# Service difficulty reports: N120DU

A list on [N120DU](https://openairdocs.org/aircraft/N120DU.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 · 61 reports

- [SDR DALA2026080704581](https://openairdocs.org/sdr/DALA2026080704581.md): Pressure Sensor · faulted · Aug 7, 2026 · N120DU · Airbus BD5001A10 · Engine RPM Indicating System
  > DIVERTED TO DTW DUE TO RIGHT ENGINE FAULT WITH ASSOCIATED N1 ERRATIC AND N1 DROP. REPLACED BURNER PRESSURE SENSOR PER A220 AMP 73-21-23. REPLACED HARNESS W04 PER A220 AMP 73-21-64. REPLACED EEC PER A220 AMP 73-21-01. (LP 8423746 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026041002300](https://openairdocs.org/sdr/DALA2026041002300.md): Light · inoperative · Apr 9, 2026 · N120DU · Airbus BD5001A10 · Emergency Lighting
  > AIRCRAFT 8120, DURING SVC CHK FOUND DOOR 2R EXTERNAL EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER A220 AMP 33-55. OPS CHK GOOD. (LP 7602175 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026041002299](https://openairdocs.org/sdr/DALA2026041002299.md): Light · inoperative · Apr 9, 2026 · N120DU · Airbus BD5001A10 · Emergency Lighting
  > AIRCRAFT 8120, DURING SVC CHK FOUND BOTH LIGHT OVERWING EMERGENCY LIGHTS INOP. REPLACED BOTH LT OVER WING EXT EMER LIGHT ASSY PER A220 AMP 33-55. (LP 7602174 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026033102109](https://openairdocs.org/sdr/DALA2026033102109.md): Skin · gouged · Mar 31, 2026 · N120DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > TWO EACH DENTS WITH GOUGE AND PUNCTURE BETWEEN FR7 AND FR 8 R/H SIDE FUSELAGE SKIN. PERFORMED REPAIR IAW PRI 633376-14 REV 0, 1 AND 2. ALL STEPS COMPLIED WITH. WAITING ON FINAL ERA, (448268). RECEIVED FINAL ER /A APPROVAL FROM ENGINEERING. O.K. FOR SERVICE. (L
- [SDR DALA2025123009514](https://openairdocs.org/sdr/DALA2025123009514.md): Tire · blown · Dec 30, 2025 · N120DU · Airbus BD5001A10 · Tire
  > MAINTENANCE DISCOVERED THE LEFT OUTBOARD MAIN LANDING GEAR TIRE BLOWN. DEBRIS WAS RECOVERED ON THE RUNWAY BY AIRPORT OPERATIONS. REPLACED BOTH LEFT MAIN LANDING GEAR TIRE AND WHEEL ASSEMBLIES, AND THE LEFT INBOARD BRAKE ASSEMBLY. (LP 7692450)
- [SDR DALA2025121209103](https://openairdocs.org/sdr/DALA2025121209103.md): Oil System · overserviced · Dec 10, 2025 · N120DU · Airbus BD5001A10 · Turbine Engine Oil System
  > A/C 8120 -FUMES- CREW REPORTED DIRTY SOCK SMELL AND DONNED O2 MASKS. EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MTC FOUND RT ENGINE OVERSERVICED. (LP# 7932476)
- [SDR DALA2025101407518](https://openairdocs.org/sdr/DALA2025101407518.md): Tire · failed · Oct 8, 2025 · N120DU · Airbus BD5001A10 · Tire
  > LEFT BRAKE FAIL CAUTION AFTER LANDING. LT BRAKE FAIL, LT WHEEL SPEED INOPERATIVE. RAMP REPORTED LT TIRE, INBD TIRE BLOWN OUT. DUE TO NR 2 TIRE FAILURE. REPLACED NR 1 AND 2 MAIN WHEEL ASSEMBLY PER AMP 32-41. R & R NR 1 MLG AXLE INTERFACE MODULE/WHEEL SPEED
- [SDR DALA2025100207163](https://openairdocs.org/sdr/DALA2025100207163.md): Unknown · odor · Sep 26, 2025 · N120DU · Airbus BD5001A10 · Air Distribution System
  > STRONG ELECTRICAL ODOR IN FLIGHT DECK AND CABIN AFTER LANDING. PERFORMED WC 0550-2001. PARTICLE READING DOUBLED WITH APU BLEED ON, AND ENGINES RUNNING WITH FAINT DUSTY SMELL. INSPECTED APU COMPARTMENT AND APU INLET WITH NO FINDINGS. C/W WORK CARD 0550-2003,
