# Service difficulty reports: Airbus Canada LP BD-500-1A11

A list on [Airbus Canada LP BD-500-1A11](https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 29 · 1,410 reports

- [SDR BAGA2026110900002](https://openairdocs.org/sdr/BAGA2026110900002.md): Oxygen Mask · no test · Nov 8, 2026 · N221BZ · Airbus BD5001A11 · Passenger Oxygen System
  > UNCOMMANDED O2 MASK DROP ON GROUND WITH L1 AND L2 DOOR OPEN. INTERMITTENT EICAS MESSAGES APPEAR AND THEN IDSAPPEAR.CABIN ALT MOMENTARILY SPIKES UP TO 33,000 FEET WITH DOORS OPEN ON GROUND. LANDING ELEVATION MOMENTARILY SPIKES FROM 400 TO 3000FT DELTA PRESSURE
- [SDR BAGA2026110900001](https://openairdocs.org/sdr/BAGA2026110900001.md): Skin · gouged · Nov 2, 2026 · N245BZ · Airbus BD5001A11 · Rudder, Plate/Skin
  > REPAIR AT VENDOR IN BHM - UPON REMOVAL OF PANELS 325DR AND 325DL, DAMAGE FOUND ON LEFT AND RIGHT RUDDER LEADING EDGES. TEMP REPAIR PERFORMED.
- [SDR YENA2026102600996](https://openairdocs.org/sdr/YENA2026102600996.md): Slide · deployed · Oct 24, 2026 · N3260J · Airbus BD5001A11 · Escape Slide
  > FLT372, SLC-JFK. L2 SLIDE DEPLOYED; R & R L2 SLIDE IAW BD500-A-J25-63-01-03AA-720A-A.
- [SDR YENA2026101900990](https://openairdocs.org/sdr/YENA2026101900990.md): Shutoff Valve · false indication · Oct 17, 2026 · N3284J · Airbus BD5001A11 · Pneumatic Distribution System
  > FLT#953, JFK-DJT-RTF. 36 L BLEED FAIL. L PRESS REG SOV INOP. ( ENGINE BLEED PRESSURE REGULATING SHUTOFF VALVE (PRSOV) LEFT SIDE CBV OPERATIVE). ACCOMPLISHED METHOD 1. VERIFIED NO EVIDENCE OF EXCESSIVE HPV LEAKAGE PER MEL 36-12-01E. A/C OK TO CONT. CROSSBLEED
- [SDR YENA2026101900989](https://openairdocs.org/sdr/YENA2026101900989.md): Door · open · Oct 17, 2026 · N3044J · Airbus BD5001A11 · Cargo/Baggage Doors
  > FLT#716, BUF-BOS. CARGO DOOR CAUTION EICAS MSG ON CLIMB OUT.11K FEET.A/C PRESSURIZED OK;CONTINUED.; ACFT ARRIVED W/CARGO DOOR HANDLE OPEN.ACCOMP OPERATIONAL CK OF FWD CARGO DOOR IAW AMP 52-30-00.DOOR OPS CK GOOD.NO DEFECT NOTED.
- [SDR BAGA2026102800004](https://openairdocs.org/sdr/BAGA2026102800004.md): Door · corroded · Oct 14, 2026 · N230BZ · Airbus BD5001A11 · Fluid Service Doors
  > REAR FUSELAGE WASTE DOOR 146BR FOUND CORROSION. WORK PERFORMED BY AVIANOR IN YMX UNDER WO 229296 AN WO 213370 REFERENCE NON-ROUTINE 3014 WASTE DOOR 146BR REPLACED IAW A220 AMP BD500-A-J52-47-06-05AAA-520A-A/.720A-A ELECTRICAL BONDING TESTED SERVICEABLE.
