N535EA

Service difficulty reports · 89

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 = 'N535EA' 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 SIMA20190925007Frame · gougedGOUGE ON STGR 6L 8.0" FWD OF FRAME FS1162 AND IS 3/8" WIDE AND THROUGH THE EDGE OF MATERIAL NEAR BEND RADIUS. "TRANSFERRED TO NRWC 535-MQT-02998" EDWARD LAKANEN 148836 UPGRADED TO A MAJOR REPAIR-C/A-REPAIRED DAMAGE IAW ERS-CR-53MR-3901, REF NRWC 535-MQT-02998Sep 25, 2019 · N535EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20190925006Frame · gougedGOUGE ON FRAME AT FS1162 BETWEEN STGR7L AND STGR8L. TRANSFERED FROM AML PAGE 4598770 BLOCK 2 T LEW 445258 MAJOR REPAIR-C/A-REPAIRED GOUGE ON FRAME AT FS1162 BETWEEN STR7L AND STR 8L IAW ERS-CR-53MR-1724.Sep 25, 2019 · N535EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20190925008Stringer · gouged"TRANSFERRED FROM AML PAGE 4598770 ITEM 3" GOUGE ON STGR7L 7 5/8" FWD OF FS1162 AND 5/8" IN WIDTH. DEPTH IS THROUGH RADIUS OF BEND, AND THROUGH EDGE OF MATERIAL. MAJOR REPAIR.-C/A-COMPLETED REPAIR ON STGR 7L FWD OF FS1162 IAW CRJ SRM 53-00-03.Sep 25, 2019 · N535EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA201908052001Panel · crackedAFT CARGO RH AFT WALL PANEL 282CRW HAS AN APPROXIMATELY 8" CRACKED. REPAIRED COMPOSITE DAMAGE ON AFT CARGO PANEL 282CRW IAW AMM 25-52-01.Aug 2, 2019 · N535EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190316003Sealant · unsecureRT (FO SIDE) OUTER WINDSHIELD SEAL STARTING TO COME OFF. C/A-PERFORMED GVI OF RT SIDE WINDOW FOUND SMALL AMOUNT OF FILLET SEAL TRIMMED EXCESS SEALANT REF. AMM 56-12-01 A/C OK FOR SERVICE.Mar 16, 2019 · N535EA · Cndair CL6002C10 · Flight Compartment WindowsSDR SIMA20180131001Packing · leakingSTEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT. UNABLE TO RECOVER AFTER LANDING. TROUBLESHOT IAW FIM 32-50-00-810-802. PERFORMED NLG STRUT REPACKING IAW W/C 32-019. OPS & LEAK CHECKED GOOD.Jan 31, 2018 · N535EA · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR SIMA20170918002Bulb · inoperativeDURING A PS-1 INSPECTION, FOUND THE RT AFT EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. R & R THE BULB IAW AMM 33-51-15. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.Sep 18, 2017 · N535EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20170905002Warning Message · false activationON APPROACH, DESCENDING FROM 6,000 FEET AND FLIGHT SPOILERS EXTENDED, OTBD SPOILERONS AND OTBD FLT SPOILER CAUTION MESSAGE POSTED ON ED1. INTERROGATED MDC FOUND LT OTBD MFS PCU JAM MDC MESSAGE. PERFORMED SPOST 1 RESET. PERFORMED OPS CHECK IAW ETN-CR-27-083. Sep 5, 2017 · N535EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20170524004Skin · dentedDENT FOUND ON THE FWD FUSELAGE AT BS 280 - 295, STRINGER 22 - 23R. PERFORMED A REPAIR IAW ERS-CR-53MR-2749.May 24, 2017 · N535EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20170508001Web · crackedLEFT FORWARD EQUIPMENT BAY FLOOR WEB HAS A .250 INCH CRACK. THE FLOOR WEB REPAIRED IAW ETN-CR-53-099.May 8, 2017 · N535EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20170201003Gauge · leakingFOUND NR 2 HYD SYS BRAKE ACCUMULATOR PRESSURE GAUGE LEAKING. REMOVED AND REPLACED THE PRESSURE GAUGE IAW AMM 32-43-30. OPS CHECKED GOOD.Feb 1, 2017 · N535EA · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20160914001Unknown · smokeSMOKE IN CABIN STARTED REAR, APU ON, PACKS OFF. GVI OF CABIN AND COCKPIT PERFORMED RAN APU ALL NIGHT WITH ALTERNATING PACKS OFF AND ON, LIGHTS OFF AND ON, NO INDICATION OF SMOKE OR ODOR OF IT. INSPECTED AVIONICS BAY APU COWL, ENGINE AND COWL NO OIL LEAK.Sep 14, 2016 · N535EA · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20160909004Profile · crackedRIGHT UPPER TRANSCOWL INBD PROFILE IS CRACKED. REPLACED THE PROFILE IAW ETN CR-54-051.Sep 9, 2016 · N535EA · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20160909001Stand Off · crackedRIGHT LOWER TRANSCOWL INBD PROFILE IS CRACKED. C/W INSTALLATION OF SERVICEABLE STAND OFF ANGLE IAW ETN CR-54-015R1.Sep 9, 2016 · N535EA · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20160908004Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1/2 INCH IN A PREVIOUSLY REPAIRED AREA ABOVE THE POWER ASSIST PULLEY BRACKET. C/W INSTALLATION OF SERVICESABLE STAND OFF ANGLE IAW ETN CR-54-015R1.Sep 8, 2016 · N535EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160908003Skin · crackedPASSENGER DOOR AFT SIDE SKIN HAS 2 CRACKS APPROXIMATELY 3" IN LENGTH AT THE MID STEP LOCATION. REPAIRED IAW ETN ETN-CR-52-039.Sep 8, 2016 · N535EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160905003Skin · dentedPASSENGER DOOR INNER SKIN HAS A DENT LOCATED BETWEEN FS 340-FS 349 & BETWEEN DOOR DATUM T/R 4 & 5. C/W ERS-CR-52DF-618 PART-A.Sep 5, 2016 · N535EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160809002Engine · vibrationN1 FAN VIBRATION REMAINED IN AMBER DURING CLIMBOUT. COULD NOT GET ENGINE BACK TO GREEN RANGE DURING CLIMB MODE. PERFORMED FIM TASK 72-00-00, & FOUND NO MESSAGES IN CURRENT FAULTS & FAULT HISTORY. PERFORMED INSPECTION OF THE FAN BLADES FOR STIFFNESS IAW 72Aug 9, 2016 · N535EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20160411004Cooling Fan · failedDISPLAY FAN FAILED, FOLLOWED BY BURNING SMELL IN COCKPIT. VERIFIED DISPLAY COOLING FAN NR 2 FAILED. SOURCE OF ODOR. DEFERRED COOLING NR 2. M PROCEDURE COMPLIED WITH. R & R NR 2 COCKPIT DISPLAY FAN IAW AMM 21-24-12. OPERATIONS CHECKED GOOD. MEL RESTORED.Apr 11, 2016 · N535EA · Cndair CL6002C10 · Air Distribution FanSDR SIMA20160409003Unknown · odorUPON START UP NOTICED ELEC SMOKE SMELL & SOUNDED LIKE DISPLAY FAN WINDING DOWN. PERFORMED OPERATIONS CHECK OF THE DISPLAY COOLING SYS IAW AMM 21-24-00. NO DEFECTS NOTED.Apr 9, 2016 · N535EA · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20160322002Flashlight · intermittentFIRST OFFICERS FLASHLIGHT WORKS INTERMITTENTLY, INDICATES CHARGING IN CRADLE. REPLACED FIRST OFFICERS FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.Mar 22, 2016 · N535EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20150116005Flashlight · inoperativeCOCKPIT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT IAW MM 25-61-02. OPERATIONS CHECKED GOOD.Jan 16, 2015 · N535EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20141201003Steering Sys · inoperativeSTEERING INOPERATIVE IN FLIGHT UPON GEAR DOWN SELECTION. COMPLIED WITH ETN-CR-019.Dec 1, 2014 · N535EA · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA20141005010Skin · crackedPASSENGER DOOR INNER SKIN AFT UPPER CORNER DENTED & CRACKED. REPLACED ANGLE UNDER CORNER IAW SRM 51-42-06 & INSTALLED NEW PAX DOOR AFT UPPER CORNER IAW SRM 51-42-13. DIAPHRAGM PN 601R38122-1.Oct 5, 2014 · N535EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20141005009Angle · crackedPASSENGER DOOR AFT STEP SHELL ANGLE ATTACHMENT CRACKED BY THE DOOR ASSIST PULLEY BRACKET. REPAIRED PAX DOOR AFT STEP ANGLE IAW SRM 52-11-04.Oct 5, 2014 · N535EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20141005001Support Bracket · crackedFAIRING SUPPORT BRACKET IN THE RT MAIN WW BELOW THE SIDE BRACE PINTLE PIN IS CRACKED. R & R WEB BRACKET IAW AMM 20-21-00.Oct 5, 2014 · N535EA · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20141005002Structure · crackedFORWARD RT ELEC