- [SDR DALA2025062404711](https://openairdocs.org/sdr/DALA2025062404711.md): Seat Track · corroded · Jun 18, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK RIGHT INBOARD @ LOCATION FR72 HAS CORROSION. REMOVED AND REPLACED AFT SEAT TRACK RH INBD CABIN FLOOR STRUCTURE FR 72 IAW A220 ASRP BD500-A-J51-42-06-00AAA-0784-A. (LP# 1031363)
- [SDR DALA2025062404710](https://openairdocs.org/sdr/DALA2025062404710.md): Seat Track · corroded · Jun 18, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK LEFT OUTBOARD @ LOCATION FR72 HAS CORROSION. REMOVED CORROSION IAW J51-21-06 ( A220 ASRP) NEW SEAT TRACK WAS INSTALLED IAW A220 ASRP BD500-J51-42-21-00AAA-078-A. (LP# 1031350)
- [SDR DALA2025061704571](https://openairdocs.org/sdr/DALA2025061704571.md): Seat Track · corroded · Jun 13, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK LEFT INBOARD @ LOCATION FR72 HAS CORROSION. REMOVED AND REPLACED AFT SEAT TRACK AT AFT CABIN FLOOR STRUCTURE FR72 IAW A220 ASRP BD500-A-J51-42-06-00AAA-0784-A. (LP# 1022356)
- [SDR DALA2025061304496](https://openairdocs.org/sdr/DALA2025061304496.md): Cable · misrigged · Jun 10, 2025 · N120DU · Airbus BD5001A10 · Escape Slide
  > L/H OWEED ARMING/DISARMING MECHANISM IS STUCK. PERFORMED RIGGING OF OWEED ESCAPE SLIDE CABLES LH SIDE IAW A220- 100 AMP J52-21-17-01AAA-275A-A AND ADJUSTED ESCAPE SLIDE MODE SELECT MECHANISM OWEED LH SIDE IAW A220-100 AMP J52-21-17-03AAA- 271A-A. (LP# 1016113)
- [SDR DALA2025060904385](https://openairdocs.org/sdr/DALA2025060904385.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR UPPER SCUFF PLATE FASTENER HOLES 130U AND 200U HAVE CORROSION. FWD CARGO DOOR UPPER SCUFF PLATE FASTENER HOLES 130U AND 200U HAVE CORROSION. (LP# 1005664)
- [SDR DALA2025060904384](https://openairdocs.org/sdr/DALA2025060904384.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT PAX DOOR (L2) SCUFF PLATE FASTENER HOLES 90L AND 80L CORROSION. REMOVED CORROSION AND EVALUATED DAMAGED AREA OF AFT PAX DOOR LWR SKIN CUTOUT, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06 AND J53-61-01. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW DELTA ERA
- [SDR DALA2025060904383](https://openairdocs.org/sdr/DALA2025060904383.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT SERVICE DOOR (R2) SCUFF PLATE FASTENER HOLES 110L - 140L HAVE CORROSION. REMOVED CORROSION AND EVALUATED DAMAGED AREA ON AFT SERVICE DOOR SKIN CUTOUT, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06 AND J53-61-01. RESTORED FINISH, ALL WORK ACCOMPLISHED IAW DEL
- [SDR DALA2025060904382](https://openairdocs.org/sdr/DALA2025060904382.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLES 20L, 30L, 50L, 80L, 90L, AND 110L HAVE CORROSION. REMOVED CORROSION AND EVALUATED DAMAGED AREA ON AFT CARGO DOOR LWR SKIN CUT-OUT, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-01. RESTORED FINISH AND ACCOM
- [SDR DALA2025060904381](https://openairdocs.org/sdr/DALA2025060904381.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD PAX DOOR (L1) SCUFF PLATE FASTENER HOLES 40L, 70L, 80L, 90L, 100L, AND 110L HAVE CORROSION. REMOVED CORROSION AND EVALUATED DAMAGED AREA ON FWD PAX DOOR LWR SKIN CUT-OUT, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53- 21-01. RESTORED FINISH AND ACCOMPLI