- [SDR DALA2026101905728](https://openairdocs.org/sdr/DALA2026101905728.md): Slat Track · damaged · Oct 14, 2026 · N325DU · Airbus BD5001A11 · Leading Edge Devices
  > PER STEP 11 OF AMDS 5742-01028-02A PERFORM EDDY CURRENT INSPECTION OF BLENDED AREA(S) OF SLAT TRACK 11. PERFORMED EDDY CURRENT INSPECTION OF BLEND PER ANDTP BD500-A-J51 -01-20-01AAA-353A-A. (LP# 1864913; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101905727](https://openairdocs.org/sdr/DALA2026101905727.md): Slat Track · damaged · Oct 14, 2026 · N325DU · Airbus BD5001A11 · Leading Edge Devices
  > PER STEP 11 OF AMDS 5742-01028-02A PERFORM EDDY CURRENT INSPECTION OF BLENDED AREA(S) OF SLAT TRACK 9. PERFORMED EDDY CURRENT INSPECTION OF BLEND PER ANDTP BD500-A-J51 -01-20-01AAA-353A-A. (LP# 1864912; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101905726](https://openairdocs.org/sdr/DALA2026101905726.md): Slat Track · damaged · Oct 14, 2026 · N325DU · Airbus BD5001A11 · Leading Edge Devices
  > PER STEP 11 OF AMDS 5742-01028-02A PERFORM EDDY CURRENT INSPECTION OF BLENDED AREA(S) OF SLAT TRACK 7. PERFORMED EDDY CURRENT INSPECTION OF BLEND PER ANDTP BD500-A-J51 -01-20-01AAA-353A-A. (LP# 1864910; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101905725](https://openairdocs.org/sdr/DALA2026101905725.md): Slat Track · damaged · Oct 14, 2026 · N325DU · Airbus BD5001A11 · Leading Edge Devices
  > PER STEP 11 OF AMDS 5742-01028-02A PERFORM EDDY CURRENT INSPECTION OF BLENDED AREA(S) OF SLAT TRACK 6. PERFORMED EDDY CURRENT INSPECTION OF BLEND PER ANDTP BD500-A-J51 -01-20-01AAA-353A-A. (LP# 1864907; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101905724](https://openairdocs.org/sdr/DALA2026101905724.md): Slat Track · not reported · Oct 14, 2026 · N325DU · Airbus BD5001A11 · Leading Edge Devices
  > PER STEP 11 OF AMDS 5742-01028-02A PERFORM EDDY CURRENT INSPECTION OF BLENDED AREA(S) OF SLAT TRACK 5. PERFORMED EDDY CURRENT INSPECTION OF BLEND PER ANDTP BD500-A-J51 -01-20-01AAA-353A-A
- [SDR DALA2026101405650](https://openairdocs.org/sdr/DALA2026101405650.md): Reu · faulted · Oct 12, 2026 · N308DU · Airbus BD5001A11 · Rudder Control System
  > DIVERTED TO XYX, DUE TO RUDDER FAIL MESSAGE. EMERGENCY DECLARED. REMOVED & REPLACED THE NR 2 AFT REU. (LP# 8954060; AIRCRAFT WAS GROUNDED)
- [SDR YENA2026101400950](https://openairdocs.org/sdr/YENA2026101400950.md): Unknown · odor · Oct 11, 2026 · N3195J · Airbus BD5001A11 · Air Distribution System
  > FLT#1307, BOS-BNA. ALL 3 FLIGHT ATTENDANTS REPORTED AN ODOR UPON LANDING SMELLED LIKE CHEMICAL OR BURNING CANDLE; TROUBLESHOOT PER TSM BD500-A-J21-22-00 WITH NO DEFECTS FOUND A/C EXTERIOR GUI WITH NO LEAKS FANNEL PERFORMED PACK RUN OF BOTH LEFT AND RIGHT PACK
- [SDR YENA2026101200946](https://openairdocs.org/sdr/YENA2026101200946.md): Control Valve · failed · Oct 11, 2026 · N3241J · Airbus BD5001A11 · Pneumatic Distribution System
  > FLT#2098, FLL-FLL AIR TURNBACK. ON T/O R BLEED FAIL CAUTION EICAS PRECAUTIONARY AIRRETURN ACCOMPLISHED DUE TO L BLEED BEING DEFERRED; REMOVED AND REPLACED ENG 2 PRESSUREREGULATING VALVE ( PRSOV) REF AMP J36-11-01. OPS AND LEAK S CHK GOOD. NO FAULTS NOTED ATTHI
- [SDR DALA2026101205600](https://openairdocs.org/sdr/DALA2026101205600.md): Elec Connector · loose · Oct 8, 2026 · N308DU · Airbus BD5001A11 · Landing Gear System Wiring
