# Service difficulty reports: N132DU A list on [N132DU](https://openairdocs.org/aircraft/N132DU.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DALA2026082504826](https://openairdocs.org/sdr/DALA2026082504826.md): Waste Box · corroded · Jul 10, 2026 · N132DU · Airbus BD5001A10 · Fuselage Main, Structure > ERA 635462-14: WASTE BOX CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN EVERY 1000 FLIGHT HOURS FROM 12873 TOTAL AIRCRAFT HOURS AS OF 09JUL2026 UNTIL SECTION III IS ACCOMPLISHED. ACCOMPLISH SECTION III WITHIN 10,000 FLIGHT HO - [SDR DALA2026071304119](https://openairdocs.org/sdr/DALA2026071304119.md): Access Panel · corroded · Jul 10, 2026 · N132DU · Airbus BD5001A10 · Fuselage Main, Structure > EVIDENCE OF CORROSION ON WASTE WATER ACCESS SURROUND STRUCTURE ON FWD INBD CORNER OF PAN. COMPLIED WITH ER/A 635462-14 REV ORIGINAL ASSOCIATED ER/A 14-635462 ADDED FOR AC 8132. (LP# 1692882; AIRCRAFT WAS GROUNDED) - [SDR DALA2026071304114](https://openairdocs.org/sdr/DALA2026071304114.md): Floor Support · corroded · Jul 9, 2026 · N132DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin > CORROSION ON FWD CARGO COMPARTMENT LOWER SILL AROUND FASTENER HOLES. COMPLIED WITH ER/A 635498-14 REV ORIGINAL ASSOCIATED ER/A 14-635498 ADDED FOR AC 8132. (LP# 1690635; AIRCRAFT WAS GROUNDED) - [SDR DALA2026071304111](https://openairdocs.org/sdr/DALA2026071304111.md): Floor Panel · corroded · Jul 8, 2026 · N132DU · Airbus BD5001A10 · Fuselage Floor Panel > CORROSION AT R2 ENTRY FLOOR RBL 52 FR74 WL 151.5. REPLACED R2 ENTRY FLOOR LOCATED ON RBL52 FR74 WL 151.5 IAW ASRP BD500-A-J51-41-02-00AAA-078A-A AND COMPLYING WITH DWG #PL C01342700 REV T. (LP# 1688457; AIRCRAFT WAS GROUNDED) - [SDR DALA2026071304110](https://openairdocs.org/sdr/DALA2026071304110.md): Floor Panel · corroded · Jul 8, 2026 · N132DU · Airbus BD5001A10 · Fuselage Floor Panel > CORROSION AT L2 ENTRY FLOOR LBL 52 FR74 WL 151.5. REMOVED AND REPLACED ENTRY FLOOR LOCATED ON FR 74 LBL 52 WL 151.5 L2 DOOR PER A220 AMP BD500-A-J53-00-47-13AAA-720A-A AND DWG C01342700 REV:-T. (LP# 1688449; AIRCRAFT WAS GROUNDED) - [SDR DALA2026082504828](https://openairdocs.org/sdr/DALA2026082504828.md): Longeron · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > ER/A 635349-14; A220-100 / FWD & CNTR WING TO BODY FAIRING / MULTIPLE LONGERON / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635349-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 12,873 TOTAL AIRCRAFT FLIGHT HOURS - [SDR DALA2026070703964](https://openairdocs.org/sdr/DALA2026070703964.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE FROM LBL 11 TO RBL 20, FR 36. ACCOMPLISHED ER/A 635384-14 REV-ORIGINAL. ASSOCIATED ER/A 14-635384 ADDED FOR AC. (LP# 1675423; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703963](https://openairdocs.org/sdr/DALA2026070703963.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE FROM LBL 5 TO RBL 8, FR 40. ACCOMPLISHED ER/A 635384-14 REV-ORIGINAL. ASSOCIATED ER/A 14-635384 ADDED FOR AC. (LP# 1675417; AIRCRAFT WAS GROUNDED). - [SDR DALA2026070703962](https://openairdocs.org/sdr/DALA2026070703962.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT TO RBL 9 FR 40. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349 ADDED FOR AC. (LP# 1675181; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703961](https://openairdocs.org/sdr/DALA2026070703961.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT TO LBL 9 FR 40. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349 ADDED. (LP# 1675166; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703960](https://openairdocs.org/sdr/DALA2026070703960.