- [SDR DALA2025060904380](https://openairdocs.org/sdr/DALA2025060904380.md): Scuff Plate · corroded · Jun 4, 2025 · N120DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR, LOWER SCUFF PLATE, CORROSION FOUND AT FASTENER HOLES 120-220 (ALL LOWER SCUFF PLATE FASTENER HOLES). REMOVED CORROSION AND EVALUATED DAMAGED AREA ON FWD CARGO DOOR LWR SKIN CUT-OUT, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-25. RESTOR
- [SDR DALA2025052704040](https://openairdocs.org/sdr/DALA2025052704040.md): Seat Track · corroded · May 21, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RIGHT INBOARD @ LOCATION FR20 HAS CORROSION. REMOVED CORROSION, REMOVED AND REPLACED FWD SEAT TRACK RH INBOARD. FR 20 IAW A220-100 ASRP BD500-A-J51-42-21-AAA-0780 JOB COMPLETED. AND 151-42-21-00AAA. (LP# 0978246)
- [SDR DALA2025051503773](https://openairdocs.org/sdr/DALA2025051503773.md): Seat Track · corroded · May 14, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK LEFT INBOARD @ LOCATION FR22 HAS CORROSION. REMOVED AND REPLACED NEW SEAT TRACK AT FWD L/H I/B FR22 IAW A220 ASRP 51-42-21,51-40-11, JOB COMPLETED. (LP# 0966229)
- [SDR DALA2025051503772](https://openairdocs.org/sdr/DALA2025051503772.md): Seat Track · corroded · May 14, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RIGHT OUTBOARD @ LOCATION FR20 HAS CORROSION. REMOVED AND REPLACED NEW SEAT TRACK AT RH O/B FR 20. IAW A220 ASRP 51-42-21, 51-21-06, 51-40-00. JOB COMPLETED. (LP# 0964868)
- [SDR DALA2025051503771](https://openairdocs.org/sdr/DALA2025051503771.md): Seat Track · corroded · May 13, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK LEFT OUTBOARD @ LOCATION FR22 HAS CORROSION. CORROSION REMOVED AND FOUND OUR LIMITS. REMOVED AND REPLACED SEAT TRACK AT FWD CABIN FLOOR STRUCTURE FT 22 I.AW A 220 ASRP BD 500-A-150-42-21-00 AAA-2. (LP# 0964580)
- [SDR DALA2025050603473](https://openairdocs.org/sdr/DALA2025050603473.md): Seat Track · corroded · May 2, 2025 · N120DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK RIGHT OUTBOARD @ LOCATION FR72 HAS CORROSION. REMOVED AND REPLACED AFT SEAT TRACK AT AFT CABIN FLOOR STRUCTURE FR 61R TO FR 74R I.A.W A220 ASRP BD500-4-J51-42-06-00AAA-0784-4. (LP# 0945036)
- [SDR DALA2025040302526](https://openairdocs.org/sdr/DALA2025040302526.md): B-Nut · loose · Apr 2, 2025 · N120DU · Airbus BD5001A10 · Hydraulic System, Main
  > SHIP 8120 - DIV - CREW REPORTED HYDRAULIC ISSUE AND DIVERTED TO JFK. DID DECLARE AN EMERGENCY. LANDED SAFELY AND MTC ADDRESSING. CORRECTIVE ACTION: FOUND B-NUT LOOSE TO PRESSURE FILTER MODULE. TIGHTENED SAME. REMOVED AND REPLACED #2 EDP. OPS CHK OK. A/C RETURN
- [SDR DALA2025031802038](https://openairdocs.org/sdr/DALA2025031802038.md): Frame · broken · Mar 14, 2025 · N120DU · Airbus BD5001A10 · Fuselage Main, Frame
  > FOUND FRAME ASSEMBLY, WTBF PN: C02383117-001 BROKEN. REMOVED AND REPLACE FRAME ASSEMBLY, WTBF PN: C02383117-001 IAW CARD 5352-01038-08A AND DWG C02383100 REV. B. (LP# 0856973)
- [SDR DALA2025031802037](https://openairdocs.org/sdr/DALA2025031802037.md): Longeron · broken · Mar 14, 2025 · N120DU · Airbus BD5001A10 · Fuselage Main, Structure
  > FOUND 1 EA LONGERON ASSEMBLY PN: C02383111-01 BROKEN. REMOVED AND REPLACED 1 EA LONGERON ASSEMBLY PN: C02383111-001 IAW CARD 5352-01038-07A AND DWG C02383100 REV. B. (LP# 0856971)
- [SDR DALA2025013100765](https://openairdocs.org/sdr/DALA2025013100765.md): Light · sparks · Jan 25, 2025 · N120DU · Airbus BD5001A10 · Flight Compartment Lighting
  > CAPT MAP LIGHT SPARKED AND CAUSED A CB TRIP. R/R CAPT MAP LIGHT PER A220 AMP 33-13. OPS TEST GOOD. NO "M" PROCEDURES. MEL & PLACARD REMOVED. (LP# 6385254)