  > DIVERTED TO FLL DUE TO WEIGHT ON WHEEL FAIL AND RT GEAR DISAGREE. GEAR HANDLE SELECTED DOWN AND NOW HAVE ALL THREE GREEN. FOUND CONNECTOR LOOSE AT MT1678. SAME SECURED. REPLACED MT677 AND MT678 SENSORS. (LP# 8954046, 1852016; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101205601](https://openairdocs.org/sdr/DALA2026101205601.md): Heater · odor · Oct 6, 2026 · N311DU · Airbus BD5001A11 · Heating System
  > AFTER ENGINE START, AFT FA'S REPORTED STRONG DIRTY SOCK/MUSTY SMELL IN AFT GALLEY AND LAST 2 ROWS. SMELL REMAINED WITH PACKS ON R ENG BLEED, L BLEED ALREADY DEFERRED. C/W SMOKE AND FUME W/C 0550-2001 WITH NO ISSUES FOUND. DUE TO REPORT OF FUME ONLY IN AFT GALL
- [SDR YENA2026100700931](https://openairdocs.org/sdr/YENA2026100700931.md): Unknown · odor · Oct 6, 2026 · N3215J · Airbus BD5001A11 · Air Distribution System
  > FLT 151, BOS-SRQ. AT FL 300 IN VMC COND THE FA REPORTED DIRTY SOCKS ODOR IN GALLEY THAT LASTED 15 MINS. UPON LANDING AFTER APU START WE GOT TWO PUFFS OF DIRTY SOCK ODOR IN THE COCKPIT.; APPLIED FIP BD500-A-J21-22-00-00AAA-423A-A FOR UNUSUAL ODOR OF SMOKE OR FU
- [SDR BAGA2026100700003](https://openairdocs.org/sdr/BAGA2026100700003.md): Elt · no test · Oct 6, 2026 · N217BZ · Airbus BD5001A11 · Life Raft
  > LEFT LIFE RAFT NR 2 ELT FAILED AN OPS TEST. REMOVED AND REPLACED ELT. OPS TESTED GOOD.
- [SDR BAGA2026100700002](https://openairdocs.org/sdr/BAGA2026100700002.md): Elt · no test · Oct 6, 2026 · N217BZ · Airbus BD5001A11 · Emergency Locator Beacon
  > LEFT LIFE RAFT, NR 1 ELT FAILED TO OPS TEST. REMOVED AND REPLACED ELT. OPS TEST GOOD.
- [SDR BAGA2026100700001](https://openairdocs.org/sdr/BAGA2026100700001.md): Elt · no test · Oct 6, 2026 · N217BZ · Airbus BD5001A11 · Emergency Locator Beacon
  > LEFT LIFE RAFT, NR 3 ELT FAILED OPS TEST. REMOVED AND REPLACED ELT. OPS TEST GOOD.
- [SDR DALA2026100705542](https://openairdocs.org/sdr/DALA2026100705542.md): Floor Panel · corroded · Oct 5, 2026 · N310DU · Airbus BD5001A11 · Fuselage Floor Panel
  > R1 DOOR FLOOR PANEL# 222KRF HAS CORROSION. REMOVED AND REPLACED R1 DOOR FLOOR PANEL# 222KRF IAW A220 AMP BD500-A-J53-00-47-12AAA-520A-A AND A220 AMP BD500-A-J53-00-47- 12AAA-720A-A. (LP# 1850064; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100705544](https://openairdocs.org/sdr/DALA2026100705544.md): Bleed Air Sys · odor · Oct 4, 2026 · N311DU · Airbus BD5001A11 · Engine Bleed Air System
  > MUSTY/BURNY SMELL COMING FROM AFT GALLEY, CAN SMELL THESE FUMES FROM MID CABIN TO AFT TO THE GALLEY, SMELL STRONGER THE FURTHER AFT YOU GO. NO SMOKE ONLY FUMES. PREFORMED GVI OF AFT GALLEY AND COFFEE MAKERS. NO DAMAGE OR ODORS NOTED. COMPLIED WITH WORK CARD 05
- [SDR DALA2026100705539](https://openairdocs.org/sdr/DALA2026100705539.md): Floor Support · corroded · Oct 3, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR20, RBL 33 HAS CORROSION. REPLACED FLOOR SUPPORT AT PASSENGER CABIN FR20, RBL33 FOR A SERVICEABLE PART PER ASRP BD500-A-J51-42-21- 00AAA-078A-A. (LP# 1846196; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100705538](https://openairdocs.org/sdr/DALA2026100705538.md): Slide · damaged · Oct 3, 2026 · N322DU · Airbus BD5001A11 · Escape Slide
