N500AE

Service difficulty reports · 181

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 = 'N500AE' 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 VNAA202604010059Seat Track · corrodedLBL 9 SEAT RAIL BETWEEN FS 581 AND FS 693 HAS GOUGES. REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202604010060Seat Track · corrodedHN00250014 DISCREPANCY: RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 847 AND FS 977. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 850.55-977.00 IAW CRJ 700 AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01.Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202604010009Seat Track · corrodedLEFT SIDE SEAT TRACK AT BS 838 - 879 IS CORRODED. REMOVED AND REPLACED SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A01.Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202604010061Strap · corrodedFOUND CORROSION ON STRAP AT LBL45 AROUND FASTENER HOLES AT F.S.847. REMOVED AND REPLACED NEW FS 847 LBL 45 FAIRING SUPPORT STRAP PN# SH670-39166-5 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-45-00-001-001-A01 & 51-23-00-001-001-A01.Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202604010008Floorbeam · corrodedPAX DOOR SURROUND FLOORBOARD SUPPORT ANGLE HAS CORROSION IN MULTIPLE AREAS BETWEEN FS310-FS349. REMOVED CORRODED ANGLE.LOCATED, DRILLED AND INSTALLED NEW SERVICABLE KICK PLATE ANGLE [P/N SH670-31875-3] IAW CRJ 700 SRM 51-40-11-001-001-A01AND 51-42-06-001-001Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202604010007Floorbeam · crackedO/B SIDE OF LH FLIGHTDECK FLOORBEAM FWD OF FS280 IS CRACKED. COMPLIED WITH REPAIR TO O/B SIDE OF LH FLIGHTDECK FLOOR BEAM AT FS. 280 MHIRJ REO 670-53-11-896 REV-- DATED 2015-03-17. REFERENCE ABOVE STEPS FOR DETAILS OF WORK PERFORMED.Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202604010006Floorbeam · crackedO/B SIDE OF RH FLIGHTDECK FLOORBEAM FWD OF FS280 IS CRACKED. COMPLIED WITH REPAIR TO O/B SIDE OF RH FLIGHTDECK FLOOR BEAM AT FS. 280 MHIRJ REO 670-53-11-896 REV-- DATED 2015-03-17. REFERENCE ABOVE STEPS FOR DETAILS OF WORK PERFORMED.Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202604010005Floorbeam · corrodedTHE LEFT HAND F.S.280 CROSS BEAM AND CORROSION CAP ANGLE HAS ELONGATED AND DOUBLE DRILLED HOLES AND IS DENTED ON THE UPPER INBOARD SURFACE. REPLACED FS. 280 LH CROSSBEAM PN CC670-34094-1, IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-22-00Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202604010004Floorbeam · corrodedWHILE ACCESSING O/B SIDE OF RH FLIGHTDECK FLOOR BEAM AT FS280 FOUND FS. 280 CROSSBEAM TO BE CORRODED REPLACEMENT REQUIRED. CORRECTIVE ACTION: REPLACED FS. 280 RH CROSSBEAM PN CC670-34094-2S, IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-22-0Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202604010003Hinge Arm · corrodedLH OB FLAP HINGE ARM AT W.S. 178.00 FOUND TO HAVE CORROSION INSIDE BORE OF AFT FASTENER HOLE CORRECTIVE ACTION: REPLACED UNSERVICEABLE LH FLAP HINGE ARM AT WS178.00 (PN:601R14551-3 SN:UNK) WITH NEW SERVICEABLE FLAP HINGE ARM (PN:601R14551-3 SN:25-00775).Apr 1, 2026 · N500AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202604010002Trunnion · corrodedCO# 10025725 BARCODE: HN00248926 DISCREPANCY: L/H MLG TRUNNION FAILED NDT. CORRECTIVE ACTION: REPAIRED LH MLG TRUNNION, FWD BEARING LUG FACE IAW MHIRJ REO 670-57-21-1066 REV A DATED 2026-02-12. CC670-10631-3Apr 1, 2026 · N500AE · Cndair CL6002C10 · Wing, Landing Gear Attach FittingsSDR VNAA202604010001Trunnion · corrodedR/H MLG TRUNNION FAILED NDT. CORRECTIVE ACTION: REPAIRED RH MLG TRUNNION, FWD BEARING LUG FACE IAW MHIRJ REO 670-57-21-1066 REV A DATED 2026-02-12. CC670-10631-3Apr 1, 2026 · N500AE · Cndair CL6002C10 · Wing, Landing Gear Attach FittingsSDR VNAA202307141111Wheel · unserviceableRIGHT SIDE MAIN OB TIRE BOLT MISSING AND SAFETY WIRE / REMOVED AND REPLACED RH OB MLG TIRE IAW CRJ 700 AMM 34-41-01-000/400-801-A01-PSA. NO DEFECTS NOTED.Jul 13, 2023 · N500AE · Cndair CL6002C10 · TireSDR VNAA202304191112Unknown · unknownPAX DOOR HINGE PIN SPRING PIN (P/N MS16562ˆ’212) WAS FOUND TO BE PROTRUDING FROM THE PIANO HINGE AND ROTATED CAUSING A .050€? GOUGE IN THE LUG LAND. / COMPLETED PERMANENT REPAIR OF THE GOUGE ON THE PASSENGER DOOR PIANO HINGE IAW CRJ 700 SRM 53-21-23-201-010-Apr 17, 2023 · N500AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202211101111Fadec · unserviceableL FADEC FAULT CAUTION MSG. REMOVED AND REPLACED LH FADEC IAW CRJ 700AMM 73-21-01-000/400-801. OPS CHECK GOOD. NO CAUTION MSGS.Nov 4, 2022 · N500AE · Cndair CL6002C10 · Fuel Controlling SystemSDR VNAA202111291111Fastener · shearedSHEARED FASTENER LOCATED BETWEEN FS169.00 - FS173.00 AND AT WL79.50. DURING REMOVAL OF DAMAGED FASTENER, A MISS DRILLED HOLE WAS DONE COMMON TO ANGLE ACCESS DOOR (DWG CC670-33422, REF) AND MACHINED BULKHEAD FS169.00 (DWG: CC670-34204, FLANGE NOM THK OF 0.063",Nov 25, 2021 · N500AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202104271111Control Unit · unserviceableSPOILER/STAB FAULT MESSAGE AND FLAPS/SLATS OVERSPEED MESSAGE ON TAKE-OFF. OVERSPEED CLACKER BEGAN GOING OFF AFTER THE ZERO POSITION WAS SUPPOSEDLY REACHED AND CREW MADE THE DECISION TO DIVERT / INTERROGATED THE MDC AND FOUND B1 CODE 008026. REMOVED AND REPLACApr 23, 2021 · N500AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA202011239996Stringer · corrodedSTR 21 RT CORRODED BETWEEN FR AT FS 295.00 AND FR AT FS310.00, FOUND DURING CLEARANCE TO CLOSE OF FLOOR PANEL.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202011239995Stringer · corrodedSTRINGER 25 RIGHT AND STRINGER 26 RIGHT HAS EVIDENCE OF CORROSION BETWEEN FS 280.00 AND FS 310.00.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202011239994Skin · chafedREPAIR DOUBLER BETWEEN FS 969.00-958.00 AND STRINGER 26L-26R IS CHAFED.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202011239993Door Sill · corrodedSERVICE DOOR SILL BETWEEN FS 319.70-349.00 IS CORRODED.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202011239992Intercostal · corrodedINTERCOSTAL BETWEEN FS 349.00-364.00 AND STRINGERS 27-26R IS CORRODED.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202011239991Frame · damaged670-53-61-1514. PERMANENT REPAIR FOR DAMAGE TO FRAME AT FS-1144, BETWEEN STR 8-9R0. PERMANENT REPAIR OF DAMAGE TO FRAME AT FS 1144 BETWEEN STR 8-9R.Nov 23, 2020 · N500AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020051711101Printed Ckt Board · failedEMER LIGHTS FLICKERING WHEN FLIGHT DECK SWITCH ARMED - REMOVED & REPLACED PCB5 IN JB11 IAW CRJ700 AMM 24-06-11-000/400-801 OPS CHECK GOOD.May 16, 2020 · N500AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2020022911101Unknown · noisyWE HEARD A LOUD SQUEALING NOISE THAT TURNED INTO A HUMMING RUBBING NOISE THAT TURNED INTO A LOUD FLAPPING SOUND THAT SLOWED DOWN WITH THE DECELERATION OF THE NOSE