N529EA

Service difficulty reports · 75

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

Query with SQL
duckdb -csv -c "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 = 'N529EA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2026081322601Spar · damagedREPAIR FOR MISALIGNED HOLES BETWEEN VERTICAL STABILIZER SPARS AND AFT FUSELAGE FRAMES, COMPLIED WITH ALL STEPS OF REO 670-51-00-121 REV - 2026-07-27, REPAIR FOR MISALIGNED HOLES BETWEEN VERTICAL STABILIZER SPARS AND AFT FUSELAGE FRAMES.Aug 11, 2026 · N529EA · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR VNAA2026041416301Elevator · ground damageELEVATOR STRUCK BY DE-ICE TRUCK DAMAGE OCCURRED / INSTALLED SERVICEABLE HORIZONTAL STABILIZER ASSY IAW AMM 27-40-00-400-801-A02. REPLACED LH ELEVATOR IAW CRJ 700 AMM 27-34-01-000/400-801. ALL OP CHECKS GOOD.Apr 10, 2026 · N529EA · Cndair CL6002C10 · Elevator StructureSDR VNAA2025062511101Coffeemaker · odorTHE FLIGHT CREW REPORTED A BURNING POPCORN SMELL WHILE ENROUTE. THE SMELL DISSIPATED. NO MEDICAL ATTENTION REQUIRED. PERFORMED OPS CHECK OF THE TEMPERATURE CONTROL SYSTEM IAW AMM 21-60-00-710-801. OPS CHECK GOOD AT THIS TIME. DURING OPS CHECK, NO ODORS WERE Jun 21, 2025 · N529EA · Cndair CL6002C10 · Buffet/GalleysSDR VNA2025F00013Angle · corrodedTHE FWD J ANGLE ON FS 280 IS CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.May 13, 2025 · N529EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202505140002Angle · corrodedPASSENGER DOOR LOWER SILL CAP ANGLE IS CORRODED ADJACENT TO THE PROX SWITCH. REMOVED UNSERVICEABLE PAX DOOR LOWER SILL CAP (P/N: SH670-31825-9S) IAW CRJ700 SRM 51-41-02-001-001-A01. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL CAP (P/NMay 13, 2025 · N529EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202505140001Frame · corrodedF.S. 319.70 FRAME FROM STRG. 26 R/H TO STRG. 27 HAS PATCH OF CORROSION. CUT AWAY DAMAGED FRAME SECTION AND SPLICED IN REPAIR FRAME IAW CRJ 700 SRM 53-00-06-201-006-A01.May 13, 2025 · N529EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2024030411101Connector · damagedBRAKE OVHT MASTER CAUTION IN FLIGHT / REMOVED ASCU MOUNTING TRAY AND FOUND CONNECTOR THREADED MOUNTING NUT MISSING, REINSTALLED ASCU MOUNTING TRAY WITH CONNECTOR ON CORRECT SIDE OF TRAY WITH NUT AND WASHER PER REO 670-32-48-002 PERMANENT REPAIR AND AMM 32-44-0Feb 26, 2024 · N529EA · Cndair CL6002C10 · Landing Gear System WiringSDR VNAA2024022011101Diaphragm · obstructedCABIN ALT CAUTION MSG, AT FLT LEVEL 360, CABIN ALT WENT TO 9000FLT / INSPECTED THE #2 SAFETY VALVE AND FOUND LOOSE INSULATION STUCK BETWEEN THE DIAPHRAGM AND IT€™S SEAT. REMOVED INSULATION AND PERFORMED A FUNCTIONAL TEST OF THE SAFETY VALVE IAW CRJ 700 AMM 21Feb 16, 2024 · N529EA · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA202208099994Seat Track · corrodedCORROSION AT SEAT RAIL RBL9 BETWEEN FS661+98 – FS677+8. SECTION OF SEAT RAIL WAS REPLACED, AT RBL9 ,BETWEEN FS=661+98 TO FS=677+8, PER CRJ-900 AMM 53-00-49 (CONFIG. A12).Aug 9, 2022 · N529EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202204179997Skin · corrodedCORROSION AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE.May 17, 2022 · N529EA · Cndair CL6002C10 · Service DoorsSDR VNAA202205149996Angle · crackedCRACK ON ATTATCHMENT ANGLE OF ACCESS PANEL 542AZ ON LH MLG SHOCK STRUT BAYMay 14, 2022 · N529EA · Cndair CL6002C10 · Main Landing Gear Strut/Axle/TruckSDR VNAA202205149995Stringer Splice · corrodedCORROSION ON STRINGER SPLICE ON FS 333.00, STGR 26RH. (SM)May 14, 2022 · N529EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202205149994Frame · corrodedCORROSION ON FRAME FS613 BETWEEN STGR 27 TO 26LH INTERNAL STRUCTURE AT CARGO COMPARTMENT FWD (CCF)May 14, 2022 · N529EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202205149993Skin · corrodedCORROSION AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTUREMay 14, 2022 · N529EA · Cndair CL6002C10 · DoorsSDR VNAA202205149992Seat Track · corrodedCORROSION ON SEAT RAIL 9RBL FROM FS 421.00 TO 477.40May 14, 2022 · N529EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202205149991Floor Support · corrodedCORROSION AT FLOOR ANGLE SUPPORT OF FS280.0 BETWEEN RBL9 AND LBL9May 14, 2022 · N529EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202203051111Switch · unserviceableIB GND SPLRS AND GND SPLR DEPLOY CAUTION MSGS IN FLIGHT, RH IB SPLR SHOWED DEPLOYED ON FLT/CTL PAGE / INTERROGATED MDC FOR B1 CODE 156704. ADVANCED DIAGNOSTICS SHOWED BIT FOR R IB GROUND SPOILER SENSOR SET TO 1. REMOVED AND REPLACED RH IB GROUND PROXIMITY SWITMar 2, 2022 · N529EA · Cndair CL6002C10 · Drag Control ActuatorSDR VNAA202202021113Spoileron · false indicationOB SPOILERONS CAUTION MESSAGE / CYCLED SYSTEM CBS MESSAGES CLEARED PROBLEM DID NOT REOCCUR.Jan 5, 2022 · N529EA · Cndair CL6002C10 · Flight Control SystemSDR VNAA202109131112Unknown · odorBURNING ODOR WHEN BLEEDS TRANSFERRED TO APU AFTER LANDING DISSIPATED AFTER A FEW MOMENTS / DEFERRED BOTH PACKS PER MEL 21-51-1-2 OPTION 3. PERFORMED OPS TEST OF AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 700 AMM 21-51-00-710-801. SMOKE ODOR NOT PRESENT FOR TSep 11, 2021 · N529EA · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202108231111Skin · dentedDURING MAINTENANCE OPERATIONS AT DAYTON INTERNATIONAL AIRPORT (DAY) FACILITIES IN DAYTON, OH, MAINTENANCE IDENTIFIED ONE SLIGHT DENT, IN THE FUSELAGE SKIN PANEL (P/N CC670ˆ’33101ˆ’5) AFT OF FS202.75, BELOW STGR12A LH SIDE. THE DENT MEASURES APPROX. 1.75"" LOAug 21, 2021 · N529EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202106081111Warning Message · false indicationNOSEWHEEL STEERING INOP MESSEGE DURING FLIGHT. EMERGENCY WAS DECLARED BEFORE LANDING IN LEX TO ENSURE TRUCKS WERE ROLLED. THE AIRCRAFT WAS ABLE TO COME TO A COMPLETE STOP, RESET THE SYSTEM, AND TAXI TO THE GATE UNDER THEIR OWN POWER. THERE WAS NO CALL FOR PAX Jun 4, 2021 · N529EA · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2020100711101Pcu · failedOUTBOARD SPOILERON/OUTBOARD FLT SPOILERS CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED RT OUTBOARD MULTI-FUNCTION SPOILERON PCU. LEAK CHECK AND OPS CHECK GOOD.Oct 4, 2020 · N529EA · Cndair CL6002C10 · Drag Control SystemSDR VNAA2020072411101Warning Message · false activationDURING APPROACH TO DCA THE CREW RECEIVED AN OB SPOILERON AND FLIGHT SPOILER CAUTION MESSAGE. THEY DECLARED AN EMERGENCY, LANDED SAFELY AND TAXIED TO THE GATE WITH NO ISSUES. TRUCKS ROLLED. PASSENGERS DID NOT BRACE. AIRCRAFT IS CURRENTLY WAITING FOR A MAINTENANJul 23, 2020 · N529EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA2019082915001Angle · crackedLBL 12 ANGLE IS CRACKED JUST FWD OF BS 280. REPAIREDTHE ANGLE IAW SRM 53-11-43.Aug 15, 2019 · N529EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA2019082915002Angle · crackedRBL 12 ANGLE IS CRACKED JUST FWD OF BS 280. REPAIRED RBL 12 IAW SRM 53-11-43.Aug 15, 2019 · N529EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA2019082614005Floorbeam · corrodedFLOORBEAM AT FS280.00 LEFT UPPER FLANGE IS CORRODED, BETWEEN UPPER L ANGLE DRIP TRAY. (FS280 CROSSBEAM)-C/A-REMOVED AND REPLACED LH FS280.00 CROSSBEAM IAW