  > LH OVERWING SIDE VALVE PIN HOLE FOUND TO BE OBSTRUCTED. COMPLIED WITH AMDS 2563-4002 AND 2561-9005. (LP# 1845624; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100705537](https://openairdocs.org/sdr/DALA2026100705537.md): Slide · damaged · Oct 3, 2026 · N322DU · Airbus BD5001A11 · Escape Slide
  > RH OVERWING SLIDE VALVE PIN HOLE FOUND TO BE OBSTRUCTED. COMPLIED WITH AMDS 2563-4005 AND 2561-9006 SLIDE, PACK, OW AIRCRAFT WAS GROUNDED)
- [SDR YENA2026100500927](https://openairdocs.org/sdr/YENA2026100500927.md): Anti-Ice Valve · faulted · Oct 3, 2026 · N3138J · Airbus BD5001A11 · Airfoil Anti/De-ice System
  > FLT 2895, BOS-PUJ-RTF. REF. DEFECT 4559648 ITEM 1 RIGHT WING ANTIICE VALVE REQ'D OPS CHECK AND ENG HIGH POWER RUN.; PERFORMED OPS CHECK & HIGH POWER RUN IAW AMP 30-12-01 ALL OPS NORMAL AT THIS TIME A/C IS OK FOR SERVICE.
- [SDR DALA2026100505499](https://openairdocs.org/sdr/DALA2026100505499.md): Waste Box · corroded · Oct 2, 2026 · N322DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > LAVATORY WASTE BOX FWD RIGHT HAND CORNER (DOOR SEAL AREA) HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 081-0001:0591-0301/004 00127 COMPLIED WITH ER/A 637082-14 PRI REV 0, 1, 2, AND ER/A 637082-14 REV ORI
- [SDR DALA2026100505502](https://openairdocs.org/sdr/DALA2026100505502.md): Unknown · odor · Oct 1, 2026 · N330DU · Airbus BD5001A11 · Air Distribution System
  > FA'S REPORTED HOT PLASTIC/ACETONE ODOR FOR ABOUT 30 SECONDS AT TOP OF DESCENT ROW 2-3. COMPLETED ISOLATE SMOKE & FUMES AMDS W/C 0550-2001. DETERMINED TO BE CARGO/CABIN PER TABLE 3. NO ISSUES NOTED IN IFE OR IN SEAT POWER SYSTEMS. FWD GALLEY OVEN HAD STRONG ODO
- [SDR DALA2026110506039](https://openairdocs.org/sdr/DALA2026110506039.md): Wing Tip · damaged · Sep 30, 2026 · N338DU · Airbus BD5001A11 · Wing Main, Frame Structure
  > RT WING TIP EROSION TAPE PEELING. C/W PERMANENT REPAIR OF EROSION TAPE IAW AMP 51-22. REF ASRP 57-32-00-00AAA-662A-A. (LP 9115191, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505501](https://openairdocs.org/sdr/DALA2026100505501.md): Light · inoperative · Sep 30, 2026 · N308DU · Airbus BD5001A11 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS, L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. (LP# 8954013; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026100505500](https://openairdocs.org/sdr/DALA2026100505500.md): Light · inoperative · Sep 30, 2026 · N308DU · Airbus BD5001A11 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - LEFT FWD OVER WING EMERGENCY LIGHT INOP. R/R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. (LP# 8964012; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505498](https://openairdocs.org/sdr/DALA2026100505498.md): Bracket · corroded · Sep 30, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > CORROSION G4 BRACKET AT LBL 1, FR 76-78 HAS CORROSION (MARKED). C/W ER/A 637185-14 REV ORIGINAL ASSOCIATED ER/A 14-637185 ADDED FOR AC 8310. (LP# 1840747; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100505497](https://openairdocs.org/sdr/DALA2026100505497.md): Frame · corroded · Sep 29, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Frame
  > CORROSION, SECTION 48 FRAME HAS EVIDENCE OF CORROSION AT FR 81 STGR 19L. REMOVED AND REPLACED CENTER SECTION FRAME AT FR 81 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG: C01401201 REV:-R. (LP# 1839389; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005436](https://openairdocs.org/sdr/DALA2026093005436.md): Unknown · odor · Sep 29, 2026 · N326DU · Airbus BD5001A11 · Air Distribution System