TIRE. DECLARED EMERGENCY AND DIVERTED TO CLT. MX INSPECTED MLG & NLG TIRE WEAR AND TEAR & WHEEL AFeb 29, 2020 · N500AE · Cndair CL6002C10 · Landing Gear SystemSDR VNAA2019121431101Connector · damagedDAMAGED ELECTRICAL CONNECTOR FOR EMERGENCY LIGHT #4 (DS144) EA74-2019-019 DEFERRED LIGHT. INSTALLED NEW PINS ON #4 CABIN EMERGENCY LIGHT IAW ESPM 20-16-00. OPS CHECK GOOD IAW AMM 33-51-00-710-801-A01. THIS CLEARS MELDec 13, 2019 · N500AE · Cndair CL6002C10 · Light System WiringSDR VNAA2019102999901Hinge · damagedPAX DOOR HINGE HAS GOUGE AT AFT LUG LAND FROM MIGRATED PIN. REMOVED PASSENGER DOOR IAW CRJ700 AMM 52-11-00-000-801-A02. 1. INSTALLED SAME SERVICEABLE PAX DOOR IAW CRJ700 AMM 52-11-00-400-801-A02. RIG CHECK, CLEARANCE CHECK AND OPS CHECK GOOD. 2. N/A C/A: 2. REOct 29, 2019 · N500AE · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA2019100192102Battery Pack · inoperativeEMERGENCY LIGHTS POWERED BY #4 BATTERY PACK DO NOT ILLUMINATE. REMOVED AND REPLACED #4 EMERGENCY BATTERY PACK IAW CRJ 700 AMM 33-51-17-000/400-801(A01). OPS. CHECK GOOD AT THIS TIMESep 25, 2019 · N500AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019072111101Warning System · false activationCREW RECEIVED AN OUTBOARD SPOILERON CAUTION MESSAGE AS A PRECAUTION THEY DECLARED AN EMERGENCY INTO CAE. FLIGHT LANDED SAFELY IN CAE WITHOUT ANY FURTHER ISSUES. THE CREW WAS ABLE TO TAXI THE AIRCRAFT TO A GATE UNDER THEIR OWN POWER. C/W SYSTEM RESET 1-3. RESETJul 21, 2019 · N500AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2019051699903Former · crackedPAX DOOR FORMER FS 347.25 AT DOOR DATUM 4 IS UNSERVICEBALE REPAIR IS REQUIRED. RIVETS ARE PULLING LOOSE SKIN FROM FORMER & PERFORMED EDDY CUURENT INSPECTION OF SUSPECTED CRACKED AREAS ON PAX DOOR INNER SKIN AND AFT FORMER IAW NDTM PART 1, 51-20-006-250-A01. FOMay 16, 2019 · N500AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2019051699902Stiffener · crackedDURING INSTALLATION OF THE RT FS280.00 BEAM, FOUND THE STIFFENER ON THE FWD SIDE OF THE FS280.00 AT RBL26.00 TO BE CRACKED AT THE LOWER END, REQUIRES REPLACEMENT. C/A: LOCATED, AND DRILLED NEW STIFFENER PART CC670-34117-2 IAW SRM 51-40-11-001-001-A01.May 16, 2019 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019051699901Beam · corrodedFS280 BEAM TOP FLANGE (MPN CC670-34175-3) AND FWD J-ANGLE (MPN CC670-34095-1) AT COCKPIT THRESHOLD ARE CORRODED BEYOND LIMITS (EXFOLIATION). C/A: COMPLIED WITH SERVICE BULLETIN 670BA-53-041 REV.F, PART A - CENTER FUSELAGE FS 280 TO FS 477 - REINFORCEMENT OF THMay 16, 2019 · N500AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2019031111101Relay · faultyEMERGENCY LIGHTS FLICKER ON/OFF IN THE ARMED POSITION. R/R K135 RELAY ON JB-11 PCB5 IAW CRJ 700 AMM 24-06-11-000/400-801. EMERGENCY LIGHTS OPS CHECK GOOD.Mar 11, 2019 · N500AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2017090611102Warning Message · false activationDURING DESCENT AT APPROXIMATELY 9000 FEET, THE CREW RECEIVED AN INBOARD SPOILERS, INBOARD SPOILERON CAUTION MESSAGE. ATC DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MX RAN SPOST 2, OPS CHECKED GOOD.Sep 6, 2017 · N500AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2017051100005Warning Message · illuminatedGEARS DISAGREE WARNING, AN EMERGENCY WAS DECLARED.May 11, 2017 · N500AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2017011300013Warning Message · activatedGEAR DISAGREE WARNING MESSAGE.Jan 13, 