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT LBL 9, FR 45. ACCOMPLISHED ER/A 635349-14 REV-ORIGINAL, ASSOCIATED ER/A 14-635349 ADDED. (LP# 1675152; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703959](https://openairdocs.org/sdr/DALA2026070703959.md): Support · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Aerodynamic Fairings > CORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT RBL 9 FR45. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349. (LP# 1675009; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703957](https://openairdocs.org/sdr/DALA2026070703957.md): Seat Track · corroded · Jun 30, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT INBD SEAT TRACK AFT END CORRODED AT FR 74, RBL 23, WL 151.5. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW REPLACEMENT SEAT TRACK ON RBL 23, FR 61- FR 74 IAW ASRP BD500-A-J51-42-20- 00AAA-078A-A, DWG C01342701 REV G. (LP# 1675572; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703954](https://openairdocs.org/sdr/DALA2026070703954.md): Frame · corroded · Jun 29, 2026 · N132DU · Airbus BD5001A10 · Fuselage Main, Frame > CORROSION ON FR-81 AFT FACE AT STR-35L. REMOVED AND REPLACED FR-81 BTW LBL=21 TO RBL=30 IAW0 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG C01401201, REV R. (LP# 1673099; AIRCRAFT WAS GROUNDED) - [SDR DALA2026070703951](https://openairdocs.org/sdr/DALA2026070703951.md): Seat Track · corroded · Jun 27, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT OTBD SEAT TRACK AFT END CORRODED AT FR 74, RBL 43.5, WL 151.5. REMOVED AND REPLACED THE SEAT TRACK, RBL 43.5 IAW ASRP BD500- A-J51-42-20-00AAA-078A-A AND DWG C01342701 REV-G. (LP# 1669803; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062903852](https://openairdocs.org/sdr/DALA2026062903852.md): Floor Panel · corroded · Jun 24, 2026 · N132DU · Airbus BD5001A10 · Fuselage Floor Panel > POSSIBLE CORROSION AT L1 ENTRY FLOOR LBL 49.5 FR20 MINUS 5 WL 151.5. REMOVED AND REPLACED ENTRY FLOOR PANEL AT L1 FWD PASSENGER DOOR PER A220 AMP BD500-A-J53-00-47-11AAA-520A-A AND BD500-A-J53-00- 47-11AAA-720A-A. (LP# 1664725; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062903851](https://openairdocs.org/sdr/DALA2026062903851.md): Floor Panel · corroded · Jun 24, 2026 · N132DU · Airbus BD5001A10 · Fuselage Floor Panel > POSSIBLE CORROSION AT R1 ENTRY FLOOR RBL 49.5 FR20 MINUS 2 WL 151.5. REMOVED AND REPLACED ENTRY FLOOR PANEL AT R1 FWD SERVICE DOOR PER A220 AMP BD500A-J53-00-47-12AAA-520A-A AND BD500A-J53-00-47- 12AAA-720A-A. (LP# 1664720; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062903850](https://openairdocs.org/sdr/DALA2026062903850.md): Seat Track · corroded · Jun 24, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > CORROSION AT FORWARD FLOOR STRUCTURE SEAT TRACK LBL 43.5 FR20 WL 151.5. REMOVED AND REPLACED SEAT TRACK AT LBL= 43.5 WL 151.5 BTW FR=20 TO FR=30 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG# BOMBARDIER C02312600 REV:K. (LP# 1664455; AIRCRAFT WAS GROUN - [SDR DALA2026062903849](https://openairdocs.org/sdr/DALA2026062903849.md): Seat Track · corroded · Jun 24, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > FORWARD CABIN RIGHT INBD SEAT TRACK CORROSION ON FORWARD END RBL 23 FR20 WL151.5. REMOVED AND REPLACED SEAT TRACK AT FORWARD CABIN RBL 23 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DRAWING C02312600 REV-K AT FR19-FR31 RBL23.5 WL 151.5. (LP# 1 - [SDR DALA2026062903848](https://openairdocs.org/sdr/DALA2026062903848.md): Seat Track · corroded · Jun 24, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > LEFT OTBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 43.5 WL151.5. REMOVED AND REPLACED SEAT TRACK L/H O/B AT FR61-FR74 LBL 43.5 WL 151.5 IAW A220ASRP BD500-A-J51-42-20-00AAAA-078A-A AND BOMBARDIER DWG C01342701 REV G. (LP# 1663940; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062903847](https://openairdocs.org/sdr/DALA2026062903847.md): Seat Track · corroded · Jun 23, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > LEFT