  > DIV - TO BOI DUE TO FUMES IN ROWS 11-20. PERFORMED LEVEL "A " DECONTAMINATION, SMELL NO LONGER PRESENT. (LP# 9456408; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005435](https://openairdocs.org/sdr/DALA2026093005435.md): Web · corroded · Sep 28, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > AFT OF R2 DOOR, FLOOR STRUCTURE WEB HAS CORROSION AT FR 76-79. REMOVED AND REPLACED FLOOR STRUCTURE WEB AFT OF R2 DOOR BETWEEN FR 76-79 IAW A220 ASRP BD500-A-J51-41-02-00AAA-078A-A AND DWG C01342700 REV T. (LP# 1837447; AIRCRAFT WAS GROUNDED)
- [SDR YENA2026092800912](https://openairdocs.org/sdr/YENA2026092800912.md): Unknown · odor · Sep 27, 2026 · N3139J · Airbus BD5001A11 · Air Distribution System
  > FLT#1486, RDU-JFK. STRONG CHEMICAL SMELL IN AFT GALLEY REPORTED BY F3 IN FLIGTH; ACCOMPLISHED ENG 1+2 RUN PER AMP 71-00-00 ISOLATED ENG1 BLEED, ENG 2 BLEED AND APU. NO CHEMCIAL SMELL FROM NIEHTER. HAD 4 JB CREW MEMBERS VERIFY NO SMELL COMING FROM CABIN NOR F
- [SDR DALA2026093005433](https://openairdocs.org/sdr/DALA2026093005433.md): Seat Track · corroded · Sep 26, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > RT INBOARD SEAT TRACK AT RBL 23, FR74 CORRODED. REMOVED AND REPLACED RT INBD SEAT TRACK AT RBL 23 BETWEEN FR 61 TO FR 74 PER DWG PL C01342701 REV-G AND ASRP BD500-A-J51-42-21-00AAA-078A-A. (LP# 1833889; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005432](https://openairdocs.org/sdr/DALA2026093005432.md): Pad · corroded · Sep 26, 2026 · N322DU · Airbus BD5001A11 · Fluid Service Doors
  > LAVATORY WASTE BOX ACCESS DOOR LATCH (WEAR PADS) HAVE CORROSION. LOCATED ON THE AFT SIDE OF THE WASTE BOX CUT OUT. REMOVED AND REPLACED WASTE BOX DOOR LATCH P ADS PER ASRP 51-42-06 (LP# 1833042; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026093005431](https://openairdocs.org/sdr/DALA2026093005431.md): Spring · corroded · Sep 26, 2026 · N322DU · Airbus BD5001A11 · Fluid Service Doors
  > LAVATORY WASTE BOX ACCESS DOOR HINGE SPRINGS HAVE CORROSION. REMOVED AND REPLACED SPRINGS REF A220 AMP 52-47-06.
- [SDR DALA2026093005430](https://openairdocs.org/sdr/DALA2026093005430.md): Door · corroded · Sep 26, 2026 · N322DU · Airbus BD5001A11 · Fluid Service Doors
  > LAVATORY WASTE BOX ACCESS DOOR HAS TWO LARGE AREAS OF CORROSION. REMOVED AND REPLACED WASTE SERVICE DOOR REF AMP 52-47-06. (LP# 1833038; AIRCRAFT WAS GROUNDED)
- [SDR YENA2026092800909](https://openairdocs.org/sdr/YENA2026092800909.md): Engine · bird ingestion · Sep 25, 2026 · N3203J · Airbus BD5001A11 · Engine (Turbine/Turboprop)
  > FLT#2008, FLL-PIT. #2 ENG BIRD STRIKE. PERFORMED ENG BIRD STRIKE INSPECTION. FOUND INGESTIION #2 ENG CORE. NO REPORTED ABNORMAL ENG PARAMETERS OR CABIN ODOR. GVI RESULT IN NO DAMAGE NOTED.. REF AMP J72-00-00. PLACED ON DEFERRAL OF BOROSCOPE FOR 10FC OR 25 HR
- [SDR DALA2026092805392](https://openairdocs.org/sdr/DALA2026092805392.md): Seat Track · corroded · Sep 25, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > OUTBOARD RT SEAT TRACK AT FR 20, RBL 43.5 WAS CORRODED. REMOVED AND REPLACED THE FWD RT SEAT TRACK, FR 20 - 30 IAW DWG PL C02312600, REV K, AND ASRP BD500-A-51-42-20-00AAA-078A-A. (LP 1832414, AIRCRAFT WAS GROUNDED).