- [SDR DALA2025012400603](https://openairdocs.org/sdr/DALA2025012400603.md): Reu · faulted · Jan 23, 2025 · N120DU · Airbus BD5001A10 · Rudder Control System
  > SHIP 8120 - DIV - TO PHL DUE TO INTERMITTENT "27 FLT CTRL FAULT PRIM REU INOP" MESSAGE FOLLOWED BY "RUDDER FAIL" MESSAGE. CORRECTIVE ACTION: CLEARED THE LATCHED FAULT FROM PRIMARY FLIGHT CONTROL COMPUTER (PFCC), REPLACED AFT REMOTE ELECTRONICS UNIT (REU) 1, PE
- [SDR DALA2025011600377](https://openairdocs.org/sdr/DALA2025011600377.md): Skin · dented · Jan 13, 2025 · N120DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > DTE, ER/A 610713-14AD REV D REQUIRES STAGE 3 DTA APPROVAL. A220-100 / NOSE FUSELAGE / LHS SKIN / FR15 / DENT.ER/A 610713-14AD REV D REQUIRES STAGE 3 DTA APPROVAL ON OR BEFORE 14,250 FLIGHT CYCLES FROM SECTION III REPAIR EMBODIMENT OR 24,930 FLIGHT HOURS FROM S
- [SDR DALA2025052704055](https://openairdocs.org/sdr/DALA2025052704055.md): Fairing · missing · Nov 9, 2024 · N120DU · Airbus BD5001A10 · Horizontal Stabilizer Miscellaneous Structure
  > DURING SVC FOUND RH TIP FAIRING HORIZONTAL STAB MISSING CORROSION PROTECTOR MATERIAL AND PAINT. PERFORMED TEMP REPAIR PER A220 ASRP 55-12-86-01AAA-662A-A. TEMP REPAIR IS PERMITTED FOR PERIOD NOT MORE THAN 8500 FLIGHT HOURS. SPEED TAPE APPLIED PER A220 ASRP 51
- [SDR DALA2024110110584](https://openairdocs.org/sdr/DALA2024110110584.md): Valve · faulted · Oct 31, 2024 · N120DU · Airbus BD5001A10 · Fuel Transfer Valve
  > SHIP 8120 - DIV - TO IAD DUE TO UNCOMMANDED FUEL TRANSFER FROM CENTER TANK TO RIGHT TANK. CORRECTIVE ACTION: R/R RT TANK TRANSFER FLOAT SOV AND #2 IFPC. (LP# 5725208)
- [SDR DALA2024053005633](https://openairdocs.org/sdr/DALA2024053005633.md): Light · inoperative · May 27, 2024 · N120DU · Airbus BD5001A10 · Emergency Lighting
  > DURING SVC CHECK FOUND AFT LEFT DOOR EMERGENCY ESCAPE LIGHT INOP. REMOVED LEFT AFT DOOR EMERGENCY LIGHT REF A220 AMM 33-55-02, C/B PULLED, SEAT ROW 28 AB SIDEWALL PANELS REMOVED. R&R LEFT AFT DOOR EMERGENCY LIGHT PER AMP 33-55. OPS CHECK GOOD. FINISHED CLOSE U
- [SDR DALA2024053005632](https://openairdocs.org/sdr/DALA2024053005632.md): Light · inoperative · May 26, 2024 · N120DU · Airbus BD5001A10 · Emergency Lighting
  > DURING SVC CHECK FOUND RT OVER WING FWD EMERGENCY ESCAPE LIGHT INOP. REMOVED RT WING FWD EMERGENCY LIGHT, REF: A220 AMP 33-55-02, C/B PULLED, PANEL 194AR REMOVED. WIP014043. INSTALLED SERVICEABLE LIGHT ASSEMBLY IN RT WING OVER WING AREA AND OPS CHECK OK. RESET
- [SDR DALA2024022902823](https://openairdocs.org/sdr/DALA2024022902823.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER FWD OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 3 LOWER FWD OB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223120)
- [SDR DALA2024022902822](https://openairdocs.org/sdr/DALA2024022902822.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 LOWER FWD IB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223119)
- [SDR DALA2024022902821](https://openairdocs.org/sdr/DALA2024022902821.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FWD OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER FWD OB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223117)
- [SDR DALA2024022902820](https://openairdocs.org/sdr/DALA2024022902820.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223114)