SRM 51-42-06 AND 51-42-13.Aug 14, 2019 · N529EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201908214004Floorbeam · corrodedFLOORBEAM AT FS280.OO RIGHT UPPER FLANGE IS CORRODED, BETWEEN UPPER L ANGLE DRIP TRAY. INSTALLED NEW RH FS280.00 CROSSBEAM IAW SRM 51-42-06 AND 51-42-13.Aug 14, 2019 · N529EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201908194003Crossbeam · corrodedLEFT HAND SIDE OF FS280. CROOSBEAM IS CORRODED AT WALL CONNECTION. (BULKHEAD REPAIR)-C/A-REMOVED AND REPLACED LHS LOWER BULKHEAD WEB AT FS-2800.00 IAW SRM 53-11-10 AND 51-42-06.Aug 14, 2019 · N529EA · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA201908163002Attach Angle · crackedLEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS AN APPROX. 1" CRACK EXTENDING FROM UNDER PREVIOUS REPAIR DOUBLER. REPAIRED LEFT VERTICAL STAB TO FUSEALGE ATTACH ANGLE IAW SRM 55-31-00.Aug 13, 2019 · N529EA · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA201908162002Floor Panel · crackedFWD EQUIPMENT COMPARTMENT FLOOR HAS AN 1/8" CRACK AT FS202.75 BY THE AFT CORNER OF CUTOUT FOR 211AL. REPAIRED LH FWD EQUIPMENT COMPARTMENT FLOOR IAW ETN-CR-53-099.Aug 12, 2019 · N529EA · Cndair CL6002C10 · Fuselage Floor PanelSDR SIMA201906110005Unknown · oscillatesMAX ABORT T.O AIRCRAFT OSCILLATING ABOVE 90-100 MPH, A/C PULLS TO THE RIGHT DURING TAXI. PERFORMED GVI OF MLG IAW AMM 32-11-00 PERFORMED OPS CHECK OF BRAKES IAW AMM 32-43-00.OPS CHECK GOOD. INSPECTED NLG TORQUE LINKS AND TIRES IAW CRJ 700 AMM 32-42-01 AND 32-Jun 10, 2019 · N529EA · Cndair CL6002C10 · Standard Practices/StructuresSDR SIMA201805165002Computer · inoperativeAT FLIGHT LEVEL AT FL270, STALL FAIL CAUTION POSTED. A SHORT TIME LATER A WARBLER TONE WAS HEARD. CA'S PFD SHOWED LOW SPEED RED RISING UP TO CURRENT SPEED OF 300. STICK SHAKER ACTIVATED AND STOPPED. ANOTHER ACTIVATION OF THE SHAKER HAPPENED AGAIN A MINUTE LATMay 15, 2018 · N529EA · Cndair CL6002C10 · Stall Warning SystemSDR SIMA20180111002Actuator · trippedSLATS FAIL CAUTION MESSAGE. THE SLAT ACTUATOR HAD TRIP INDICATORS. FOUND THE LT NR 6 AND RT NR 5 TRIPPED. RESET THE LT NR 6 IAW ETN-CR-27-084R8 BUT THE RT NR 5 INDICATOR WILL NOT RESET. AFTER FURTHER INSPECTION OF SLAT ACTUATOR TRIP INDICATORS FOUND THE LTJan 11, 2018 · N529EA · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR SIMA20170912003Door · out of adjustPAX DOOR WAS HARD TO CLOSE. WAS ABLE TO CLOSE IT. THEN ON ARRIVAL, HAD TO CYCLE THE HANDLE 5 TIMES TO GET DOOR TO OPEN. GROUND WAS UNABLE TO OPEN FROM OUTSIDE. GAVE PROX SYST 1 FAULT DURING THE PROCESS. AIRCRAFT HAD SIMILAR WRITEUPS IN THE PAST. ADJUSTED DOOSep 12, 2017 · N529EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170821001Acm · seizedF/A REPORTED A SMOKE ODOR IN CABIN DURING SHORT FINAL. COULDN`T DETERMAIN WHERE THE ODOR WAS FROM. AFTER TOUCHDOWN, THE RT PACK AUTOFAIL CAUTION MESSAGE APPEARED ON EICAS. TROUBLESHOT DISCREPANCY TO A SEIZED NR 2 ACM.Aug 21, 2017 · N529EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20170208002Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED, ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.Feb 8, 2017 · N529EA · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20170208001Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED APPROX. ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.Feb 8, 2017 · N529EA · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20161023003Lamp · inoperativeRT EXTERIOR EMERGENCY LIGHT JUST AFT OF EMERGENCY EXIT DOOR INOPERATIVE. REMOVED AND REPLACED THE LAMP.Oct 23, 2016 · N529EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20160515002Spoiler Sys · malfunctionedON APPROACH, INBD FLT SPLRS, & INBD SPOILERONS, CAUTION MSG POSTED UPON SELECTION OF THE FLIGHT SPOILER HANDLE. AOM VOL 1 EMER & ABNORMAL PROCEDURES COMPLIED WITH. INTERROGATED MDC FOUND LT INBD MFS PCU & PCU JAM MDC MSG. PERFORMED SPOST 1 RESET. PERFORMEDMay 15, 2016 · N529EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20160503005Frame · corrodedFRAME AT FS 295.00 IS CORRODED, BETWEEN STRINGERS 25 LT - 25 RT. REPAIRED FRAME AT FS 295, BETWEEN STRINGER 25 LT - 25 RT IAW ERS-CR-53MR-2078.May 3, 2016 · N529EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20160503004Panel · crackedPASSENGER DOOR AFT STEP SHELL SIDE PANEL HAS A CRACK BY SECOND STEP FROM BOTTOM WITH DOOR OPEN. REPAIRED IAW ERS-CR-5200-544.May 3, 2016 · N529EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160430005Marker · wornLEFT AFT AISLE EMER EXIT LIGHT RED MARKINGS ARE WORN OFF GOING INTO LT EMER EXIT SEATS. R & R LT AFT AISLE EMER EXIT LIGHT STRIP GOING INTO LT EMER EXIT SEATS IAW 33-51-01.Apr 30, 2016 · N529EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20160430004Skin · corrodedPASSENGER DOOR INNER SKIN HAS CORROSION ON LOWER EDGE WITH DOOR OPEN. REPAIRED CORROSION ON PAX DOOR INNER SKIN ALONG LOWER EDGE IAW SRM 52-00-01.Apr 30, 2016 · N529EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160412004Handle · lack of lubeREF ITEM 1 MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED MAIN DOOR HANDLE & PERFORMED OPERATIONS CHECK IAW AMM 52-11-03, FOUND WORKING GOOD.Apr 12, 2016 · N529EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160412003Door · stuckGATE AGENT REPORTS MAIN CABIN DOOR WILL NOT OPEN. PERFORMED GVI INSPECTION OF MAIN CABIN DOOR, FOUND DOOR TO NOT OPEN FROM OUTSIDE. VERIFIED DOOR OPERATION OF CABIN DOOR FROM INSIDE TO OPERATE NORMAL IAW AMM 52-11-00 REF ITEM 2.Apr 12, 2016 · N529EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160331005Pcu · failedOUTBOARD SPOILERS & OUTBOARD FLIGHT SPLRS, CAUTION MSG DISPLAYED IN DESCENT. TRANSFERRED TO NRWC 9 EACH ORD 01764. R & R MULTI-FUNCTION SPOILER PCU IAW AMM 27-62-01. OPERATIONS CHECKED GOOD.Mar 31, 2016 · N529EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20160310001Unknown · not reportedAIRCRAFT WILL NOT PRESSURIZE IN AUTO OR MANUAL MODE. COMPLIED WITH M PROCEDURE FOR MEL 21-6 & COMPLIED WITH PRESSURIZATION SYS. OPERATIONS CHECKED IAW AMM 21-31-00. FOUND SATISFACTORY AT THIS TIME.Mar 10, 2016 · N529EA · Cndair CL6002C10 · Cabin Pressure Control SystemSDR SIMA20160224001Actuator · failedMLG FAULT STATUS ON ED 2 FINAL APPROACH PREPARING TO LAND. TROUBLE SHOT IAW FIM 32-11-00-810-802. R & R LT MLG RETRACTION ACTUATOR IAW AMM 32-32-05. OPERATIONS & LEAK CHECKED GOOD.Feb 24, 2016 · N529EA · Cndair CL6002C10 · Landing Gear ActuatorSDR SIMA20160112001Sensor · defectiveBRAKE OVERHEAT, WARNING MSG OCCURRED AT ROTATION SPEED ON TAKEOFF. LT OTBD BRAKE TEMP CONTINUED RISING TO 18, BEFORE SLOWLY DROPPING BACK TO NORMAL. R & R THERMOCOUPLE SENSOR IAW AMM TASK 32-46-01. OPERATIONS CHECKED GOOD.Jan 12, 2016 · N529EA · Cndair CL6002C10 · Landing Gear Brake SystemSDR SIMA20150814003Warning System · false activationON APPROACH, DECLARED EMER DUE INBD FLIGHT SPOILERS & SPOILERONS CAUTION MSG. EMER DECLARED & LANDED SAFELY. INTERROGATED MDC FOUND LT INBD MFS PCU & PCU JAM WAS NOTED. PERFORMED SPOST 1 RESET & PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECAug 14, 2015 · N529EA · Cndair CL6002C10 · Drag Control System
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