N543EA

Service difficulty reports · 71

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 = 'N543EA' 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 VNAA2025021011102Dcu · unserviceableON DESCENT BURNING SMELL CBP2 Q2 POPPED. DCU AURAL INOP STATUS MESSAGE. THERE WAS NO MEDICAL ATTENTION REPORTED / INSPECTED FOR SMOKE ODOR ON FLIGHT DECK IAW FIM 21-21-00-810-806-A01. SUSPECT DCU 2 AND DCU CONTROL PANEL AS CAUSE OF ODOR. REMOVED AND REPLACED DFeb 6, 2025 · N543EA · Cndair CL6002C10 · Central ComputersSDR WRXR20241115003Floor Support · corroded3 AREAS OF PITTING CORROSION IN 2.5" X 1.5" AREA AT LBL 27/ FS 1031. PERFORMED FLOOR BEAM SPLICE REPAIR FOR SECTION FS 1031 TO FS 1060 LBL27 IAW CRJ700 SRM 53-00-41-201-001-A01 COMPLIED WITH REO 670-53-61-2389 DEVIATION TO SRM FLOOR BEAM SPLICE REPAIR (TASK 53Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241115002Skin · dentedWO DENTS FOUND AT F.S. 985 AT BOTTOM CENTERLINE. FWD DENT 1 1/4" X 1 9/16" X .041 DEEP, AFT DENT 1 3/16" X 1 1/2" X .085" DEEP. CUT DAMAGE 2 PLACE BETWEEN FS 969.00 - FS 985.00 STGR 2. FABRICATED TOP AND BOTTOM DOUBLERS (2EA) FROM 2024-T3 .063 LOT # 459396B8, Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WRXR202411150001Skin · dentedMULTIPLE DENTS LOCATED ON THE LOWER SKIN PANEL AT FS 1015 TO FS 1031 BETWEEN STR22R TO STR24R. COMPLETED REPAIR OF ALL AREAS IAW REO 670-53-61-2400 REV --.Nov 15, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WRXR20241103001Door · damagedPERM REPAIR BEFORE 29,283.37 FH - LH NLG SURROUND DOUBLER. REMOVED AND REPLACED DOUBLER IAW BOMBARDIER DRAWING CC670-32010 REV F, SECTION III - PERMANENT REPAIR OF OLIVER WYMAN EA 22-C7-53-1311 REV. A.Nov 3, 2024 · N543EA · Cndair CL6002C10 · Landing Gear DoorsSDR WRXR20241018001Beam · mechanic errorQTY (1) BLENDED AREA OF MISDRILLED DAMAGE TO RBL 36.00 PRESSURE SILL BEAM WEB (DWG SH670-36180, AL ALY 2024-T3511, S8347AA EXTRUSION, 0.090" NOM. THK, REF) BETWEEN FS785.00 AND FS797.00. COMPLETED LPI (FLUORESCENT) PER NDTM 51-20-008 OR EDDY CURRENT INSPECT PEOct 18, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, StructureSDR WRXR20241017001Fitting · gougedGOUGES ON RH MLG SIDE-STAY FITTING PN:CC670-10608 BETWEEN RBL 22.5 AND RBL 45.0 INBD. GOUGE (A)MEASURES ROUGHLY .3" X .1" AND THE O/B GOUGE (B) MEASURES .2" X .1". BLENDED DAMAGED AREA IAW PSA EA A1-670-32-00008 STEPS 1-4. ROTO-PEEN REWORKED ARA IAW CRJ700 SRMOct 17, 2024 · N543EA · Cndair CL6002C10 · Main Landing GearSDR WRXR20241016001Frame · corrodedCORROSION FOUND ON FRAME F.S 310.00 IN BETWEEN L/H STRGR #22 TO R/H STRGR #22. REMOVED AND REPLACED FRAME SECTION FS310.00 AT AND BETWEEN 25L AND 25R IAW CRJ700 SRM 53-00-06-201-006-A01.Oct 16, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, FrameSDR WRXR20241011002Skin · gougedMULTIPLE GOUGES ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27. BLENDED AREAS A-G TO A 20:1 RATIO ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27 IAW REO 670-53-61-2384 REV--.Oct 11, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WRXR20241011001Bulkhead · gougedTHERE ARE THREE GOUGES IN THE FS 169.00 BULKHEAD WHERE THE ATTACHMENT HARDWARE OF THE NOSE RADOME