- [SDR DALA2026092805391](https://openairdocs.org/sdr/DALA2026092805391.md): Mount · cracked · Sep 25, 2026 · N333DU · Airbus BD5001A11 · Wing Main, Frame Structure
  > WHILE WORKING AMDS 5742-01028-01A FOUND POSSIBLE CRACK ON LT UPPER OTBD CORNER OF TELESCOPING DUCT MOUNTING PLATE. C/W AMDS W/C 2881-4002-LH REF. NRC 018 ASSOCIATED AA 5742-01028 ADDED FOR AC 8333. (LP# 1832219; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805390](https://openairdocs.org/sdr/DALA2026092805390.md): Mount · cracked · Sep 25, 2026 · N333DU · Airbus BD5001A11 · Leading Edge Devices
  > DURING INSPECTION OF THE LT WING, SLAT 2, FOUND A CRACK ON UPPER OTBD CORNER OF TELESCOPING DUCT MOUNTING PLATE. COMPLIED WITH AMDS W/C 2781-4002-LT SLAT NR 2. REMOVED & INSTALLED IAW C01612003-001. (LP 1832213; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026092805389](https://openairdocs.org/sdr/DALA2026092805389.md): Seat Track · corroded · Sep 25, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK CORRODED. RBL 43.5, FR 74. R & R THE RT SEAT TRACK, FR 61 - 74 IAW DWG PL C01342701, REV G AND ASRP BD500-A-J51-42-20-00AAA-078A-A. (LP 1831445; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805388](https://openairdocs.org/sdr/DALA2026092805388.md): Support · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > SUPPORT, LAV E HAD CORROSION IN FASTENER HOLES, LBL 11, FR 76-79, WL147. REMOVED AND REPLACED THE LAV SUPPORT IAW ASRP BD500-J51-42-21-00AAA-078A-A, & DWG PL C01342700, REV T. (LP 1830130; AIRCRAFT WAS GROUNDED).
- [SDR DALA2026092805387](https://openairdocs.org/sdr/DALA2026092805387.md): Seat Track · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OTBD SEAT TRACK CORRODED, LBL 43.50, FR 74. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J53-61-49-00AAA -661A-A, ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C01342701, REV G. (LP 1829629; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805385](https://openairdocs.org/sdr/DALA2026092805385.md): Web · corroded · Sep 24, 2026 · N310DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > AFT OF L2 DOOR, FLOOR WEB WAS CORRODED, FR 76 - 79. EVALUATED DAMAGE ON FLOOR WEB AND FOUND OUT OF LIMITS, NO DAMAGE PERMITTED IAW ASRP BD500-A-J51-10-06- 00AAA-028A-A, REMOVED AND REPLACED THE WEB IAW ASRP BD500-A-J51 -40-11-01AAA-652A-A, ASRP BD500-A-J51-
- [SDR DALA2026092805384](https://openairdocs.org/sdr/DALA2026092805384.md): Seat Track · corroded · Sep 23, 2026 · N310DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > INBOARD RT SEAT TRACK AT FR20, RBL 23 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW ASRP BD500-A-J51-42-20-00AAA-078A-A, AND DWG PL C02312600, REV K. (LP 1828498; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092805383](https://openairdocs.org/sdr/DALA2026092805383.md): Support Beam · corroded · Sep 23, 2026 · N310DU · Airbus BD5001A11 · Fuselage Main, Structure
  > RIGHT OTBD SUPPORT BEAM CORRODED AT FR 76-78, RBL 36.5, WL 147 IN THE NUT PLATE HOLE. REMOVED AND REPLACED THE SUPPORT BEAM IAW ASRP BD500-A-J51-42-21-00AAA-078A-A. AND DWG PL C01342700 REV-T. (LP 18283474; AIRCRAFT WAS GROUNDED).

Next page: https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11/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 aircraft_model_key = 'BD5001A11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-canada-lp-bd-500-1a11/reports

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