INBD SEAT TRACK AFT END CORRODED AT FR 74 LBL 23 WL151.5. REMOVED AND REPLACED SEAT TRACK AT FR 74 TO FR61 LBL 23 WL 151.5 PER BOMBARDIER DWG C01342701 REV- G AND A220 ASRP BD500-A-J51- 42-21-00AAA-078A-A. (LP# 1662276; AIRCRAFT WAS GROUNDED) - [SDR DALA2026062903846](https://openairdocs.org/sdr/DALA2026062903846.md): Seat Track · corroded · Jun 22, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > FORWARD CABIN RIGHT O/B SEAT TRACK CORROSION ON FORWARD END RBL 43.5 FR20 WL151.5. REMOVED AND REPLACED SEAT TRACK AT RBL=43.5 BTW FR=19 TO FR=31, WL 151.5 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG= C02312600 REV: K. (LP# 1660243; AIRCR - [SDR DALA2026062903845](https://openairdocs.org/sdr/DALA2026062903845.md): Seat Track · corroded · Jun 22, 2026 · N132DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > CORROSION AT FORWARD FLOOR STRUCTURE SEAT TRACK LBL23 FR20 WL 151.5. REMOVED AND REPLACED SEAT TRACK AT LBL=23 BTW FR =19 TO FR=31 WL = 151.5 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND DWG= C02312600 REV K. (LP# 1660229; AIRCRAFT WAS GROUNDED) - [SDR DALA2025080705928](https://openairdocs.org/sdr/DALA2025080705928.md): Longeron · cracked · Aug 1, 2025 · N132DU · Airbus BD5001A10 · Fuselage Main, Longeron/Stringer > WHILE WORKING LOG 6823744, REMOVED WHEEL WELL BIN F.O.M. FOUND LONGERON CRACKED. REMOVED AND REPLACED LONGERON. OK FOR SERVICE. (LP# 1119309) - [SDR DALA2025091806856](https://openairdocs.org/sdr/DALA2025091806856.md): Skin · punctured · May 5, 2024 · N132DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin > STRINGER 1R TO 2R, SKIN PUNCTURED. SINCE THE COMPLIANCE TO PART 26.43 IS REQUIRED, THE AIRCRAFT IS LIMITED TO 12 MONTHS SERVICE AFTER REPAIR AND FATIGUE AND DAMAGE TOLERANCE EVALUATION (DTE) ARE REQUIRED WITHIN THIS TIME LIMIT IN ACCORDANCE WITH FAA ADVISORY - [SDR DALA2023021301099](https://openairdocs.org/sdr/DALA2023021301099.md): None · none · Feb 12, 2023 · N132DU · Airbus A300* · Aileron Control System > SHIP 8132 - DIV - DUE TO AILERON FAIL MESSAGE, CAUTION MESSAGE OCCURRED AT FL 390, RIGHT DEFLECTED HALFWAY UP WITH LEFT MULTIFUNCTION SPOILERS DEFLECTED SLIGHTLY ON SYNOPTIC PAGE. CORRECTIVE ACTION: REPLACED RIGHT OUTBOARD AILERON PCU. (LP 9991586) - [SDR DALA2023021301098](https://openairdocs.org/sdr/DALA2023021301098.md): None · none · Feb 10, 2023 · N132DU · Airbus A300* · Central Display > SHIP 8132 - ATO - DUE TO RIGHT SIDE FMS BLANKED OUT. CORRECTIVE ACTION: REMOVED AND REPLACED NUMBER 5 DISPLAY UNIT OK FOR SERVICE. (LP 2623820) - [SDR DALA2022081605562](https://openairdocs.org/sdr/DALA2022081605562.md): Slide · low pressure · Aug 11, 2022 · N132DU · Bombdr BD1001A10 · Escape Slide > FOUND R1 DOOR SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED R1 DOOR SLIDE PER AMDS WORKCARD 2563-4004 ( 975725) C/W RII OF FWD SVC DOOR SLIDE IAW AMDS 2563-4004. VERIFIED INFLATION BOTTLE SAFETY PIN REMOVED AND EOAM SYSTEM ARMED (QC5285) (360734). (LP# 895 - [SDR DALA2021100506088](https://openairdocs.org/sdr/DALA2021100506088.md): None · none · Sep 30, 2021 · N132DU · Airbus BD5001A10 · Wind Shear Detection System > SHIP 8132 - ATO - AT 80 KNOTS DUE TO WINDSHEAR WARNING. CORRECTIVE ACTION: NO ACTIVE FAULTS PRESENT. PERFORMED WEATHER RADAR SYSTEM AND TAWS OPERATIONAL TESTS. (LP# 7872342) - [SDR DALA2021071504000](https://openairdocs.org/sdr/DALA2021071504000.md): Valve · failed · Jul 14, 2021 · N132DU · Bombdr BD1001A10 · Air Intake Anti/De-Ice System > SHIP 8132 - DE DUE TO R ENG DEGRADED MESSAGE ON APPROACH. MESSAGE CAUSED BY R UPPER CAI VALVE FAIL. CORRECTIVE ACTION: REPLACED UPPER AND LOWER R ENG CAI VALVES. (LP# 7822764) ## 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 = 'N132DU' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N132DU/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.