SEEN IN VIEW F PER CRJ 700 IPC 53-81-80 HAVE CONTACTED EACH OTHER. AT THE NINE-O CLOCK POSITION THE GOUGE DEPTH IS 0.023", AT THE SIX-O CLOCK POSITION THE GOUGE DOct 11, 2024 · N543EA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR WRXR20241008002Drain Line · corrodedFWD DRAIN VALVE TUBE ASSY ON PASSENGER DOOR SILL IS CORRODED THROUGH. REMOVED & REPLACED DRAIN TUBE ASSY SH670-31904-5 IAW CRJ700 SRM 51-42-06-001-001-A01.Oct 8, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20241008001Drain Line · corrodedAFT DRAIN VALVE TUBE ASSY ON PASSENGER DOOR SILL IS CORRODED THROUGH. REMOVED & REPLACED DRAIN TUBE ASSY SH670-31904-5.IAW CRJ700 SRM SRM 51-42-06-001-001-A01.Oct 8, 2024 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202304181111Gcu · unknownIDG 2 FAIL INFLIGHT, MULTIPLE STATUS MESSAGES APU BATTERY CHARGER, FLAPS HALFSPEED, SLATS HALFSPEED, DC ESS TIED CLOSED, DC MAIN TIE CLOSED, ICE DET 2 FAIL / REMOVED AND #2 GCU IAW CRJ 900 AMM 24-11-07-000/400-801 AND OPS CHECK GOOD IAW CRJ 900 AMM 24-11-01-71Apr 14, 2023 · N543EA · Cndair CL6002C10 · AC Generation SystemSDR VNAA2022112009915Floor Support · corrodedCORROSION ON RH FLOOR SILL UNDERSIDE FS 310- FS 319. REMOVED CORRODED RH FLOOR SILL PN:SH670-32172-11 IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH FLOOR SILL PN: SH670-32172-11 Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2022112099914Support Bracket · crackedDURING ACCESS FOUND SUPPORT BRACKET BETWEEN PANELS 195DL AND 196DR TO BE CRACKED TOWARDS THE AFT SECTION OF THE BRACKET. CORRECTIVE ACTION: LOCATED, DRILLED CHANNEL PN# CC670-39251-1 IAW CRJ700 SRM 51-40-11-001-001-A01 AND INSTALLED IAW CRJ700 SRM 51-42-06-Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2022112099913Angle · corrodedREAR FUSELAGE FAIRING SUPPORT FRAME, LOWER SPLICE IS CORRODED AT F.S. 939.00, STRINGER 27. CORRECTIVE ACTION: LOCATED, DRILLED, AND DEBURRED REAR FUSELAGE FAIRING SUPPORT FRAME, LOWER SPLICE AT F.S.939.00, STGR27 IAW CRJ700 SRM 51-40-11-001-001-A01. INSTANov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2022112099912Stringer · crackedFOUND FS280-295 STRINGER 3L HAS INDICATION NOTED 3.950 LONG 100%FSH FROM FWD EDGE OF STRINGER TO THE 4TH HOLE FAILED NDT INSPECTION CORRECTIVE ACTION: REPAIRED F.S. 280 TO F.S. 295 STRINGER 3L CRACK IAW BOMBARDIER REO 670-53-21-493, REV -B, DATED 2011-11-18Nov 20, 2022 · N543EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2022112099911Actuator · corrodedBUTE DOOR ACTUATOR SPRING ON THE RH WING OTBD FLAP MIDDLE HINGE BOX IS CORRODED. CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE BUTE DOOR ACTUATOR SPRING ON RH WING OTBD FLAP MIDDLE HINGE BOX IAW CRJ700 AMM 57-54-02-400-804-A01Nov 20, 2022 · N543EA · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202109171111Slat System · malfunctionedON THE WAY INTO KILM THE CREW HAD A SLATS FAILURE. ONCE ON THE GROUND MX HAD CLEARED THE FAILURE. FOR THE NEXT LEG TO KPHL THE EXACT SAME FAIRURE HAPPENED AT FL060 THEY THEN DECLARED AN EMERGENCY AND TURNED BACK TO KILM. THEY LANDED SAFELY WITHOUT ANY ISSUE."Sep 17, 2021 · N543EA · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR VNAA202108051111Acm · odorAT FL050 THE CREW SMELLED SMOKE AND CALLED TO THE FA WHO REPORTED THEY SMELLED IT IN THE CABIN. THE AFT FA SAID THERE WAS VISIBLE SMOKE AS WELL. THE CREW DECLARED AN EMERGENCY, RAN THE QRH AND THE SMOKE AND SMELL BEGAN TO DISSIPATE. THEY CONTINUED ON THE APPROAug 3, 2021 · N543EA · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA202012291111Acm · damagedCREW REPORTED SMOKE IN COCKPIT (NO FIRE) WHILE AT GATE IN CLT. PASSENGERS WERE DEPLANED THRU MAIN CABIN DOOR WITHOUT INCIDENT AND MAINTENANCE WAS CALLED TO AIRCRAFT. RIGHT AC PACK WAS FOUND TO BE THE CAUSE. 12/27/20: DEFERRED RT PACK, IAW CRJ-900 MEL 21-51-Dec 27, 2020 · N543EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA2020031615003Channel · crackedAFT BAGGAGE BAY STRUCTURE CHANNEL FOR BAGGAGE BAY DOOR IS CRACKED.-C/A-REPAIRED IAW ERS-CR-53MR-4070.Mar 15, 2020 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA202002253005Bracket · bentLH ELEVATOR UPPER INPUT ARM BRACKET (VERT. STAB. TO HORZ. STAB. FLANGES ARE BENT. (LEVER ASSY)-C/A-REMOVED AND REPLACED LH ELEVATOR UPPER BELLCRANK LEVER ON HORZ. STAB AFT SPAR IAW CRJ 700 27-31-30-400-805. SEE E776830 FOR OPS CHECK.Feb 23, 2020 · N543EA · Cndair CL6002C10 · Elevator StructureSDR SIMA202002253004Bracket · damagedRH ELEVATOR INPUT ARM BRACKET (VERT. STAB. TO HORZ. STAB.) FLANGES ARE BENT/CRACKED. (LEVER ASSEMBLY.)-C/A-REMOVED AND REPLACED RH ELEVATOR UPPER BELLCRANK LEVER ON HORZ. STAB. AFT SPAR IAW CRJ 700-27-31-30-400-805. SEE E776803 FOR OPS CHECK.Feb 23, 2020 · N543EA · Cndair CL6002C10 · Elevator StructureSDR SIMA202003021003Door Sill · corrodedCORROSION ON SERVICE DOOR SILL-C/A-REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-11, SRM 51-42-06, DRGSH670-3195, SRM 51-42-34 AND SRM 51-25-16.Feb 21, 2020 · N543EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA2020030419010Floorbeam · crackedRH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM FS280.00-C/A-REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF THE FLOOR BEAM AT FS 280.00 IAW SRM 53-11-43-201-003.Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA2020030419009Floorbeam · corrodedLH FLOOR BEAM AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION WHERE IT IS SANDWITCHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD.-C/A-REPLACED LH SIDE FLOOR BEAM AT FS280. IAW SRM 51-42-06 AND 51-42-13.Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA2020030419008Floorbeam · corrodedRH FLOOR BEAM AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION WHERE IT IS SANDWITCHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD.-C/A-REPLACED RH SIDE FLOOR BEAM AT FS280. IAW SRM 51-42-06 AND 51-42-13.Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA202003029005Floorbeam · crackedLH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM FS280.00-C/A-REPAIRED IAW SRM 53-11-43-201-003Feb 19, 2020 · N543EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA2020032706009Cover · crackedMULTIPLE EMERGENCY LIGHT STRIPS: (#1 FWD RHT AND LFT)(#2 RHT)(#3 LFT)(#4 LFT AND RHT)(#6 RHT)(#7 LFT)(#8 RHT AND LFT)(#9 LFT)(#10 EXIT RH FWD)(#12 RHT) ARE CRACKED.