2017 · N500AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2017010400001Selector Valve · leakingGEAR DISAGREE WARNING AFTER TAKE OFF. REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE.Jan 4, 2017 · N500AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2016120300006Proximity Sensor · out of adjustLEFT EMERGENCY DOOR CAUTION MESSAGE. ADJUSTED THE LEFT OVERWING EXIT DOOR PROXIMITY SENSOR.Dec 3, 2016 · N500AE · Cndair CL6002C10 · Door Warning SystemSDR VNAA2016111500022Warning Light · false activationLEFT OVERWING EMERGENCY EXIT INDICATION SYSTEM INOPERATIVE, LEFT EMERGENCY DOOR AMBER CAUTION MESSAGE AT THE GATE. MAINTENANCE COMPLIED WITH OPS CHECK OF EMERGENCY DOOR WARNING SYSTEM IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.Nov 15, 2016 · N500AE · Cndair CL6002C10 · Central WarningSDR VNAA2016110600008Stringer · corrodedSTRINGER 26L CORRODED BETWEEN BS 280 AND 319. MAINTENANCE REMOVED AND REPLACED STRINGER AND PERFORMED CHECKS IAW THE AMM.Nov 6, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2016110500007Frame · chafedBS 1144 FRAME CHAFED AT WL BETWEEN STRINGERS 8 AND 9R. MAINTENANCE REPAIRED THE FRAME AND PERFORMED CHECKS IAW THE AMM.Nov 5, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016110200004Frame · corrodedLOWER FRAME SEGMENT AT BS 319 CORRODED BETWEEN STRINGER 25L AND STRINGER 25R. MAINTENANCE REMOVED AND REPLACED THE LOWER FRAME SEGMENT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY MAINTENANCE CHECKS.Nov 2, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016110200003Floor Support · corrodedRIGHT HAND FLOOR SUPPORT CORRODED FROM BS 349 TO 364. MAINTENANCE REPAIRED THE FLOOR SUPPORT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY MAINTENANCE CHECKS.Nov 2, 2016 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016110200002Stringer · corrodedBS 319 TO 310 STRINGER 27 IS CORRODED. MAINTENANCE REPLACED THE STRINGER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.Nov 2, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2016103000040Stringer · corrodedBS 280 TO 295 STRINGER 25L CORRODED. MAINTENANCE REMOVED AND REPLACED THE STRINGER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 30, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2016103000039Angle · corrodedPASSENGER DOOR LOWER SILL UPPER ANGLE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ANGLE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.Oct 30, 2016 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016103000038Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AND PERFORMED CHECKS IAW THE AMM.Oct 30, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2016102800035Skin · dentedRIGHT INBOARD FLAP BOTTOM SKIN HAS THREE DENTS. MAINTENANCE REPAIRED THE DENTS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.Oct 28, 2016 · N500AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA2016102800034Angle · corrodedBS 280 J ANGLE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD J ANGLE.Oct 28, 2016 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016102800033Bulkhead Web · corrodedBS 280 LEFT AND RIGHT WEBS CORRODED BETWEEN LBL - RBL 9 AND LBL-RBL 18. MAINTENANCE PERFORMED A MAJOR REPAIR TO BULKHEAD LOWER WEB, FS 280 LHS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECKS MAINTENANCE.Oct 28, 2016 · N500AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
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