N524AE

Service difficulty reports · 131

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 = 'N524AE' 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 VNAA2026052018201Ballast · unserviceableBURNING ODOR COMING FROM OVERHEAD BIN VENT 1-3A. PERFORMED ABNORMAL SMELL IN CABIN INSPECTION IAW FIM 21-22-00-810-806. SIDEWALL LIGHTS OVER SEATS 2 AND 3 ARE OUT AND WITH RECERT FAN OFF SMELL DECREASED SIGNIFICANTLY. REMOVED AND REPLACED BOTH BALLAST OVER SEMay 18, 2026 · N524AE · Cndair CL6002C10 · Passenger Compartment LightingSDR VNAA2024122711101Acm · unserviceableTHE CREW REPORTED THERE WAS A BURNING SMELL IN THE COCKPIT (NO SMOKE NOTED) WITH A SLIGHT HAZE IN THE CABIN WHILE BOARDING. THE EVENT LASTED BETWEEN 5 TO 10 MINUTES AND THERE WAS NO MEDICAL ATTENTION REQUIRED. / REMOVED AND REPLACED RH ACM IAW AMM 21-51-08-000Dec 23, 2024 · N524AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2024082711105Window · unserviceableR SIDE WINDOW ARCING / INSTALLED FLIGHT COMPARTMENT RH SIDE WINDOW IAW CRJ700 AMM 56-12-01-400-801-A01-PSA. LEAK CHECK AND OPERATIONAL TEST OF WINDOW TEMP CONTEROLLER IAW CRJ700 AMM 21-31-00-910-801-A01 AND AMM 30-41-06-710-801-A01 RESPECTIVELY. ALL CHECKS GOAug 25, 2024 · N524AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA20230829018Intercostal · corrodedSTGR 21L INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND FS 333.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2023082919Intercostal · corrodedSTGR 21L INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND FS 333.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308290018Seat Track · corrodedCORROSION FOUND ON RBL 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202308290017Seat Track · corrodedCORROSION FOUND ON LH SIDE SEAT RAIL BETWEEN FS 379.00-485.00Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202308290016Striker · dentedPAX DOOR LOWER SURROUND IS DENTED IN MULTIPLE PLACESAug 29, 2023 · N524AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202308290015Stringer Clip · corrodedSTR CLIP CORRODED AT F.S.586 AND STR 25L.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202308290014Plate · corrodedFORWARD BAGGAGE BAY DOOR SILL AFT JOINT PLATE AT F.S.533 HAS 2 CORRODED FASTENERS.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308290013Plate · corrodedFORWARD BAGGAGE BAY DOOR SILL FORWARD JOINT PLATE AT F.S.533 HAS 7 CORRODED FASTENERS.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308290012Stringer · corrodedSTGR 27 IS CORRODED BETWEEN FS 310 AND FS 319.70.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308290011Skin Splice · corrodedSKIN SPLICE STRAP IS CORRODED AT FS 333 BETWEEN STGR 27 AND STGR 26R.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202308290010Attach Angle · corrodedFS 280 FWD ANGLE ATTACHING TO THE CROSSBEAM IS CORRODED AT RBL 4.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202308290009Intercostal · corrodedINTERCOSTAL AT RBL 2 IS CORRODED BETWEEN FS 349 AND FS 364.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308290008Intercostal · corrodedINTERCOSTAL AT STGR 26R IS CORRODED BETWEEN FS 349 AND FS 364Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308290007Joint · corrodedF.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24L AND STGR 23L.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202308290006Angle · corrodedCORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202308290005Angle · corrodedCORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202308290004Angle · corrodedCORROSION FOUND ON PAX DOOR LOWER SILL ANGLE.Aug 29, 2023 · N524AE · Cndair CL6002C10 · DoorsSDR VNAA202308290003Vane · chafedRH I/B FLAP VANE LEADING-EDGE IS CHAFED AT W.S. 48.95 APPROXIMATELY 8" LONG AND .008" DEEP.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202308290002Skin · chafedRH I/B FLAP VANE LEADING-EDGE IS CHAFED AT W.S. 48.95 APPROXIMATELY 8" LONG AND .008" DEEP.Aug 29, 2023 · N524AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202308290001Seat Track · corrodedCORROSION FOUND ON RBR 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202308290019Seat Track · corrodedCORROSION FOUND ON RBR 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202308280035Striker · corrodedGALLEY DOOR LOWER SEAL RETAINER IS CORRODED AROUND SCREW HOLES ON THE AFT SIDEAug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308280034Fitting · gougedFWD BAGGAGE BAY DOOR AFT HINGE IS GOUGED.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202308280020Frame · corrodedFS 379 FRAME IS CORRODED BETWEEN STR 20R AND 21RAug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202308280021Stringer · corrodedSTGR 26R IS CORRODED BETWEEN FS 295 AND FS 310.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280022Seat Track · corrodedCORROSION FOUND ON RBL 9 FLOOR SEAT RAIL BETWEEN FS 485.00-581.00.