-C/A-COMPLETE:REMOVED AND REPLACED MULTIPLE EMERGENCY LIGHT STRIP COVERS IAW AMM 33-51-01.Dec 6, 2019 · N543EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20190903001Actuator · failedPITCH FEEL CAUTION MSG IN FLIGHT. QRH COMPLIED WITH. EMERGENCY DECLARED. C/A-REMOVED AND REPLACED LINEAR PITCH TRIM ACTUATOR IAW AMM 27-31-23 OPS CHECK GOOD.Sep 3, 2019 · N543EA · Cndair CL6002C10 · Stabilizer ActuatorSDR SIMA20190320002Flashlight · missingAFT FLIGHT ATTENDENT FLASHLIGHT MISSING-C/A-DEFERRED AFT FLIGHT ATTENDENT FLASHLIGHT TEMP INSTALLED. COULD NOT LOCATE TEMPORARY FLASHLIGHT. INSTALLED NEW AFT FLASHLIGHT IAW AMM 25-61-02. OPS CHECK GOOD IAW AMM 25-61-00. MEL 25-14 ITEM RESTOREDMar 20, 2019 · N543EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA2018073130002Handle · not seatedAFT CARGO CAUTION MSG AFTER TAKE OFF. FOUND CARGO DOOR HANDLE PARTIALLY OPEN. CLOSED CARGO DOOR AND VERIFIED SECURED. NO FURTHER DEFECTS NOTED.Jul 30, 2018 · N543EA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SIMA201807081004Flashlight · odorSTRONG SULFUR SMELL IN CABIN AND ALSO COCKPIT BURNS THE EYES BOTH ENGINE AND PACK ON. PERFORMED GVI FWD AVIONICS AFT BAY NO FINDINGS INSPECTED CABIN AND FOUND ALL FLASHLIGHTS BURNT SMELL LIKE SULFUR. RAN APU PACKS AND BLEEDS NO SMELL NOTED CREW RAN ENGINES NO Jul 6, 2018 · N543EA · Cndair CL6002C10 · Emergency EquipmentSDR SIMA201806185003Fan · failedON ENTERING THE COCKPIT, SMELLED A BURNED ELECTRONIC LIKE ODOR. PERFORMED FIM 21-21-00-810-806. FOUND RTU NR 2 INTERNAL FAN INOPERATIVE MESSAGE ON THE MDC. VERIFIED SOURCE OF THE ODOR TO BE THE RTU . R & R RTU 2 IAW AMM 23-81-01. OPS CHECKED GOOD.Jun 15, 2018 · N543EA · Cndair CL6002C10 · Communications SystemSDR SIMA20170821005Tire · failedNR 2 TIRE DESTROYED WITH THROWN THREAD SEPARATION. REMOVED AND REPLACED THE TIRE & WHEEL ASSEMMBLY IAW W/C 32-008.Aug 21, 2017 · N543EA · Cndair CL6002C10 · TireSDR SIMA20170626001Pcu · malfunctionedON DESCENT MOVED FLIGHT SPOILER UNF POSITION RECEIVED IB FLT SPOILERS AND IB SPOILERONS CAUTION MESSAGE. INTERROGATED MDC FOUND RT INBD MFS PCU JAM PERFORMED S POST 1 RESET PERFORMED OPS CHECK IAW ETN-CR-27-093 OPS CHECK GOOD.Jun 26, 2017 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20170226005Panel · crackedPAX DOOR AFT STEP PANEL HAS TWO CRACKS IN THE CORNERS. REPAIRED THE PAX DOOR AFT STEP SHELL IAW SRM 52-11-04 AND ETN CR-52-039R2Feb 26, 2017 · N543EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20161223004Acm · smokeRIGHT PACK AUTO FAIL SMOKE IN CABIN. R & R THE ACM AND TEMPERATURE CONTROL VALVE IAW AMM 21-51-08 AND AMM 21-51-20. OPS CHECKED GOOD AND NO LEAKS FOUND.Dec 23, 2016 · N543EA · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20160530003Vane · defectiveSTALL FAIL CAUTION POSTED JUST AFTER TAKEOFF. STICK SHAKER ACTIVATED CONTINUOUSLY AT & ABOVE FL 220. PULLED LT CHANNEL STALL PROTECTION CB B/C CAPTAINS LOW SPEED TAPE COMPLETELY CLOSED ON HIGH SPEED, FIRST OFFICERS SIDE NORMAL. FOUND LT AOA VANE FROZEN MSG May 30, 2016 · N543EA · Cndair CL6002C10 · Stall Warning SystemSDR SIMA20150828006Mcu · failedPITCH TRIM RUNAWAY NOTED, FOLLOWED BY STAB FAULT STATUS MSG, FOLLOWED BY AUTOPILOT STAB TRIM CAUTION MSG. TRANSFERRED TO NRWC 543-ORD-01276. R & R