COMPARTMENT FLOOR UNDER & OTBD OF THE ADG HYD HAND PUMP IS CRACKED. COMPLETED REPAIR IAW ETN-CR-53-099.Oct 5, 2014 · N535EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140624005Autopilot Sys · malfunctionedIN CRUISE AT FL190 AUTO PILOT ENGAGED. AUTO PILOT LAGGED FLIGHT DIRECTOR RESULTING IN 400 FPM CLIMB & 500 FPM OSCILLATIONS, FROM CAPTURED ALTITUDE, 1/8 INCH GAP BETWEEN FLIGHT DIRECTOR & ACFT SYMBOL. LEVELED AT 2100 FT ON APPROACH & AGAIN WITH GLIDESLOPE CAPJun 24, 2014 · N535EA · Cndair CL6002C10 · Autopilot SystemSDR SIMA20140607005Pcu · malfunctionedINBOARD FLT SPOILERS & IB SPOILERONS MSG PRESENTED IN FLIGHT. TRANSFERRED TO NRWC 535-ORD-01112. R & R MFS PCU RT INBD IAW AMM TASK 27-62-01. OPERATIONS CHECKED GOOD. RETURN ACFT TO SERVICE.Jun 7, 2014 · N535EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20140531002Pcu · malfunctionedAT 11,000 FT, DEPLOYED FLIGHT SPOILERS. INBD FLT SPOILERS & INBD SPOILERONS ILLUMINATED ON EICAS. REMOVED AND REPLACED RT INBD PCU IAW AMM 27-62-01.May 31, 2014 · N535EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20140519002Warning System · false activationINBD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSG DURING ARRIVAL TO APPROACH. PERFORMED SPOST 1 & 2 TEST IAW AMM 27-40-00 FIM 27-41-00. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.May 19, 2014 · N535EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20140507002Transceiver · defectiveCLIMB OUT OF LGA GLD UNSAFE EICAS CAUTION PRESENTED. COMPLIED WITH EMER & ABNORMAL CHECKLIST, RETURNED TO LGA & LANDED UNEVENTFULLY. R & R NR 2 A43 RADIO ALTIMETER TRANSCEIVER IAW AMM 34-44-01, OPERATIONS TESTED GOOD.May 7, 2014 · N535EA · Cndair CL6002C10 · Ground Proximity SystemSDR SIMA20140328012Flashlight · malfunctionedCAPTAIN`S FLASHLIGHT RED INDICATOR LIGHT MISSING. PERFORMED OPERATIONAL CHECK OF CAPTAIN'S EMERGENCY FLASHLIGHT IAW MM 25-61-02. OPS CHECKED GOOD.Mar 28, 2014 · N535EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20131027006Acm · failedON GROUND, PARKED AT GATE, APU RUNNING. TURNED ON LT & RT PACKS. SMOKE BEGAN COMING FROM VENTS IN COCKPIT AND LT PACK AUTOFAIL CAUTION MESSAGE WAS PRESENTED. REMOVED AND REPLACED THE LEFT HAND AIR CYCLE MACHINE ASSY. IAW MM 21-51-08 -PERFORMED OPS TEST OFOct 27, 2013 · N535EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20131016001A/C Pack · seizedCREW REPORTED DIRTY SOCK ODOR FROM RT PACK. FOUND RT PACK SEIZED.Oct 16, 2013 · N535EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20130920005Flashlight Assy · inoperativeCAPTAIN`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW 65-08-12. OPS CHECKED GOOD.Sep 20, 2013 · N535EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20130601009Printer · malfunctionedTHE CREW REPORTED A COCKPIT ODOR. THE ACFT WAS REMOVED FROM SERVICE, MEL 23-06. R & R PRINTER IAW MM 23-22-05. THE OPS CHECK WAS GOOD. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.Jun 1, 2013 · N535EA · Cndair CL6002C10 · Data Transmission Auto CallSDR SIMA20130322004Warning System · malfunctionedON FLIGHT 3743 THE CREW REPORTED THAT UPON DESCENT THEY RECEIVED AN EICAS I/B SPOILERON AND I/B FLT SPOILERS FAULT MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. Mar 21, 2013 · N535EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA201032703Thrust Reverser · malfunctionedON FLIGHT 3877 ON THE LANDING ROLL OUT THE CREW TRIED TO STOW THE THRUST REVERSERS BUT THE LEFT REVERSER STAYED DEPLOYED. THE CAPTAIN DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE.Nov 17, 2010 · N535EA · Cndair CL6002C10 · Engine Thrust Reverser
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