 2 LOCATIONS IAW ER/A 608356-14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224314)
- [SDR DALA2024030503026](https://openairdocs.org/sdr/DALA2024030503026.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224311)
- [SDR DALA2024030503025](https://openairdocs.org/sdr/DALA2024030503025.md): Slat Track · corroded · Feb 29, 2024 · N302DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 608356- 14AD REV C AND PRI 608356-14AD REV 0 MATCHED. (LP# 0224307)
- [SDR DALA2023091407549](https://openairdocs.org/sdr/DALA2023091407549.md): Unknown · unknown · Sep 9, 2023 · N302DU · Airbus BD5001A11 · Service Doors
  > R1 DOOR HAS DENT. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 128-0002:0500-2004/002 00314 REPAIRED PER PRI 610830-14 REV 0, REV 1 AND FINAL ER/A 610830-14 REV A. (LP# 2961513)
- [SDR DALA2023090807370](https://openairdocs.org/sdr/DALA2023090807370.md): Unknown · unknown · Sep 7, 2023 · N302DU · Airbus BD5001A11 · Standard Practices/Structures
  > ER/A 610830-14 REV A ISSUED FOR SECTION IV PERMANENT REPAIR ACCOMPLISHMENT. FOLLOW ON ACTION (DTE) IS REQUIRED. DTE IS REQUIRED. ER/A 610830-14 REV A SECTION IV APPROVAL IS LIMITED TO 12 MONTHS. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED
- [SDR DALA2023081506635](https://openairdocs.org/sdr/DALA2023081506635.md): Unknown · unknown · Aug 10, 2023 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT DOOR SCUFF PLATE, INSIDE AFT POCKET AREA HAS 2 EA. FASTENER HOLES WITH EVIDENCE OF CORROSION. 'M'. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0234:5321-2015/001 00230 CMOR - COMPLIED WITH
- [SDR DALA2024041304395](https://openairdocs.org/sdr/DALA2024041304395.md): Scuff Plate · corroded · Aug 9, 2023 · N302DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8302, DURING C CHECK IN MSP MTC REPORTED CORROSION UNDER THE SCUFF PLATES SILL, POST BLENDING THE MINIMUM REPORTED THICKNESS WAS LOWER THAN REQUIRED. CORRECTIVE ACTION: TRIM AFT TAB OF NEW SILL (P/N: C02313004007 REF) AT FR29 PER ASRP 51-24-36 AS SHOW
- [SDR DALA2023050903641](https://openairdocs.org/sdr/DALA2023050903641.md): Unknown · unknown · May 5, 2023 · N302DU · Airbus BD5001A11 · Doors
  > SHIP 8302 - ATB - DUE TO AFT CARGO DOOR CAUTION MESSAGE. CORRECTIVE ACTION: FOUND DOOR HANDLE RED FLAG DISPLAYED. CYCLED MULTIPLE TIMES DOOR HANDLE REMAINED FLUSH AND GREEN FLAG DISPLAYED. LIGHTLY PULLED UP ON HANDLE SEVERAL TIMES WITH DOOR FULLY CLOSED AND HA

Next page: https://openairdocs.org/aircraft/N302DU/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 = 'N302DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N302DU/reports

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