MCU IAW AMM 27-42-07. OPERATIONS CHECKED GOOD. REFERENCE NRWC 543-ORD-01276 FOR CORRECTIVE ACTION.Aug 28, 2015 · N543EA · Cndair CL6002C10 · Stabilizer ActuatorSDR SIMA20150828007Printed Ckt Board · inoperativeEMERGENCY LIGHTS CAME ON AFTER LANDING & REMAINED ON UNTIL FLIGHT ATTENDANT TURNED THEM OFF. PSU LIGHTS CAME ON & STAYED ON. INSPECTED ACFT & FOUND PCB AT SEAT 18A INOPERATIVE. REPLACED PCB AT 18A IAW 23-31-17. OPERATIONS CHECKED GOOD IAW 33-51-00TR. ACFTAug 28, 2015 · N543EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20150820002Warning System · false activationINBOARD FLIGHT SPOILERS CAUTION MSG ILLUMINATED DURING INITIAL APPROACH AT APPROX 4000 FT. DECLARED EMER, LANDED SAFELY & TAXIED TO GATE. POWERED UP ACFT, NO MSG POSTED. PERFORMED SELF-TEST OF THE SPOILER & STAB CONTROL UNIT IAW MM 27-61-05. CHECKED GOOD NAug 20, 2015 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150803001Handle · out of adjustPASSENGER DOOR WARNING AT 500FT ON FINAL. NR 1 FLIGHT ATTENDANT REPORTS RED FLAG UNLOCKED, APPEARED WHILE AIRBORNE. PRIOR LANDING FLIGHT ATTENDANT NR 2 OBSERVED DOOR HANDLE UP THEN DOWN, APPROXIMATELY 2" AFTER LANDING. ADJUSTED LATCH MECHANISM INNER HANDLEAug 3, 2015 · N543EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20150517001Warning System · false activationON APPROACH, INBD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSGS, DECLARED EMER. COMPLIED WITH AOM VOL 1. INTERROGATED MDC, FOUND RIB MFS PCU & PCU JAM MDC MSG. PERFORM SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.May 17, 2015 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150401004Warning System · false activationINBOARD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSG POSTED ON EICAS ON APPROACH AT 4000' WHEN FLIGHT SPOILERS DISPLAYED. CHECKED AML, NO HISTORY. PERFORMED RESET PROCEDURES IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.Apr 1, 2015 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150309005Pcu · failedOTBD FL & OTBD SPOILERONS CAUTION MSG AT 8,000 FT. TRANSFERRED TO NRWC 543-DFW-01187. LT OTBD MULTI-FUNCTION SPOILER PCU WAS R & R. OPERATIONS CHECKED GOOD WITH NO LEAKS. REFERENCE NRWC 543-DFW-01187 FOR WORK PERFORMED. FOLLOWING TURN OVER WORK PERFORMED,Mar 9, 2015 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150304005Warning System · activatedOUTBOARD SPOILERONS & OTBD FLIGHT SPOILER CAUTION MSGS IN FLIGHT WITH FLIGHT SPOILER HANDLE DEPLOYED. STOWED FLIGHT SPOILERS. MSG DID NOT EXTINGUISH. COMPLIED WITH AOM VOL 1 EMER PROCEDURES. CAUTION MSGS DID NOT EXTINGUISH. PERFORMED RESET IAW ETN-CR-27-0Mar 4, 2015 · N543EA · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150127008Angle · crackedRIGHT VERTICAL STABILIZER TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. REPAIRED RT VERTICAL STAB TO FUSELAGE FWD ANGLE AFT END IAW EO CR-55MR-038 & ERS CR--5500-230.Jan 27, 2015 · N543EA · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20150108012Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1 INCH LONG. REPAIRED IAW EO CR-55MR-038.Jan 8, 2015 · N543EA · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
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