- [SDR DALA2024022902819](https://openairdocs.org/sdr/DALA2024022902819.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · 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 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223113)
- [SDR DALA2024022902818](https://openairdocs.org/sdr/DALA2024022902818.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LOWER FWD IB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223111)
- [SDR DALA2024022902817](https://openairdocs.org/sdr/DALA2024022902817.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 LOWER FWD OB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 LOWER FWD OB SIDE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223108)
- [SDR DALA2024022902816](https://openairdocs.org/sdr/DALA2024022902816.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER FWD SURFACE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223106)
- [SDR DALA2024022902815](https://openairdocs.org/sdr/DALA2024022902815.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 UPPER AFT SURFACE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223105)
- [SDR DALA2024022902814](https://openairdocs.org/sdr/DALA2024022902814.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223104)
- [SDR DALA2024022902813](https://openairdocs.org/sdr/DALA2024022902813.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 29FEB24 0210 UTC 02 CORR BY ALLISON 02532897 IAH 29FEB24 ATA 5742 RII
- [SDR DALA2024022902812](https://openairdocs.org/sdr/DALA2024022902812.md): Slat Track · corroded · Feb 29, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 608436- 14AD REV C AND PRI 608436-14AD REV 0 MATCHED. (LP# 0223097)
- [SDR DALA2024022902811](https://openairdocs.org/sdr/DALA2024022902811.md): Slat Track · corroded · Feb 28, 2024 · N120DU · Airbus BD5001A10 · 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 608437- 14AD REV B AND PRI 608437-14AD REV 0 MATCHED. (LP# 0222876)
- [SDR DALA2024022902810](https://openairdocs.org/sdr/DALA2024022902810.md): Slat Track · corroded · Feb 28, 2024 · N120DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 608437- 14AD REV B AND PRI 608437-14AD REV 0 MATCHED. (LP# 0222874)
- [SDR DALA2024022902809](https://openairdocs.org/sdr/DALA2024022902809.md): Slat Track · corroded · Feb 28, 2024 · N120DU · Airbus BD5001A10 · 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 608437- 14AD REV B AND PRI 608437-14AD REV 0 MATCHED. (LP# 0222871)
- [SDR DALA2024022902808](https://openairdocs.org/sdr/DALA2024022902808.md): Slat Track · corroded · Feb 28, 2024 · N120DU · Airbus BD5001A10 · 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 608437- 14AD REV B AND PRI 608437-14AD REV 0 MATCHED. (LP# 0222870)
- [SDR DALA2024022302542](https://openairdocs.org/sdr/DALA2024022302542.md): Engine · vibration · Feb 20, 2024 · N120DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > SHIP 8120 -DIV- TO DTW DUE TO #1 ENGINE N2 VIBRATION INDICATION. THROTTLE WAS REDUCED TO STOP VIBRATION INDICATION, VIBE CAUTION MESSAGE REOCCURRED EACH TIME THROTTLE ADVANCED. CORRECTIVE ACTION: #1 ENGINE REPLACED. (LP# 0209612, 4898355, 0209953) PW1521G3

Next page: https://openairdocs.org/aircraft/N120DU/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 = 'N120DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N120DU/reports

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