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202308280023Stringer Splice · corrodedSTGR 25R SPLICE IS CORRODED AT FS 333.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280026Stringer Splice · corrodedSTGR 25R SPLICE IS CORRODED AT FS 333.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280025Door Sill · corrodedAFT CARGO BAY DOOR SILL IS CORRODED BETWEEN FS 1000 AND FS 1047 AT WL 72.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308280024Angle · corrodedCORROSION FOUND ON GALLEY SERVICE DOOR LOWER SILL ANGLE.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202308280027Stringer · gougedNICK/GOUGE ON STGR 24L BETWEEN FS 645 AND FS 661Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280028Fitting · corrodedL/H I/B FLAP HINGE ARM FITTING LUGS AT WS 54.55 ARE GOUGEDAug 28, 2023 · N524AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202308280029Stringer · corrodedSTGR 25R IS CORRODED BETWEEN FS 280 AND FS 333.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280030Stringer · corrodedUPON REMOVING STRINGER 21R FORWARD FS 333 TO FS 477 FOUND THE STRINGER TO HAVE EXTREME EXFOLIATION IN MULTIPLE SPOTS.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280031Stringer · corrodedUPON REMOVING STRINGER 21R FORWARD FS 333 TO FS 477 FOUND THE STRINGER TO HAVE EXTREME EXFOLIATION IN MULTIPLE SPOTS.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202308280032Skin · dentedEA21-C7-53-287_REV-D (PERM REPAIR - FUSELAGE SKIN PANEL - FS509, STR16L) 1.WITHIN 1,500 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR ATDISCREPANT AREA INACCORDANCE WITH APPROVED PROCEDURES.2. PERFORM ULTRASONIC THICKNESS (UT) INSPECTION PER NDTMAug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202308280033Skin · dentedEA21-C7-53-287_REV-D (PERM REPAIR - FUSELAGE SKIN PANEL - FS509, STR16L) 1.WITHIN 1,500 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR ATDISCREPANT AREA INACCORDANCE WITH APPROVED PROCEDURES.2. PERFORM ULTRASONIC THICKNESS (UT) INSPECTION PER NDTMAug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA2023082800033Skin · damagedAFT CARGO DOOR, AFT UPPER CORNER: THE CABLE HAS SPLIT THE PULLEY IN HALF, CAUSING THE CABLE TO SAW-TOOTH INTO THE UPPER CROSSBEAM.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202308280002Skin · damagedLEADING EDGE 522AL HAS ONE DAMAGED FASTENER COUNTERSINK ON THE LOWER LEADING EDGE AT WS 178.00.Aug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202307020001Skin · gougedLH LEADING EDGE PANEL (FIXED UPPER SKIN) 521AT WAS FOUND TO HAVE GOUGEJul 2, 2023 · N524AE · Cndair CL6002C10 · Wing StructureSDR VNAA202207111111Trim Panel · unserviceableFLIGHT RETURNED TO FIELD AFTER TAKEOFF. CREW DISCOVERED THAT AILERON AND RUDDER TRIM WERE DEFLECTING SEVERELY TO THE LEFT. CREW THEN CONTACTED ATC AND DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY AND TAXIED BACK TO GATE. CREW REPORTS LANDING OVERWEIGHT. CABIN WJul 8, 2022 · N524AE · Cndair CL6002C10 · Flight Control SystemSDR VNAA2021010321111Ballast · failedFA REPORTED BURNING SMELL AT ROW 16,17 / TRACED ODOR TO BALLAST OF 16DF SIDEWALL LIGHTS. R/R 16 DF SIDEWALL LIGHT BALLAST IAW CRJ700 AMM 33-21-09-000/400-801. OPS AND SMELL TEST GOOD.Dec 30, 2021 · N524AE · Cndair CL6002C10 · Passenger Compartment LightingSDR VNAA202104081111Slat · damagedDURING ROUTINE MAINTENANCE, TECHNICIANS REPORT THE LH #2 SLAT (P/N: CC670-12700-1, S/N: UNKNOWN) HAS A CHIP MISSING (DAMAGE #1) IN THE TRAILING EDGE (P/N CC670-12742-1) AT APPROXIMATELY SLAT STATION 249 MEASURING .28Ï¿½ WIDE X .22Ï¿½ DEEP. THE CORNERS OF THE CApr 4, 2021 · N524AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202103081111Skin · dentedDURING OVERNIGHT MAINTENANCE, A DENT WAS DISCOVERED ON THE RH FUSELAGE SKIN JUST FORWARD OF FS 220 ABOVE THE RH PITOT PROBE BETWEEN STGR 13A AND 14A. THE DENT MEASURES 2.05Ï¿½ X 2.0Ï¿½ X 0.016Ï¿½ DEEP AND IS NOT WITHIN ALLOWABLE DAMAGE LIMITS DUE TO EDGE OF DEMar 4, 2021 · N524AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2020100211101Battery · dischargedNR 4 EMERGENCY BATTERY NOT SUPPLYING VOLTAGE TO LT EXTERIOR AFT EMERGENCY LIGHT. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY. OPERATIONS CHECK GOOD AT THIS TIME.Oct 2, 2020 · N524AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019100111102Bulb · inoperativeMX FOUND LEFT AND RIGHT OVER WING EXITS LOWER SIGNS HAS A LIGHT NOT ILLUMINATING. RELAMPED RIGHT AND LEFT OVER WING EXIT LOWER SIGN BULBS , OPS CHECKS GOOD.Oct 1, 2019 · N524AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019100111101Lamp · inoperativeMX FOUND AT SEAT 14 EMERGENCY OVERHEAD LIGHT WILL NOT ILLUMINATE.RELAMPED SEAT 14 OVERHEAD EMERGENCY FLOOD LAMP , OPS CHECKS GOOD IAW CRJ 700 AMM 33-51-09-000-801/400-801.Oct 1, 2019 · N524AE · Cndair CL6002C10 · Emergency Lighting
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